Patent Assignment
Reel/Frame 026298/0269
Merger
Recorded: 2011-05-18
Pages: 75
Assignor
AIRBUS FRANCE
Executed: 2009-06-30
Assignee
AIRBUS OPERATIONS SAS
316, ROUTE DE BAYONNE,, 31060 TOULOUSE,, FRANCE
Covered Properties
(1107)
System Enabling the Flutter Behavior of an Aircraft to Be Improved
Patent:
5,224,667 →
Application:
07/827,612 →
Access Door, Especially for an Aircraft Engine Cowling, Provided with a Synchronized Pivoting Articulated Flap
Patent:
5,303,508 →
Application:
07/842,079 →
Process and Device for Synchronizing Two Digital Pulse Sequences S and Rf of the Same High Frequency
Patent:
5,315,271 →
Application:
07/894,246 →
Method of Signalling Insufficient Maneuverability of an Aircraft and Device Implementing Such a Method
Patent:
5,367,460 →
Application:
07/898,084 →
Three-Input Signal Section, Application to a Selector with N Inputs and to a Poller with N Inputs
Patent:
5,347,180 →
Application:
07/919,139 →
Three-Input Poller
Patent:
5,414,718 →
Application:
07/919,178 →
Device for Controlling the Speed of the Engines of an Aircraft
Patent:
5,277,024 →
Application:
07/921,238 →
Low Loss Power Switch
Patent:
5,291,082 →
Application:
07/935,098 →
A Sound and Thermic Insulation Mattress Having a Foam Insert for Securing to a Support and a Method for Preparing Such Mattress
Patent:
5,866,231 →
Application:
07/994,770 →
System for Control of an Aerodynamic Surface of an Aircraft
Patent:
5,374,014 →
Application:
07/994,907 →
Aircraft Flight Process When "Maintaining the Speed by Action on the Elevator
Patent:
5,386,954 →
Application:
08/023,208 →
Sealed Drainage Unit for a Hydraulic Circuit
Patent:
5,348,044 →
Application:
08/032,506 →
Device Managing Accessing Priority to Common Resources, of Functional Modules Divided Over a Plurality of Local Units in Each of Which They Form of Local Daisy Chain
Patent:
5,423,053 →
Application:
08/063,702 →
Command System with Interactive Command Sources, Enabling Any Number of Heterogeneous Systems to Be Accessed
Patent:
5,450,323 →
Application:
08/077,340 →
Method and Device for Manufacturing Adhesive Elements to Be Applied to a Three-Dimensional Surface for the Purpose of Decorating It
Patent:
5,556,491 →
Application:
08/087,333 →
Device for Attaching a Turbojet Engine to an Aircraft Structure
Patent:
5,447,282 →
Application:
08/102,560 →
Process for the Control of the Control Surfaces of an Aircraft for the Low Speed Compensation of a Lateral Path Deviation
Patent:
5,375,793 →
Application:
08/105,498 →
Press for Forming an Article of Composite Material Comprising Reinforcing Fibers in a Polymer Matrix
Patent:
5,378,134 →
Application:
08/108,402 →
Shock Detector and Distress Beacon for an Aircraft Incorporating Such a Detector
Patent:
5,394,142 →
Application:
08/113,595 →
Process for Connecting an Electric Cable Having a Light Metal Core to a Standardized End Element
Patent:
5,408,743 →
Application:
08/119,135 →
Rigid Kruger Nose for the Leading Edge of an Aircraft Wing
Patent:
5,474,265 →
Application:
08/126,708 →
Method and Device for Decorating a Trimimensional Object
Patent:
5,490,080 →
Application:
08/134,203 →
A Process and Device for Estimating the Altitude of an Aircraft Including an Inertial Reference Systems,Radio Altimeters and a Poller
Patent:
5,415,031 →
Application:
08/141,596 →
Device for Measuring a Physical Quantity by Time-Division Coding
Patent:
5,408,091 →
Application:
08/149,471 →
Method and a Machine for Making Hollow Reinforcing Members
Patent:
5,390,707 →
Application:
08/162,938 →
Integrated Multichannel Pressure Measuring System and Corresponding Measuring Process
Patent:
5,537,869 →
Application:
08/217,369 →
Flight Refuelling System
Patent:
5,499,784 →
Application:
08/241,018 →
Process and Device for Detecting the Current Phase of Operation of a System with Multiple Phases of Operation
Patent:
5,479,346 →
Application:
08/242,979 →
Device for Controlling a Mechanism Driven by a Lens One Electric Motor
Patent:
5,598,312 →
Application:
08/248,952 →
Method and Device for Multimode and Multifunction Communication Between an Operator and One or More Processors
Patent:
6,072,473 →
Application:
08/249,079 →
Method and Device for Assistance in Piloting an Aerodyne by the Graphic Representation of the Vertical Flight Plan of This Aerodyne
Patent:
5,445,021 →
Application:
08/266,118 →
Process for Connecting an Electric Cable to an End Member
Patent:
5,499,448 →
Application:
08/275,953 →
A System for Controlling a Plurality of Parallel Hydraulic Circuits in an Aircraft
Patent:
5,623,411 →
Application:
08/282,216 →
Device for Supervising the Propulsion System of an Aircraft
Patent:
5,608,627 →
Application:
08/308,427 →
Electrical Flight Control System for an Airplane, with Attitude Protection on Takeoff
Patent:
5,527,002 →
Application:
08/314,815 →
Crimping Tool for the Connection of an Electric Cable in an End Element
Patent:
5,546,653 →
Application:
08/314,828 →
Method and Apparatus for Checking the Integrity of a Complex Computer Installation Used in the Flight Control of an Aircraft
Patent:
5,579,511 →
Application:
08/324,374 →
Digital Bus Simulator Integrated in a System for Automatically Testing Electronic Packages Embarked on an Aircraft
Patent:
5,615,136 →
Application:
08/342,828 →
A Process and Device for Detecting Operating Inconsistencies in a System with Multiple Phases of Operation
Patent:
5,713,007 →
Application:
08/348,873 →
Method and Device for Detecting That the Design Loads of an Aircraft Have Been Exceeded
Patent:
5,511,430 →
Application:
08/350,082 →
Method for the Production of a Silicone-Based Fireproof Protection Means and Protection Means Thus Obtained
Patent:
5,571,625 →
Application:
08/358,713 →
Aircraft and in Particular Rotary-Wing Aircraft Seat Having an Energy Absorption Device Automatically Adjustable as a Function of the Size of the Occupant
Patent:
5,558,301 →
Application:
08/360,564 →
Apparatus for the Fabrication of Fiber Composites with a Vitreous or Glass-Ceramic Matrix
Patent:
5,639,337 →
Application:
08/360,983 →
Adaptor for a Machine for Testing Electronic Equipment
Patent:
5,562,505 →
Application:
08/377,458 →
Method and Device for Finding Spurious Maintenance Messages
Patent:
5,610,923 →
Application:
08/377,609 →
Process for the Replacement of a Hydraulic Fluid Contained in a Control Circuit Such as an Aircraft Circuit
Patent:
5,641,003 →
Application:
08/418,206 →
Device for the Protection of a Control Surface Hinge Particularly for an Aircraft
Patent:
5,622,336 →
Application:
08/421,985 →
Transport Airplane with Front Empennage
Patent:
5,722,615 →
Application:
08/433,727 →
Device for Making Use of Information Related to the Breakdown Detected by One or More Central Units of an Aircraft
Patent:
5,500,797 →
Application:
08/443,095 →
Process for Regulating the Orientation of a Support Structure Such as That Carrying a Head-Up Control System on an Aircraft
Patent:
5,612,687 →
Application:
08/453,576 →
Process and Device for Indentifying Faults in a Complex System
Patent:
5,774,645 →
Application:
08/521,060 →
Hydraulic Equipment Draining Means
Patent:
5,770,053 →
Application:
08/541,615 →
Process for the Space Localization of the Focal Point of a Laser Beam of a Machining Machine and Equipment for Performing This Process
Patent:
5,670,773 →
Application:
08/555,005 →
Conical Rotary Actuator and Its Application to the Control of a Rudder
Patent:
5,722,616 →
Application:
08/562,761 →
Gripping Tool for Machining Parts on a Machine Tool
Patent:
5,582,397 →
Application:
08/562,794 →
Variable Slot Airbrake for Aircraft Wing
Patent:
5,735,485 →
Application:
08/577,834 →
Sealing Device Between an Air Inlet and a Fan Frame of a Turbofan Engine
Patent:
5,706,648 →
Application:
08/595,670 →
Device for Fixing an Air Intake to a Jet Engine and Jet Engine Incorporating Such a Device
Patent:
5,737,914 →
Application:
08/608,594 →
Emergency Exit Accessible from the Outside for an Aircraft Cockpit
Patent:
5,769,361 →
Application:
08/611,548 →
Turbofan Engine with a Floating Pod
Patent:
5,642,615 →
Application:
08/618,840 →
System for Deriving an Anomaly Signal During the Take-Off of an Aircraft
Patent:
5,668,541 →
Application:
08/635,977 →
Device for Bleeding Off and Cooling Hot Air in an Aircraft Engine
Patent:
5,782,077 →
Application:
08/647,060 →
Device for Bleeding Off and Cooling Hot Air in an Aircraft Engine
Patent:
5,729,969 →
Application:
08/647,063 →
Aircraft Motor Pod Including a Pivotable Cowling
Patent:
5,755,403 →
Application:
08/652,002 →
Method for Producing a Panel or the Like with Structural and Acoustic Properties and Panel Obtained by Said Method
Patent:
5,888,610 →
Application:
08/655,932 →
Method for the Production of a Silicone-Based Fireproof Protection Means
Patent:
5,716,668 →
Application:
08/657,047 →
Aid Method Concerning the Specification of an Interface Between a Control Terminal and at Least One Computer
Patent:
5,828,373 →
Application:
08/662,015 →
Sandwich Panel Made of a Composite Material and Production Method
Application:
08/662,765 →
Process and Device for Guiding a Mobile Craft
Patent:
5,925,079 →
Application:
08/681,977 →
Method and Device for Supplying Information, an Alert or Alarm for an Aircraft in Proximity to the Ground
Patent:
5,798,712 →
Application:
08/682,711 →
System for Controlling a Control Surface Articulated to a Structure of a Vehicle
Patent:
5,823,471 →
Application:
08/688,095 →
Turbofan with Thrust Reversal Doors Not Submitted to Bypass Air in Their Inactive Position
Patent:
5,722,231 →
Application:
08/690,165 →
Process and Device for the Control of the Rudder of an Aircraft
Patent:
5,791,596 →
Application:
08/708,698 →
Machine for Marking an Electric Cable
Patent:
5,827,391 →
Application:
08/729,744 →
Radio Navigation Testing Method and Device Using Standard Signal Measuring and Generating Equipment
Patent:
5,790,438 →
Application:
08/760,575 →
Device for Monitoring a Complex System Such as an Aircraft
Patent:
5,838,261 →
Application:
08/768,989 →
Device for Maintaining the Speed of an Aircraft Within a Particular Speed Range
Patent:
5,884,870 →
Application:
08/829,081 →
Process and Device for Damping Vibrations or Preventing Their Appearance in Aircraft Airframes in Transonic Flight
Patent:
5,890,675 →
Application:
08/838,140 →
Computer Module Having Removable Remotely Programmable Non-Volatile Memory
Patent:
6,038,640 →
Application:
08/847,382 →
Instrumented Device of Small Thickness Forming a Skin
Patent:
5,874,671 →
Application:
08/871,958 →
Method and Device for Vertical Guidance of an Aircraft
Patent:
5,957,412 →
Application:
08/936,549 →
Braided Tubular Structure for a Composite Part Its Construction and Its Applications
Patent:
6,495,227 →
Application:
08/942,326 →
Flying Aid Device for a Fly-by-Wire Aircraft
Patent:
6,000,662 →
Application:
08/950,366 →
Device for Allowing the Use in an Aircraft of Radio Communication Means
Patent:
5,887,258 →
Application:
08/957,086 →
System for Coupling Control Columns
Patent:
5,900,710 →
Application:
08/976,479 →
Method and Device for Detecting Vertical Gusts of Wind and Application Thereof to the Pitch-Attitude Control of an Aircraft
Patent:
5,995,880 →
Application:
08/977,016 →
Method for Protecting an Aircraft Against Vertical Gusts of Wind and Pitch-Attitude Control Device Employing This Method
Patent:
6,044,311 →
Application:
08/977,754 →
Water Repellent Composition
Patent:
5,973,055 →
Application:
08/995,001 →
Process and Device for the Control of the Rudder of an Aircraft
Patent:
6,206,329 →
Application:
09/003,890 →
Process and Device for Verifying the Consistency of the Measurements from an Angle-of-Attack Probe
Patent:
6,073,084 →
Application:
09/033,977 →
Process and Device for Determining an Optimal Flight Path of an Aircraft
Patent:
6,148,259 →
Application:
09/034,785 →
Data Link System Between an Aircraft and the Ground and Procedure for Recovering from a Failure
Patent:
6,173,230 →
Application:
09/055,267 →
Device for Measuring Noise in a Pipe Traversed by a Fluid
Patent:
5,925,821 →
Application:
09/092,960 →
Device for Attaching an Engine to an Aircraft
Patent:
6,059,227 →
Application:
09/098,953 →
Turbojet Pod with Laminar Flow
Patent:
6,179,249 →
Application:
09/125,204 →
Aircraft Landing Gear Element with Mechanically Slewable Undercarriage and Axles
Patent:
6,029,931 →
Application:
09/125,205 →
Noise Reducing Connection Assembly for Aircraft Turbine Housings
Patent:
6,123,170 →
Application:
09/132,902 →
Acoustically Resistive Layer, Process for Production of This Layer and Absorbent Acoustic Panel Provided with at Least One Such Layer, as Well as Its Process for Production
Patent:
6,268,038 →
Application:
09/133,678 →
Device for Starting a Gas Turbine in an Aircraft
Patent:
6,351,090 →
Application:
09/175,654 →
Protective Device for a Jet Engine Air Inlet Cowl Equipped with a Deicing System
Patent:
6,241,189 →
Application:
09/190,104 →
Deicing Device for a Jet Engine Air Inlet Cowl
Patent:
6,193,192 →
Application:
09/190,105 →
Hot Air Diffuser for a Jet Engine Air Inlet Cowl with De-Icing Circuit
Patent:
6,079,670 →
Application:
09/203,376 →
Device for Removing Hot Air for a Jet Engine Air Inlet Cowl with a De-Icing Circuit
Patent:
6,131,855 →
Application:
09/203,377 →
Device and Method for Interconnection Between Two Electronic Devices
Patent:
6,031,728 →
Application:
09/204,502 →
Device for Controlling Operation and Operating Power of Radiocommunication Unit to Allow Use in an Aircraft
Patent:
6,269,243 →
Application:
09/216,919 →
Engine Control System for an Aircraft
Patent:
6,088,632 →
Application:
09/225,571 →
Process for Depositing by Winding on a Support Several Rovings Simultaneously of Pre-Impregnated Fibers, Device for Practicing the Same, and Structure of a Composite Material Thus Obtained
Patent:
6,431,490 →
Application:
09/235,764 →
Attachment Device for an Aircraft Engine
Patent:
6,173,919 →
Application:
09/236,899 →
Aircraft Hot-Air Supply System
Patent:
6,058,725 →
Application:
09/244,434 →
Device for Attaching an Engine to an Aircraft Strut
Patent:
6,209,822 →
Application:
09/244,629 →
Aircraft Fore Structure
Patent:
6,213,428 →
Application:
09/245,842 →
Fibrous Reinforcement for a Composite Component, and Process and Device for Producing It
Patent:
6,123,043 →
Application:
09/292,837 →
Removable Rear Connector for a Plug Such as a Circular Electrical Plug
Patent:
6,196,865 →
Application:
09/297,526 →
Telescopic Rod for Opening a Mobile Cowl, in Particular of an Aircraft Engine Bay
Patent:
6,334,730 →
Application:
09/297,745 →
Opening Device Common to Two Adjacent Aircraft Engine Nacelle Covers
Patent:
6,227,485 →
Application:
09/297,887 →
Hybrid Control System for an Aircraft Aerodynamic Surface
Patent:
6,241,182 →
Application:
09/300,915 →
Aircraft with Reduced Wing Structure Loading
Patent:
6,064,923 →
Application:
09/301,171 →
Autonomous Device for Limiting the Rate of Flow of a Fluid Through a Pipe, and Fuel Circuit for an Aircraft Comprising Such a Device
Patent:
6,182,688 →
Application:
09/306,570 →
Aircraft Propulsion Unit with Fan Cowls Equipped with Maintaining and Positioning Safety Elements
Patent:
6,334,588 →
Application:
09/341,573 →
Composite Material Panel with Shock-Protected Edges
Patent:
6,479,124 →
Application:
09/341,960 →
Device and Method for Severing Lesions
Patent:
6,315,782 →
Application:
09/351,292 →
Method for Making a Composite Panel and Resulting Panel
Patent:
6,375,121 →
Application:
09/355,197 →
Device for Locating a Rupture in a Transparent Panel with at Least Two Panes and Panel Thus Obtained
Patent:
6,346,314 →
Application:
09/393,018 →
Hinge for Movable Control Surfaces in an Aircraft and a Connecting Piece to Be Used with Such a Hinge
Patent:
6,270,039 →
Application:
09/416,622 →
Method for Implementing an Air Traffic Service Unit
Patent:
6,275,767 →
Application:
09/456,434 →
Air Intake Structure for Aircraft Engine
Patent:
6,328,258 →
Application:
09/461,177 →
Process and Control System for an Aircraft Control Surface Actuated by Multiple Hydraulic Jacks and with Modular Power
Patent:
6,651,930 →
Application:
09/467,299 →
Aircraft Landing Gear, Equipped with a Device for Protection of a Nearby Fuel Tank, and Aircraft Equipped with This Landing Gear
Patent:
6,264,139 →
Application:
09/473,956 →
Sandwich Panel Made of a Composite Material and Production Method
Patent:
6,267,838 →
Application:
09/477,406 →
System for the Yaw Control of an Aircraft
Patent:
6,352,223 →
Application:
09/497,397 →
Process for the production of flexible silicone membranes particularly in the case of molding by resin transfer
Application:
09/511,304 →
Aerospatiale Matra Airbus
Patent:
6,508,401 →
Application:
09/515,922 →
Device for Emitting a Time Varying Signal in the Field of Vision of a Picture Taking Device
Patent:
6,801,249 →
Application:
09/522,295 →
Structure for attaching a landing gear to an aircraft fuselage
Patent:
6,273,364 →
Application:
09/557,968 →
Process for Providing Metallized Areas on Surface by Electrically Detecting Removal of Insulating Layer
Patent:
6,495,197 →
Application:
09/560,332 →
Process for Protection Against Corrosion by Chemical Products, of Flexible Self-Demoulding Silicone Membranes
Patent:
6,261,503 →
Application:
09/560,335 →
Aircraft comprising a landing gear with controlled detachment in the event of an accident
Patent:
6,318,669 →
Application:
09/577,886 →
Method of Manufacturing a Sandwich Panel, Made of Composite Material, and a Panel Thereby Obtained
Patent:
6,679,969 →
Application:
09/642,650 →
Closure Fault Indicator, Particularly for an Aircraft Engine Pod Cowl
Patent:
6,666,408 →
Application:
09/689,830 →
Aircraft Wing Structure Profiled Suspension Pylon
Patent:
6,378,804 →
Application:
09/697,072 →
Auxiliary Nose Landing Gear for Aircraft
Patent:
6,698,689 →
Application:
09/699,685 →
Method and Device for the Surface Machining of a Structure Such as a Cellular Structure
Device for Discharging Hot Air for a Jet Engine Air Inlet Cowl, with a Deicing Circuit
Process for the Production of an Acoustively Resistive Layer, Resistive Layer Thus Obtained, and Wall Using Such Layer
Flight Control Indicator for an Aircraft, Intended to Supply the Engine Pressure Ratio
Rotatable Gripping Device for Transport or Machining of an Arbitrarily Shaped Part
Aircraft Wing Structure Profiled Suspension Pylon
Device for Aircraft Thrust Recovery Capable of Linking a Turboshaft Engine and an Engine Strut
Electromagnetic Pulse Train Generation for Testing Optical Fibres
Patent:
6,762,828 →
Application:
09/806,343 →
Device for Pressure Tapping and Procedure for Setting It on a Fuselage Panel of an Aircraft
Method for Determining a Minimum Control Speed for an Aircraft
Aircraft Door and Aircraft Fitted with Such a Door
Process for the Production of a Panel of Composite Material with Stiffening Strips
Aricraft with Electrical Fly-by-Wire Controls, Equipped with an Automatic Pilot
Method for making a sound reducing panel with resistive layer having structural property and resulting panel
Application:
09/914,181 →
Publication:
US 2002/0157764
Air Inlet Cowl for a Jet Engine Equipped with De-Icing Means
Process and Device for Detecting the Lift-Off of an Aircraft in the Course of Take-Off
Process for Hydroforming Sheet Metal and Device for Practicing the Same
Noise Reduction Sandwich Panel, Notably for Aircraft Turbojet Engine
Device and Mechanism for Transmission of Radial Forces Between the Central and End Regions of This Device
Device for Determining the Values of at Least One Parameter of Particles, in Particular Water Droplets
Boarding Device for Aircraft and Flying Wings Equipped with Such a Device
Sandwich Acoustic Panel
System for Automatically Controlling Lift-Augmentation Devices of an Aircraft During Take-Off
Process and Device for Deterministic Transmission of Asynchronous Data in Packets
Device and process for flow control in a switched network
Application:
09/995,820 →
Publication:
US 2002/0118646
Real Time Multi-Task Process and Operating System
Electrical Energy Distribution System and Contactor for Such a System
Method and Device for Controlling an Aircraft Manoeuvring Components, with Electrical Standby Modules
Articulation Device for an Aircraft Door Panel and an Aircraft Door Integrating Such a Device
Device for Joining a Panel and a Structure, Able to Transmit Significant Forces
Device for Attachment of an Engine Onto an Aircraft Nacelle Stub
Aircraft Dialog Device, Through Which a Dialog with a System of Said Aircraft Is Possible
Device for Controlling a System for Monitoring the Environment of an Aircraft, in Particular of a Transport Aircraft
Aircraft Dialog Device, for Dialog with a System of Said Aircraft
Device for Reviewing the Flight Plan of an Aircraft, in Particular of a Transport Plane
Control Device for a Communication System of an Aircraft, in Particular of a Transport Plane
Electronically Controlled Hydraulic Actuating System
Device for Monitoring a Plurality of Systems of an Aircraft, in Particular of a Transport Aircraft
Process for De-Icing an Air Intake Cowling of a Reaction Motor and Device for Practicing the Same
Process for De-Icing by Forced Circulation of a Fluid, an Air Intake Cowling of a Reaction Motor and Device for Practicing the Same
Method for Producing a Panel Comprising an Adapted Acoustically Resistive Layer and Panel So Obtained
Method and Device for Assistance with the Piloting of an Aircraft, Especially a Transport Airplane
Air Inlet Cowl for a Jet Engine, Provided with Deicing Means
Device and Process for Documentary Assistance of an Aircraft Operator, in Particular a Pilot of the Aircraft
Fast Evacuation Device for Aircraft
Flight Simulator Adapted for a Family of Aircraft
Antenna for Transmission / Reception of Radio Frequency Waves and an Aircraft Using Such an Antenna
Process and Device for Controlling at Least One Aerodynamic Elevator Surface of an Aircraft During a Takeoff
Aircraft with Ventral Fairing and Seal for Such an Aircraft
Device for Recovery of Forces Generated by an Aircraft Engine
Process for producing a reinforced acoustically resistive layer, resistive layer thus obtained and panel using such a layer
Application:
10/173,095 →
Publication:
US 2003/0021976
Method for the Production of Metal Profiles
Optimised Method for Assembling Two Substantially Flat Parts
Process for the Production of Holes Particularly Micro-Perforations in a Composite Material, Device for Its Practice and Sound Damping Layer Constituted by Said Material
Rotary Cutting Tool and High Speed Machining Method with Nano-Lubrication Using Such a Tool
Device for the Attachment of an Engine to an Aircraft
Aircraft with Ventral Fairing and Seal for Such an Aircraft
Air Inlet for Commercial Aircraft Jet Engine Nacelle
Airport Display Device
Deterministic Field Bus and Process for Managing Same Such That When Transmissions from One Subscriber Station Are Enabled Transmissions from Other Subscriber Stations Are Disabled
Process and Device for Aiding the Piloting of an Aircraft
Aircraft Windshield Attachment Device
Method and Device for Displaying a Velocity Vector of an Aircraft
Control Device and Method for Emergency Opening of an Aircraft Evacuation Door
Tubular Acoustic Attenuation Piece for an Aircraft Jet Engine Air Intake
Process for the Production of Composite Tubing Particularly for Air Conditioning and Tubing Thus Obtained
Switched Full-Duplex Ethernet Type Communication Network and Implementation Process for This Network
Process for Implementation of a Redundant Switched Full-Duplex Ethernet Type Communication Network
Process for Checking the Deterministic Behavior of a Packet Switching Network
Ball Joint Bearing Block Lubrication Device
Process for Management of a Light Signaling Device, and a Device Using This Process, Particularly for Avionics
Light Signaling Device Related to the Operating State of a System
Acoustically Resistive Layer for an Acoustical Attenuation Panel, Panel Using Such a Layer
Process for Making a Composite Material Assembly and Aircraft Wing and Stabilizing Element Obtained by This Process
Gripping Unit for Automated Machining of Parts, and Machining Device and Process Integrating Such a Unit
Device for Indicating Incorrect Closure of Locking Means Located Between Two Fan Cowlings of an Aircraft Engine Nacelle
Process and Device for Assembly of Landing Gear on an Aircraft Structure and Aircraft Comprising Such Landing Gear
Aircraft Engine Pod with Acoustic Attenuation
Method and Device for Depositing Adhesive on an Alveolar Surface
Aircraft with Electric Flight Controls Provided with a Fuselage Able to Deform and Vibrate
Method and Device for Transmitting Data on an Aircraft
Method of Guiding an Aircraft in the Final Approach Phase and a Corresponding System
Ejectable Door for Aircraft
Closing System Interposed Between Two Elements
Method of Identifying a Source of a Signal
Distress Beacon, Process and Device for Monitoring Distress Signals, and Vehicle on Which Such a Device Is Installed
Process and Device for Testing Parts by X Rays
Device for Weighing an Object by Lifting Which Invalidates a Weight Measurement Reading Whenever a Detected Shear Force Is Too Great
Device and Process for Acquisition of Measurments Using a Digital Communication Bus, Particularly Used During Aircraft Tests
Process for Forming a Sector of an Air Intake Lip, Device for Practicing the Same, and Sector Thus Obtained
Process for Ultrasonic Bonding
Installation, gateway and process for downloading information between equipment onboard an aircraft and offboard loading means
Application:
10/397,598 →
Publication:
US 2003/0182404
Control System and Process for Several Actuators
Multi-Component Acoustically Resistive Layer for Acoutical Attenuation Panel and Panel Thus Obtained
Perforated Adhesive Film and Its Manufacturing Process
Composite Beam with Integrated Rupture Initiator and Aircraft Fuselage Including Such Beams
Device for Connecting Two Tubular Pieces of an Aircraft Turbine Engine
Method and Device for Reducing the Vibratory Motions of the Fuselage of an Aircraft
Device for Aiding the Visual Spotting of an Aircraft in Flight from Another Aircraft, Also in Flight
Device for Articulating a Flap to an Aircraft Aerodynamic Surface
Aircraft with Active Control of the Warping of Its Wings
Exchanger for Aircraft Air Conditioning Circuit and Integrated Propulsion Assembly for Such an Exchanger
Flight Control Indicator for an Aircraft, in Particular a Transport Airplane, Intended to Supply the Thrust Generated by at Least One Engine of the Aircraft
Rapid-Opening Door
Method and Device for Automatic Control of an Aircraft Deceleration in Running Phase
Device for Assembly of Landing Gear on an Aircraft Structure
Process and System for Piloting an Aircraft
Process and Device for Devising an Abridged Form of Any Term That Is Used in an Alarm Message Intended to Be Displayed on a Screen of the Cockpit of an Aircraft
Sound Attenuation Panel Comprising a Resistive Layer with Reinforced Structural Component
Hooking Strut of an Engine Under the Wing Unit of an Aircraft
Method and Circuit for Real Time Frequency Analysis of a Non-Stationary Signal
System for Controlling the Operation of at Least One Aircraft Engine
Device for Lock-Fixing an Apparatus Designed to Be Mounted in a Rack
Door Which Is Intended to Be Positioned Between the Cockpit and the Cabin Ofan Aircraft
Process and a Device for the Machining of Panels
Movable Tyre Test Bench and Method Therefor
Tooling for Molding with Keys Particularly for the Production of Air Intakes Without Clips
Process and Device for Aiding the Driving of a Vehicle Running Over the Ground
Device and Method for Protection Against Overcurrents in an Electrical Energy Distribution Cabinet
Method and System for Controlling an Aircraft Control Surface
Process and System for Moving a Control Surface of an Aircraft
Device and System for Filtering Vibrational Movements of a Passenger Support, and Passenger Support Equipped with Such a System
Process and Device for Automatically Controlling the Thrust of at Least One Engine of an Aircraft During a Phase of Horizontal Flight at Stabilized Speed
Method for Detection of a Shielding Fault in a Multiwire Cable
Fly-by-wire control system for an aircraft comprising detection of pilot induced oscillations and a control for such a system
Application:
10/703,564 →
Publication:
US 2005/0021193
Process and Device for Detecting the Failure of a Pressure Sensor of an Air Data System of an Aircraft
Method and Device for Detecting Pilot Induced Oscillations in an Aircraft
Inertial Reference System for an Aircraft
Method for Controlling the Flight of an Aircraft
Aircraft Dialog Device for Dialog with System of Aircraft
Method for Displaying Flight Information
Display System for an Aircraft
Aircraft Dialog Device for Dialog with System of Aircraft
Process for Transmitting Asynchronous Data Packets
Aircraft Dialog Method Including Auxiliary Object Marker
Aircraft Dialog Device Including Discrete Moving Mechanism
System for Transmitting Asynchronous Data Packets
Process for Controlling a Switched Full-Duplex Ethernet Type Communication Network
Method for accelerating destruction of a vortex formed by a wing of an aircraft
Application:
10/717,465 →
Publication:
US 2004/0256521
System for Identifying a Signal Source
Package Switching Network with a Deterministic Behavior
Redundant Switched Full-Duplex Ethernet Type Communication Network
Process for Implementing a Switched Full-Duplex Ethernet Type Communication Network with Redundancy
Switched Full-Duplex Ethernet Type Communication Network and Implementation Process for This Network
Method for Identifying a Signal Source
Process and System Evaluating Deterministic Behavior of a Packet Switching Network
Airport Display Device
Apparatus for accelerating destruction of a vortex formed by a wing of an aircraft
Application:
10/717,672 →
Publication:
US 2005/0006533
Airport Display Method Including Changing Zoom Scales
Method for Monitoring a Plurality of Systems of an Aircraft Including Displaying Tasks Already Performed
Device for monitoring a plurality of systems of an aircraft including a display displaying tasks already performed
Aircraft Cockpit Window
Control Device and Method for Emergency Opening of an Aircraft Evacuation Door
Method of manufacturing a sandwich panel, made of composite material, and a panel thereby obtained
Application:
10/760,027 →
Publication:
US 2004/0146687
Method and Device for Determining a Final Approach Path of an Aircraft for a Non-Precision Approach for the Purpose of Landing the Aircraft
Method and Device to Assist in the Piloting of an Aircraft in a Non-Precision Approach During a Landing Phase
Articulated Junction Device
Protection Device for a Jet Engine Air Intake Structure
Process and Device for Constructing a Synthetic Image of the Environment of an Aircraft and Presenting It on a Screen of Said Aircraft
Device for Moving a Machine
Method and Indicator for Displaying Information Showing the Airspeed Tolerance Margins for an Aircraft
Process for Countering the Vibrations Induced in an Aircraft by the Windmilling of a Fan and System of Electric Flight Controls Implementing This Process
Switching Method and Device on an Aircraft Radiofrequency Landing System
Method and Device for Determining at Least One Cue of Vertical Position of an Aircraft
Aircraft Piloting System, at Least for Piloting the Aircraft During a Non Precision Approach with a View to a Landing
Method and on board device for providing pilot assistance in the lack of air control
Application:
10/810,125 →
Publication:
US 2011/0298648
Aircraft Engine in Which There Is a Small Clearance Separating the Fan Cowls and the Thrust Inverter Cowls
Aircraft Cockpit Display Device for Information Concerning Surrounding Traffic
Process for the Production of a Panel of Composite Material with Stiffening Strips and Panel Thus Obtained
Method and Device for Piloting an Aircraft
Device for Adjusting at Least One Parameter, in Particular for an Aircraft Automatic Pilot System
Aircraft Standby Display Device and System
Process and System for Transmitting Information on an Aircraft
Process and System for Transmitting Information on an Aircraft
Device and Process for Acquisition of Measurements Using a Digital Communication Bus, Particularly Used During Aircraft Tests
Method for Illuminating Particles for the Purpose of Forming Their Images
Milling Tool
Method and Device for Monitoring the Validity of at Least One Parameter Which Is Calculated by an Anemometeric Unit of an Aircraft
Method and Device for Generating a Flight Plan for a Tactical Flight of an Aircraft
Patent:
7,272,491 →
Application:
10/883,803 →
System for Aiding Control of the Deceleration of an Aircraft Moving Over the Ground
System for Automatically Controlling Lift-Enhancing Devices of an Aircraft, in Particular Wing Leading Edge Slats
Gripping Unit for Automated Machining of Parts, and Machining Device and Process Integrating Such a Unit
Process and Device for Monitoring the Validity of a Speed Cue of an Aircraft and System for Generating a Speed Cue Comprising Such a Device
Process and Device for Supplying the Turbojets of an Aircraft During Automatic Flight
Screwed Device Tightening/Untightening Tool
Aircraft Equipment Control System
Method and Device for Controlling the Attitude of an Aircraft
Device and Method for Measuring Parameters During Flight Tests of an Aircraft
Aircraft Provided with Thrust Reversers
Maintenance Process and Device for a Radionavigation Installation of an Aircraft
Fixed Frequency Electrical Generation System and Corresponding Control Procedure
Method of Designing and Manufacturing a Pipe Fitting, Particularly for Aircraft
Terrain Avoidance Method and Device for an Aircraft
Method and Spoiler System for Ensuring the Aerodynamic Continuity of the Upper Surface of an Aircraft
Device for Assembly of a Shroud Placed Between an Aircraft Engine Air Intake and a Pylon
Procedure and Device for Optimizing the Quantity of Fuel Transferred on an Aircraft During at Least One in-Fligh Fuel Transfer
Device for Equipping a Hole in a Panel, and Panel Thus Equipped
Procedure for Determining Modifications Made to an Electronic Card and Methods of Fabricating an Electronic Card and an Item Equipment Provided with an Electronic Card
System for Monitoring a Plurality of Zones
Aircraft Partition Designed to Separate a Cargo Part from a Cockpit or from a Passenger Compartment
Aircraft Partition Designed to Separate a Cargo Part from a Cockpit or from a Passenger Compartment
Engine Mounting Structure Under an Aircraft Wing
Structure for Mounting a Turboprop Under an Aircraft Wing
Mounting Structure for Mounting a Turboprop Under an Aircraft Wing
Self-Stiffened Panels of Preimpregnated Composite and Manufacturing Process for Components of Such Panels
Assembly comprising two metallic parts protected against the formation of a galvanic couple
Application:
10/994,285 →
Publication:
US 2007/0184261
Hanging Device to Connect an Engine to an Aircraft Wing
Engine Mounting Structure Under an Aircraft Wing
Method Making It Possible to Prevent Vibration of a Rudder of an Aircraft and Aircraft Using This Method
Parachuting Aid Method and Device
Process and Device for Detecting on an Aricraft an Overshoot of Design Loads at the Level of a Structural Part of Said Aircraft
Switched Flight Test Installation with a "Packet" Type Data Format
Placement Process for Elements of a Self-Stiffened Panel of Preimpregnated Composite
Method for making a laminated structure and aircraft provided with such a structure
Application:
11/001,682 →
Publication:
US 2005/0224655
Process for Reducing the Aerodynamic Loads Applied to the Elevators of an Aircraft During Takeoff
Method and System for the Automatic Piloting of an Aircraft on the Approach to an Airdrop Position
Process for Improving the Maneuverability of an Aircraft During a Resource
Machine and Machining Method for a Long Profile
Redundant Communication Network of the Switched Full-Duplex Ethernet Type and a Management Method of the Redundancy of Such a Network, Notably in the Avionic Domain
Device for assembly of several elements by riveting and procedure for assembly of panels especially for aircraft fuselages by means of said device
Application:
11/010,187 →
Publication:
US 2005/0183260
Anti-Loosening Device for Screw or Nut
Device for Crimping a Contact on a Cable
Apparatus for Forming Complex Sheets of Composite Material by Hot Stamping and Tool for Its Implementation
Drain Particularly for Engine Support Strut
Aircraft Nose with Shield
Method to Joggle a Structural Element and Structural Element Joggled According to This Method
Device for the Protection of a Probe Joined to an External Wall of an Aircraft
Acoustic Measuring System for Locating Noise Sources
Electrical Connection Device to Make a Metallisation Point, Support Equipped with Such a Connection Device and Aircraft Equipped with Such a Support
Fire Extinguishing Device
Process for the Production of an Electrical Wiring Diagram
Method and Device for Verifying a Temperature Value at a Destination Altitude of an Aircraft
Method and Device for Calculating a Target Speed for an Aircraft
Seat Rail for Aircraft Cabin and Method of Manufacturing Such a Rail
Process for Improving the Landing of an Aircraft
Landing Gear Door with Controlled Kinematic Control
Hinged Door for Aircraft Landing Gear
Process and Mechanical Device for Machining Flexible Panels, in Particular with a Complex Shape
Process and Device for Localized Gripping and Holding of a Thin, Flexible Panel, in Particular Having a Complex Shape
Communicating Ladder Between an Upper Level and a Lower Level of an Aircraft, and an Aircraft Provided with Such a Ladder
Process and Device for Machining by Windowing of Non-Deformable Thin Panels
Mounting System Inserted Between an Aircraft Engine and a Rigid Structure of an Attachment Strut Fixed Under a Wing of This Aircraft
Mounting System Inserted Between an Aircraft Engine and a Rigid Structure of an Attachment Strut Fixed Under a Wing of This Aircraft
Mounting System Inserted Between an Aircraft Engine and a Rigid Structure of an Attachment Strut Fixed Under a Wing of This Aircraft
Electrical Current Return Device for Avionic Equipment
Stiffener Stop with Staggered Slopes and Panel Fitted with Such a Stop
Process and Device for the Optimization of the Deflection of the Spoiler Flaps of an Aircraft in Flight
Image processing system and image processing method
Application:
11/066,565 →
Publication:
US 2005/0213174
Fuselage Spar for Aircraft and Central Sparbox Provided with Such a Spar
Simulation and Test System for at Least One Item of Equipment on an Afdx Network
Air Intake Structure for Aircraft Engine
Air Intake Structure for Aircraft Engine
Chevron-Type Primary Exhaust Nozzle for Aircraft Turbofan Engine, and Aircraft Comprising Such a Nozzle
Aircraft Comprising a Device for Detection and/or Measurement of Atmospheric Disturbances
Method and System for Characterizing Structural Damage from Observing Surface Distortions
Three-Dimensional Measurement System
Device for Reinforcement of a Hollow Structure, Especially a Box Structure for an Aircraft and a Hollow Structure Equipped with Such a Device
Production Management System and Associated Warning Process
Method of Optimizing an Electrical Cabling
Method for Ensuring the Safety of an Aircraft Flying Horizontally at Low Speed
Method and Device for Controlling and Braking an Aircraft Running on the Ground
Noise reduction assembly for aircraft turbojet
Application:
11/102,713 →
Publication:
US 2005/0252195
Longitudinal Piloting System for a Taxiing Aircraft
Throttle Lever for Controlling the Speed of at Least One Aircraft Engine
Method and Device for Aiding the Landing of an Aircraft on a Runway
Aerodynamic Airflow Deflector for Aircraft Landing Gear
Assembly of aircraft structural parts
Application:
11/111,926 →
Publication:
US 2005/0244215
Process for Aiding the Takeoff of an Aircraft
Transition Shim Between Structure for Fastening a Wing to a Fuselage of an Aircraft, and Aircraft Having Such a Shim
Flight Control Indicator Determining the Maximum Slope for the Flight Control of an Aircraft by Terrain Following
Method and Device for Providing an Aircraft with a Flight Trajectory
Method and Device for Revising a Flight Plan of an Aircraft
Method and Device for Automatically Determining a Capture Trajectory of a Flight Trajectory for an Aircraft, as Well as a Procedure and System for Automatic Guidance of an Aircraft
Cross-Connecting by Permutations Using Configurable Printed Circuits
Device for the protection against and detection of impacts on the edges of a layered composite structure
Application:
11/120,931 →
Publication:
US 2006/0234007
Flight Control Indicator for an Aircraft
Method and Device for Ensuring the Safety of a Low-Altitude Flight of an Aircraft
Method and Device for Ensuring the Safety of Low-Altitude Flight of an Aircraft
Method and Device for Automatic Guidance of an Aircraft, for a Flight at Least in Part at Low Altitude
Method and Device for Guiding an Aircraft for Aiding Parachute Drops
Method to Determine and Guide Aircraft Approach Trajectory
Method and Device for Determining a Safe Altitude for an Aircraft
Flight Control Indicator Displaying the Aircraft's Thrust Information
Method and Device for Ensuring the Safety of a Low-Altitude Flight of an Aircraft
Method and Device for Constructing a Low Altitude Flight Trajectory Intended to Be Followed by an Aircraft
Push Button Control Device
Control System for Airbrakes of an Aircraft
Device for Extinguishing Fire by Injection of a Gas Generated by the Combustion of a Pyrotechnic Block
Drilling Device and Drilling Method Used with Such a Device
Jet Engine Nacelle for a Supersonic Aircraft
Aircraft Propulsion System Comprising Four Engines with Pusher Propellers
Floor for Aircraft
Cockpit Floor for Aircraft
Method and Device for Detecting an Overstepping of Design Loads of the Fin of an Aircraft
Floor for Aircraft
System for Aiding the Piloting of an Aircraft During the Approach to a Runway with a View to a Landing
Method and Device for Detecting an Overstepping of Design Loads of the Tailplane of an Aircraft
Process for Making a Composite Material Assembly and Aircraft Wing and Stabilizing Element Obtained by This Process
Aircraft Provided with a Belly Fairing, and Corresponding Belly Fairing
Device and Method for Fastening an Aircraft Radome
Door for Aircraft, and Aircraft Provided with Such a Door
Multi-Engined Aircraft with Lowering Shaft
Procedure and Device for Improving the Maneuverability of an Aircraft During the Approach to Landing and Flare-Out Phases
Cage for Electrical Connection Nut
Device for Joining Composite Structure Elements with Metallic Structure Elements
Process for the production of composite tubing particularly for air conditioning and tubing thus obtained
Application:
11/266,349 →
Publication:
US 2006/0051545
Navigation System for an Aircraft and Associated Command Process
Flight Management Process for an Aircraft
Fixed Frequency Electrical Generation System with Induction Coupler and Use Thereof in an Aircraft
Long-Haul Airplane
Method and System for Aiding the Piloting of an Aircraft, During a Maneuver Bringing About an Increase in the Attitude of the Aircraft
Method and Device for Assisting the Lateral Control of an Aircraft Running on a Runway
Method and a Device for Assisting the Piloting of an Aircraft During an Approach Phase
Electrical Emergency Source Device Located on an Aircraft
Cellulose Ester Film, Polarizing Plate and Liquid Crystal Display
Method and device for interception of data transiting on a link in an Ethernet network
Application:
11/446,248 →
Publication:
US 2009/0028227
Engine Assembly for Aircraft Comprising an Engine and a Mounting Device for Such an Engine
Diagnostic Tool for Repairing Aircraft and Method of Using Such a Tool
Turbojet Engine for Aircraft, Propulsion Unit Comprising Such a Turbojet Engine and Aircraft Comprising Such a Propulsion Unit
System for Displaying on a First Moving Object a Position Indication Dependent on a Position of a Second Moving Object
Heat Exchanger, Propulsion Unit, and Aircraft Comprising Such a Propulsion Unit
Device and Method for Controlling the State of an Energy Accumulator
Method for the Automatic Sequencing of the Specifications of a Computer, Especially for Aircraft
Apparatus for Testing a Fuselage Structure Having a Longitudinal and Circumferential Curvature
Apparatus for Testing a Fuselage Structure Having a Longitudinal and Circumferential Curvature
Assembly for an Aircraft Including a Wing Element and a Suspension Pylon
Engine Suspension Pylon for Aircraft
Method of Imaging Using Topologic Energy Calculation
Articulated Rod
Engine Assembly for Aircraft
Reconfigurable Voltage Inverter with Tolerance to Failures
Method for Detecting an Error in Input of One of the Takeoff Parameters into a Flight Management System
Device for Securing an Insert in a Structure
Method for Checking Takeoff or Landing Parameters, and Associated Device
System for Measurement of Projected Turbulence Downwind of an Aircraft
Aircraft Engine Unit
Tool for Crimping a Contact Onto a Wire
Engine Assembly for Aircraft
Aircraft Engine Assembly
Aircraft Standby Display Device
Electric Flight Control System for Aircraft Elevators
Display System for Aircraft
Device for Protection Against Icing for Aircraft Engines and Related De-Icing Method
Device for Connecting in Flight an Aircraft to a Refuelling Device of a Tanker Aeroplane
Tool for Assisting in Cutting the Conductors of an Electrical Cable to a Precise Length
Method and Device for Measuring the Orientation of an Aircraft Nose Landing Gear
Method and Device for Detecting Electric Arc Phenomenon on at Least One Electric Cable
Avoidance Method and System for an Aircraft
Method for Displaying Roll-Down Messages on an Aircraft Display, and a Device Employing the Said Method
Method and Device for Detecting Oscillatory Failures in a Position Servocontrol Subsystem of an Aircraft Control Surface
Process for Continuous Consolidation for Obtaining a Stratified Material and Device for Its Implementation
Method for Ensuring the Safety of an Aircraft Flying Horizontally at Low Speed
Rear Suspension for an Aircraft Engine with Shackle in Waiting and Spring for Such a Hinge Pin in Waiting
Process and Device for Regulating the Luminous Intensity of Indicator Lights of a Piece of Monitoring and Control Equipment in an Airplane Cockpit
System, Method and Computer Program Product for Managing and Tracking Technical Events Associated with Production of a Product
Turbojet Pylon for Aircraft
Multi-Engine Aircraft
Method and Device for Assisting in the Piloting of an Aircraft in Free Flight
Method and Device for Assisting in the Piloting of an Aircraft
Method and Device to Assist in the Piloting of an Aircraft
Device for Localizing Acoustic Sources and Measuring Their Intensities
System for Maneuvering an Aircraft Landing Gear and Aircraft Comprising Same
Vertical Tail Unit for Aircraft and Aircraft Equipped with Same
Device for Constructing and Securing a Low Altitude Flight Plan Path Intended to Be Followed by an Aircraft
Device for Supplying Electricity and Air to an Airplane on the Ground
Process for Conducting Adherence Tests for a Coating on a Substrate
Generator of a.C. Signals, Such as Reference Signals, and Aircraft Equipped with Such a Generator
Method and Device for Assisting a Pilot of a Follower Aircraft During a Patrol Flight
Device for Determining a Flight Trajectory of a Follower Aircraft During a Patrol Flight, as Well as a System for Aiding a Patrol Flight Comprising Such a Device
Device for Determining a Maximum Lateral Separation of a Follower Craft with Respect to a Lead Craft
Method and Device for Assisting in the Piloting of an Aircraft
Method and Device for Assisting in the Piloting of an Aircraft
Device for Aiding the Guidance of a Follower Aircraft Forming Part of a Patrol, as Well as a System for Aiding a Patrol Flight Comprising Such a Device
Method and Device for Determining the Lateral Path of a Moving Body, in Particular of an Aircraft
Tool for Assisting in the Design of an Aircraft Flight Deck Compatible with a Night Vision System
Method, System and Computer Program Product for the Optimization of Power System Architectures at the Aircraft Level During Pre-Design
Hydraulic Distributor for Airplane Landing Gear
System and Method for Supplying Power to User Systems Onboard an Aircraft
Power System Comprising Several Synchronous Machines Synchronously Self-Controlled by a Converter and Control Method for Such a System
Aircraft with Reduced Environmental Impact
Method and Device for Determining the Air Turbulence Likely to Be Encountered by an Aircraft
Radio-Frequency Communication System for Aircraft
Method and Device for Enhancing the Braking Efficiency of an Aircraft During the Ground Run Thereof
Device for Supplying Pasty Material
Application:
11/718,544 →
Publication:
US 2009/0217868
Aircraft Connector Assembly
Application:
11/718,836 →
Publication:
US 2011/0117773
Structural Frame for an Aircraft Fuselage
Electrical Cabinet with Electrical Connection to Its Door
Aircraft Terrain Avoidance and Alarm Method and Device
Detection of Errors in Data Relating to the Actuation of a Vehicle Member
Method for Fixing an Engine Strut to an Airplane Wing
Device for Increasing the Effectiveness of the Pressurizing Gas in an Extinguisher Bottle
Method for Improving Roll Steering of an Aircraft and Aircraft Using Same
Device for Issuing Authorization to Act on the Operating Conditions of an Aircraft Engine and Engine Control System Comprising Same
System for Detecting, Quantifying and/or Locating Water in Aircraft Sandwich Structures and Methods for Using This System
Ventilating Air Intake Arrangement
Ventilating Air Intake Arrangement with Mobile Closing Device
Method and Device for Inputting Digital Values
Method and Device for Audible Warning When an Aircraft Autopilot Is Deactivated
Method and Device for Piloting a Pitching Aircraft
Method and Device for Reducing the Wake Vortices of an Aircraft in the Approach/Landing Phase
Method and Device of Assisting in the Piloting of an Aircraft in a Search and Rescue Mission
Application:
11/738,600 →
Publication:
US 2008/0039985
Flight Deck Layout for Aircraft
Damage-Tolerant Attachment System for an Aircraft Engine
Method and Device for Consolidation by Software Synchronisation in Flight Control Computers
Computerised Flight Manual and Method for Dynamic Control of Such a Flight Manual
Ejection Device, Ejectable Hatch and Aircraft Having at Least One Ejectable Hatch
System for Measurement and Detection of Parameters and Anomalies
Method, System, and Computer Program Product for a Maintenance Optimization Model
Device for Monitoring Aircraft Control Information
Method and Device for Assisting in the Navigation of an Airplane on the Ground at an Airport
Method and Device for Assisting in the Navigation of an Airplane on the Ground at an Airport
Mobile Airfoil Device for an Aircraft Wing
Application:
11/760,934 →
Publication:
US 2007/0284483
Device and Method for the Surveillance of an Aircraft
System for the Spraying of Spray Liquid for Aircraft Windshield, and Cockpit Provided with Such a Spraying System
System for the Spraying of Spray Liquid for Aircraft Windshield, and Cockpit Provided with Such a Spraying System
Hinge Device of a Nacelle Cowling of an Aircraft Engine on a Supporting Structure
Stiff Panel Having Composite Stiffeners with Reduced Shock Sensitivity
Device to Aid the Positioning of a Pilot in an Aircraft
Turbojet for Aircraft
Mounting Device for an Aircraft Engine Comprising Two Thrust Recovery Rods with a Double Rear Mechanical Connection
Flight Control System for Aircraft and Test for Testing Such a Flight Control System
Method and Device for Detecting Air Turbulence in the Environment of an Aircraft
Method and Device for Predicting the Stopping Position of an Aircraft Whilst Landing
Airplane Protected Against Projections of Tire Debris
Avionic System and Architecture with Integrated Power Management
Process and Device for Monitoring the Illumination of Lamp Bulbs
Display System for Aircraft
Flight Command and Direction on Ground Command System for an Aircraft
Application:
11/775,250 →
Publication:
US 2008/0011905
Vortex Generator at Hot Gas Output
Aircraft for Transport of Passengers
Application:
11/775,882 →
Publication:
US 2008/0179457
Aircraft Cabin Layout Having Berths in the Upper Portion of the Cabin
Rest Unit for an Aircraft
Method, System, and Computer Program Product for Calculating the Residual Stress Equilibrium of Two Concentric Cylinders Coldworked by a Loading-Unloading Expansion Process
Aircraft Engine Mounting Device Attachment Arrangement
Method for Optimizing the Mass of a Composite Panel
Super-Transporter Aircraft
Composite Internal Beam for Reinforcing the Structure of an Aircraft
Hinged Device for Doors of an Aircraft Nacelle and Nacelle Equipped with Said Hinged Device
Aircraft cabin configuration
Application:
11/798,826 →
Publication:
US 2007/0278346
Device for Articulating a Door of a Nacelle of an Aircraft and Nacelle Provided with Said Articulation Device
Test Flight on-Board Processing System and Method
Method and Device for Detecting, on the Ground, the Obstruction of a Pressure Tap of a Static Pressure Sensor of an Aircraft
Probe for Measuring the Thickness of Frost Accretion on a Surface
Engine Attachment for an Assembly System Mounted Between an Attachment Strut and an Aircraft Engine.
Method and Device for Displaying a Flight Plan of an Aircraft
Method and Device for Aiding the Management of Successive Flights of an Aircraft
Method and Device for Determining a Decision Height During an Autonomous Approach of an Aircraft
Device for Aircraft Dialogue
Cable Support for Aeronautic Construction
Application:
11/837,705 →
Publication:
US 2008/0156931
Attachment System for Cables and Support for Cables Used in Aeronautic Construction
Method for Monitoring the Integrity of an Aircraft Position Computed on Board
Method for Producing an Aircraft with Reduced Envrionmental Impact and the Aircraft Thus Obtained
Windscreen Frame and a Method of Production for a Windscreen Frame
Splice Plate for Stringers and Orbital Joining Device
Device for Wind Estimation and Method Associated Therewith
System and Process for Direct Current Power Supply of an Electrical Network on Board an Aircraft
Device for Controlling the Switching of a User Interface
Device for Supplying Electrical Power to an Aircraft and for Electrically Starting a Jet Engine on Board an Aircraft
Device for the Integration of a Laptop Computer into an Aircraft
Power Supply System and Method on Board an Aircraft
Method and Device for Aiding the Guidance of an Aircraft Along a Flight Trajectory
Aircraft Comprising a Landing Gear Compartment Permitting Better Integration of the Landing Gear
Terrain Avoidance Method and System for an Aircraft
Hollow Structural Rod and Production Method Thereof
Device and method for non-symmetrical mixed carbon-metal assembly
Application:
11/909,334 →
Publication:
US 2009/0065644
Method and Device for Measuring Air Turbulence in the Surroundings of an Aircraft
Method and Device for Assisting the Ground Navigation of an Aeroplane in an Airport
Method and Device for Displaying Part of an Airport on a Viewing Screen
System for Assisting the Ground Navigation of an Aeroplane in an Airport
Low-Noise Aircraft, Particularly at Take-Off and Landing
Method and Device for Assisting an Aircraft Flight Control During Landing Approach
Assisted Take-Off Method for Aircraft
Turboshaft Engine That Reduces Rear Noise Emissions
Engine Mount for an Aircraft, to Be Placed Between an Engine and an Engine Mounting Structure
Device for Slinging a Piece with Stress Compensation and Hoisting System Containing This Device
Aircraft Engine Unit
Application:
11/914,327 →
Publication:
US 2008/0210811
Engine Mounting Structure for an Aircraft
System for Deicing the Leading Edge of a Nose Inlet Cowl Turbine Engine
Ladder System, Especially for Vehicles
Aircraft Jet Engine Pylon Suspension Attachment
Module for Testing Electromagnetic Compatibility of a High-Speed Ethernet Interface Onboard an Aircraft
Expansion Tool for Cold Expansion of Holes
Application:
11/915,960 →
Publication:
US 2009/0113979
System for Opening and Closing the Flap of a Casing for the Landing Gear of an Aircraft
Engine Mounting Structure for an Aircraft
Electrical Cable Provided with External Marking and Method of Crimping the Barrel of a Contact Onto an Electrical Cable Provided with External Marking
Method and Device for Driving an Aircraft During the Ground Run Thereof
Method and System for Assisting Flight Control of a Low-Flying Aircraft
Communication Flap and Aircraft Provided with One Such Flap
Application:
11/917,791 →
Publication:
US 2009/0084039
Sol for sol-gel process coating of a surface and coating method by sol-gel process using same
Guidance System for an Aircraft
Non-Destructive Ultrasound Inspection Method and Measurement Probe for Implementing the Method
Method and Device for Estimating the Forces Exerted on a Control Surface of an Aircraft
Device for Guiding an Aircraft Along a Flight Trajectory
Method and Device for Aiding the Piloting of an Airplane During an Approach Phase
Active Pitch Control Method and Device for an Aircraft
Aircraft Viewing System
Application:
11/940,675 →
Publication:
US 2010/0289671
Aircraft Control System Containing an Aeronautical Data Base
Aircraft with Jet Engines Arranged at the Rear
Method and Device for Active Control of the Roll of an Aircraft
Automatic Take-Off Method and Device for an Airplane
Aircraft Horizontal Stabilizer
Front Aircraft Part Comprising a Flat Partition Between a Pressurised Zone and a Non-Pressurised Zone Housing Landing Gear
Secured Cockpit for an Aircraft
Application:
11/965,142 →
Publication:
US 2008/0164377
Apparatus for Interconnecting a Pilot Station to at Least One Other Aircraft Zone, Cockpit and Aircraft Equipped with Such an Apparatus
Method for Predicting the Operational Reliability of an Aircraft System
Air Discharge Device for an Aircraft
Method of Optimizing Stiffened Panels Under Stress
Data Viewing System for an Aircraft
System for Opening and Closing a Landing-Gear Compartment for an Aircraft
Double Crimping Tool
Displaying Method and Device for an Aircraft Following a Flight Plan
System for Defrosting the Leading Edge Sheath of an Air Inlet Hood for a Turboengine
Method for Detecting a Fuel Leakage in an Aircraft Engine and System for Carrying Out Said Method
Systeme D'anti Givrage Et De Degivrage De Nacelle De Moteur D'aeronef a Tapis Resistif
Application:
11/993,693 →
Publication:
US 2010/0199629
Compact Steering Device for the Landing Gear of an Aircraft
Aircraft Pod and Aircraft Equipped with at Least One Such Pod
Method and Device for Lightening Loads on the Wing System of an Aircraft in Roll Motion
Device for Fixing a Seat Rail on a Floor, and Aircraft Equipped with Such a Fixing Device
Device For Assisting a Vertical Guidance Approach For Aircraft
Application:
11/994,979 →
Publication:
US 2008/0172149
Method and Device for Determining the Group Position of a Mobile Object, in Particular an Aircraft on an Airport
Device for Assisting Ground Navigation of an Aircraft on an Airport
Assembly for Aircraft Comprising a Wing System Element as Well as an Attachment Mast
Airport Viewing System for an Aircraft
Propulsion Unit for Aircraft with Heat Exchanger Having Front Inlet Faces for Cooling Air Flow and Hot Air Flow
Method and Device for Simulating Bending of a Tube
Application:
11/996,137 →
Publication:
US 2008/0228454
Monolithic Self-Stiffened Panels
Method and Device for Detecting a Risk of Collison of an Aircraft with the Surrounding Terrain
Aircraft Data Transmission System for Transmitting Data Between an Aircraft and a Transmission Station Located Outside Thereof
Method and Device for Flying an Aircraft According to at Least One Flying Line
Heat exchanger unit for an aircraft
Control Device for Locking and Unlocking and Aircraft Door and Aircraft Door That Integrates Such a Device
Method for measuring a shape anomaly on an aircraft structural panel and system therefor
Application:
11/997,072 →
Publication:
US 2009/0220143
Primary Engine Strut Structure of an Aircraft
Application:
11/997,834 →
Publication:
US 2009/0294579
System and Method for Supplying Power for Actuators on Board an Aircraft
Aircraft Air Conditioning System
Device for Controlling an Electromechanical Actuator
Method and Device for Determining a Maximum Stabilization Height in the Final Flight Phase of an Airplane
Device and Method for Assisting in the Management of an Engine Failure on an Aircraft
Device and Method for Assisting in the Management of an Engine Failure on an Aircraft
Authentication Method for an Electronic Document and Verification Method of a Document Thus Authenticated
Self-Restoring on-Board Information System
Method and Device for Dynamically Alleviating Loads Generated on an Airplane
Method and System for the Entry of Flight Data for an Aircraft, Transmitted Between a Crew on Board the Aircraft and Ground Staff
Device and Method for Detecting Lightning Strikes on a Structure Made of Electrically Insulating Material
Aircraft Floor and Fuselage Supplied with Said Floor
Container for Air Freight Transport and Fuselage of an Aircraft for Freight Transport
Aircraft Including an Air Conditioning System
Mast for an Aircraft Nacelle Incorporating Means for Limiting the Appearance of Vibrations, in Particular in Certain Flight Regimes, at a High Mach Number and Low Lift
Application:
12/043,157 →
Publication:
US 2008/0217468
Method and Device to Assist in the Guidance of an Airplane
Group of Flight Simulators and Associated Structure
Method and Device to Assist in the Piloting of an Aircraft in a Landing Phase
Method and Device for Limiting the Roll Command of an Aircraft as a Function of a Thrust Asymmetry
Method of Data Integrity Control in an Afdx Network
Support Device to Mount Against the Rear of the Back of a Cockpit Seat
Method and Device for Modifying the Sound Volume of an Audio Alarm Signal Onboard an Aircraft
Method and Device for Determining an Aircraft Landing Delay Margin
Aircraft That Comprises a Structure That Ensures the Structural and Electrical Functions
System for Connecting a Crossbar to an Aircraft Engine Pylon
Engine Assembly for Aircraft Comprising an Engine as Well as a Device for Locking Said Engine
Optical Communication Bus Network for Avionic Equipment
Nacelle Cowling for Turbojet and Nacelle Comprising at Least One Such Cowling
Engine Mounting Structure Interposed Between an Aircraft Wing System and Said Engine
Method for Attenuating the Noise of a Turbofan
Energy Protecting Device for Aircraft
Method for Through Repair of a Composite Structure Comprising Three Skins and Two Core Layers
Application:
12/066,668 →
Publication:
US 2008/0226818
Method for Repairing a Composite Structural Outer Skin
Application:
12/066,677 →
Publication:
US 2008/0283172
Boring Device
Method for Mounting an Aircraft Engine on a Rigid Structure of a Strut for Locking the Engine
A Mounting Assembly for Securing an Engine to an Aircraft Wing
Strut for Locking the Engine of an Aircraft
Two-Shackle Aircraft Engine Attachment
Engine Assembly for an Aircraft Comprising an Engine as Well as an Engine Mounting Structure for Such an Engine
System for Deicing and/or Defogging an Aircraft Surface, Method for Controlling Same, and Aircraft Equipped with Same
System for Monitoring Anemobaroclinometric Parameters for Aircraft
Turbojet for Aircraft, Aircraft Equipped with Such a Turbojet, and Method for Mounting Such a Turbojet on an Aircraft
Method and Device for Carrying Out at Least One Flight Testing on an Aircraft and the Use Thereof
Device for Controlling a Vortex Trail Generated by the Oblong Element of an Aircraft Bearing Surface
Turbofan Provided with a Pre-Cooler
Rigid Framework for Aircraft Engine Mounting Structure and Engine Mounting Structure Comprising Same
Device for Fastening a Turbojet Engine to an Aircraft Fixing Strut
Traction Pad for Device Testing Adhesion of a Coating on a Substrate
Device for Controlling Equipment
Application:
12/088,307 →
Publication:
US 2009/0018710
Floor Panel And Installation For Fixing Layout Elements Comprising Such Panels
Device for Fixing a Lightweight Panel Onto a Support
Engine Assembly for Aircraft
Turbojet Engine Mounting Structure for Aircraft
Nut System and Aircraft Engine Mounting Structure Comprising Same
Display System for an Aircraft
Method and Device for Attenuating on an Aircraft the Effects of a Vertical Turbulence
Combined Device for Controlling the Power Transfer Between Two Cores of a Direct Current Network and for Powering an Alternating Current Engine.
Device for Controlling Power Transfer Between Two Cores of a Direct Current Network
Turbojet Engine with Attenuated Jet Noise
Engine Speed Control Device, a Method for Controlling Engine Speed and an Aircraft Provided Therewith
Tool for Machining Composite Material Parts
Aircraft Having a Reduced Environmental Impact
Method and System for Limiting an Aircraft Control Surface Steering Angle
Aircraft Comprising a Central Fairing That Adjusts the Pressure on the Wing Structures by Means of Local Geometric Deformations
System for Detecting and Locating Water in a Sandwich-Type Stucture for Aircrafts
Landing Gear Casing Provided with a Dissociated Structure
Aircraft Landing Gear Comprising an Operation Strut Device and Aircraft Provided Therewith
Method and Device for Assisting the Flying of an Aircraft During an Autonomous Approach
System For Piloting an Aircraft, at Least For Piloting the Aircraft During an Autonomous Approach For the Purpose of Landing
Aircraft Ventral Fairing Partition Wall and Aircraft Equipped with a Ventral Fairing
System and Method for Diagnosing Aircraft Components for Maintenance Purposes
Process and System for Modifying the Content of an Alarm Message Onboard an Aircraft
Aircraft with Reduced Environmental Impact
Process and Device for Controlling the Deformation of a Metal Part, in Particular for Redressing a Metal Part
Method for Determining an Identifier Corresponding to a Frequency Set on a Display Unit of the Cockpit and System of Implementation
Assembly of Panels of an Airplane Fuselage
Autonomous Plane Architecture for the Transport and the Replacement of Propulsion Engines
Wide Body Aircraft Architecture
Method and Device for Detecting Noise on a Guide Signal of Loc Type Received by an Aircraft
Display System for an Aircraft Cockpit
Noise Reduction Assembly for Aircraft Turbojet
Aircraft Display System
System for Selecting Data Representing an Air Parameter, Process and Computer Program Relating to the Same
Device for Aiding to Take a Decision Concerning the Ability of an Aircraft to Start a Flight
Application:
12/123,296 →
Publication:
US 2009/0326738
Method and Device for Detecting Oscillatory Failures Related to a Servocontrol Subsystem of an Aircraft Control Surface
Method and Device for Monitoring a Position Indication of an Aircraft
Landing Gear Casing Provided with a Box Structure
Method and Device for Determining the Dynamic Stability Margin of an Aircraft
System for Guiding and Piloting an Aircraft in Case of Inability of the Pilots
Procedure and Device for Improving the Maneuverability of an Aircraft During the Approach to Landing and Flare-Out Phases
Aircraft Piloting Method and Device for Picking Up a Vertical Profile of a Flight Plan
Axisymmetric Parts Equipped with Dust Removal Grooves
Method and Device for Simulating Radio Navigation Instruments
Jack System with Automatic Locking of the Piston in High Position, Especially for Aircraft
Hatch Equipped with at Least One Locking Socket Capable of Being Actuated on Each Side of the Hatch
Process and Device for Managing the Activating of a Warning Message in an Aircraft
Process and System for Managing an Interruption of a Broadcast of a Sonorous Message in an Aircraft
Method and Device for Exchanging Diagnostic Data for the Simulation of Aircraft Computer Networks
Method for Frabricating an Aircraft Fuselage in Composite Material
Device for Protecting and Guiding a Cable from a Direct-Vision Window of an Aircraft Flight Deck
Method of De-Icing the Leading Edge of an Aerodynamic Surface and Aircraft Implementing Such a Method
Dual Flow Turbine Engine Equipped with a Precooler
Dual Flow Turbine Engine Equipped with a Precooler
Method for Cutting Out a Panoply of Parts
Purge Device and Hydraulic System Comprising Such a Purge Device
Application:
12/161,672 →
Publication:
US 2010/0219289
Minimizing Dynamic Structural Loads of an Aircraft
Cockpit and Aircraft Including Such Cockpit
Electrical Control System for an Aircraft Steering Vane
Application:
12/162,465 →
Publication:
US 2009/0014595
Method and System for Predicting the Possibility of Complete Stoppage of an Aircraft on a Landing Runway
Method and System for Piloting an Aircraft
Method and Device for Detecting a Lateral Dissymmetry of an Aircraft
Method and Device for Automatically Adjusting an Image of an Aircraft Navigation Screen
Device for Aiding the Piloting of an Aircraft During an Approach Phase for the Purpose of Landing
Aircraft Having Reduced Environmental Impact
Method and Device for Controlling the Thrust of a Multi-Engine Aircraft
Retractable Aerodynamic Device Permitting the Control of the Wake Trajectory of an Aircraft Trap
Braking-Energy Equalization System
Differential Braking System
Pitch-Oscillation Limitation System Applied to an Aircraft
Aircraft Having a Reduced Acoustic Signature
Short Take-Off Aircraft
Process and Apparatus for Evaluating Operational Risks for Aiding in Vehicular Maintenance Decisions
Process and Apparatus for Annotating Electronic Map Data
Process and Apparatus for Generating Map Data in Real Time
Application:
12/191,009 →
Publication:
US 2009/0051702
System and Method for Data Transmission Between at Least One Display Screen and a Client System
Device for Generating Aerodynamic Disturbances So as to Protect the Outer Surface of an Aircraft Against Elevated Temperatures
Method and System for Synchronizing a Display Context
Method and Device for Automatically Protecting an Aircraft Against a Hard Landing
Method and System for Maneuvering an Aircraft by Shifting Its Center of Gravity
Method for Fabricating a Semiconductor Device with Self-Aligned Stressor and Extension Regions
Application:
12/194,246 →
Publication:
US 2010/0047985
Method and Device for Aiding the Piloting of an Aircraft
Device and Method for Estimating a Side-Slip Angle of an Aircraft
Aircraft Turbofan Engine
Method of locally reinforcing a composite element and reinforced aircraft wing structure central box section
Application:
12/244,847 →
Publication:
US 2009/0121082
Entity-Identity Based Security Procurement of Computer Files That Are Downloadable to an Aircraft, Method of Authentication, and Associated System and Aircraft
Method and Device for Creating an Aircraft Flight Plan
Method and Device for Updating the Position of an Aircraft
Method of Reducing the Compressibility Drag of a Wing, and Container Implementing the Method
Method and Device for Aiding the Piloting of an Aircraft to Prepare a Phase of Descent
Device for Rest Managment for Aircraft Pilot
Method and Device for Preventing Collisions on the Ground for Aircraft
Device for Managing the Waking Up Phase of an Aircraft Pilot
Method for Determining the Total Temperature of an Airflow Surrounding an Aircraft
System for Deicing an Air Inlet Cowl for a Turbine Engine
Aircraft Guidance System
Fire Detection System and Aircraft Equipped with Such a System
Image Viewing System for Passengers of an Aircraft and Aircraft Comprising Such a System
Method and Device for Detecting Attempts at Intruding on a Communication Link Between an Aircraft and a Ground Station
Methods and Devices for the Transmission and Reception of a Message to Be Exchanged Between an Aircraft and a Ground Base, and Aircraft Provided with Such Devices
Method for Characterizing the Endurance Limit of a Part from Its Surface Profile
Radiocommunication System for Aircraft
Method and Device for Piloting an Aircraft About a Piloting Axis
Aircraft Wing Arrangement Comprising an Engine Attachment Pylon Defining, in the Forward Region, a Lateral Airflow Channel
Method for Communicating Data Between Locally Networked Heterogeneous Processing Systems and Communication System Using Said Method
Method for Transmitting and Receiving Data, in Particular for Secure Exchanges Between an Aircraft and a Ground Base, Related Devices and Aircraft Equipped with Such Devices
Nut Attaching an Aircraft Windshield and Device for Attaching an Aircraft Windshield Incorporating Said Nut
Application:
12/294,429 →
Publication:
US 2009/0245968
Device and Method for Emergency Electricity Supply on Board an Aircraft
Method and Device for Piloting an Aircraft Optimizing the Control of the Ailerons in an Enhanced-Lift Configuration
Device for Detecting the State of a Switch
Method and Device for Communication on a Communication Link Between an Aircraft and a Ground Station
System and Method for Electric Power Distribution Inside an Aircraft
Aircraft Floor, Use of Said Floor and Aircraft Section Fitted with Said Floor
Safety Device for a Semiconductor Switch
Device for Attaching an Aircraft Engine
Aircraft Comprising a Device for Reducing the Induced Drag
Secure File Transfer Method
Process for Repairing a Damaged Area of an Aircraft Fuselage
Device for Receiving Messages, in Particular Within the Framework of Secure Data Exchanges, Associated Aircraft and Method
Device for Non-Destructive Testing of a Component by Analyzing Generated Radiation
Device for Non-Destructive Testing of a Component by Analyzing Distibution of a Leakage Magnetic Field
Device for Non-Destructive Testing of a Structure by Vibratory Analysis
Aircraft Pressurized Floor
Method of Routing Virtual Links in a Frame-Switching Network
Method for Routing Virtual Links in a Frame-Switching Network with Guaranteed Determinism
Landing Assistance Device and Method for Aircraft
Method for Piloting an Aircraft in Approach Phase
Method for Instantaneously Determining Rates of Distortion of Signals on an Ac Electrical Network, and Associated Device
Aircraft Engine Mount Structure Comprising Two Thrust Links with Transverse Fitting
Aircraft Propulsion Unit That Comprises an Exhaust Pipe with a Scalloped Trailing Edge
Application:
12/305,558 →
Publication:
US 2009/0277181
Fairing for a Pylon via Which a Turbine Engine Is Suspended from a Wing of an Aircraft
Turboreactor for Aircraft
Device for Autonomous Movement of an Aircraft on the Ground
Application:
12/306,669 →
Publication:
US 2009/0294577
Aircraft Engine Assembly for an Comprising a Fan Cowl-Supporting Cradle Mounted on Two Separate Elements
Aircraft Engine Assembly Comprising a Junction Aerodynamic Fairing Mounted on Two Separate Elements
Method of Analyzing an Assembly of Parts with Respect to a Predetermined Design Criterion
Process for Reversing the Thrust Produced by a Propulsion Unit of an Aircraft, Device for Its Implementation, Nacelle Equipped with Said Device
Application:
12/307,483 →
Publication:
US 2009/0199536
Turbine Engine for Aircraft
Aircraft Turbine Engine
Application:
12/307,881 →
Publication:
US 2010/0000227
Turbine Engine for Aircraft
Aircraft Tail Cone
Turbojet Nacelle and Method for Controlling Separation in a Turbojet Nacelle
Method and Device for Generating a Speed for an Aircraft During a Taxiing
Method and Device for Generating a Taxiing Trajectory for an Aircraft
Method and Device Concerning the Taxiing of an Aircraft, Which Is Automatic at Least in Part
Method and Device for Generating a Yaw Speed Order for an Aircraft During a Taxiing
Method and Device for Generating a Speed Profile for an Aircraft During a Taxiing
Lightning Protection System and an Aircraft Having Such a System
Method and Device for Detecting Oscillatory Failures in a Position Servocontrol Subsystem of an Aircraft Control Surface
Casing and Front Landing Gear Assembly for an Aircraft
Method and Device for Automatically Guiding an Aircraft During a Spacing Flight with a Landing
Hydraulic System Protected from External Impacts
Methods and Devices for Improving the Reliability of Communication Between an Aircraft and a Remote System
Secure Command Method and Device for Remote Maintenance Terminal
Switching Device Adapted to Switch an Aircraft Wireless Network from a Maintenance Configuration to a Commercial Configuration and Vice-Versa
Process and Device for Diagnostic and Maintenance Operations of Aircraft
Method and Device for Reducing on an Aircraft Lateral Effects of a Turbulence
Method and Device for Reducing on an Aircraft the Effects of a Vertical Turbulence
Storage Compartment for the Nose Gear of an Aircraft
Device for Detecting and Eliminating the Presence of a Layer of Ice or Liquid
Heat Flow Device
Application:
12/373,975 →
Publication:
US 2009/0283251
Heat Flow Device
Application:
12/373,988 →
Publication:
US 2010/0012311
Sensor Simulation System
Method and Devices for Aiding in Determining the Feasibility of an Electronic Assembly
Aircraft Doorway
Aircraft Conduit
Structural Element of an Aircraft
Application:
12/376,143 →
Publication:
US 2009/0314899
Support to Fix Electrical Cables on a Structure
Application:
12/376,639 →
Publication:
US 2010/0238642
Method and Device for Detecting an Environning Aircraft
Beam Mounted Rear Propulsion System for an Aircraft and Aircraft with Such System
Rear Propulsion System with Lateral Air Inlets for an Aircraft with Such System
Aircraft Comprising a Window Panel
Method and Device for Automatically Controlling an Emergency Descent of an Aircraft
Assembling Panels Edge to Edge
Airplane Engine Pylon Comprising at Least One Protruding Element to Generate a Vortex of the Airflow
Braking Process for an Airplane
Application:
12/409,751 →
Publication:
US 2010/0076623
Process for High-Energy Density Beam Welding
Process for the Production of a Stiffener That Is Scooped Out in the Shape of an Omega and Core for the Production of a Stiffener That Is Scooped Out in the Shape of an Omega
Application:
12/413,743 →
Publication:
US 2009/0246531
Airplane with Pitch and Yaw Command by Propulsion System
Aerodynamic Surface Assembly for Aircraft
Method and Device for an Aircraft Buffet Reduction
Device with Plane Jets for Reducing the Noise Generated by an Aircraft Engine
Advanced Feed Device for a Superplastic Press Forming System
Method and Device for Guiding an Aircraft
Method and Device for Guiding an Aircraft
Pylon for Suspending a Turboengine
Method and Device for Aiding the Airport Navigation
Unit Comprised of a Glidepath Aerial and a Support Member
Device and Method for Determining a Runway State, Aircraft Comprising Such a Device and Piloting Assistance System Using That Runway State
Method and Device for Correcting the Lateral Dissymmetry of an Aircraft
Process and Apparatus for Aiding in the Conception of Texts for a Pilot or a Conductor
Device to Handle and Lock a Cover of an Aircraft Nacelle
Panel Assembly and Method for Mounting a Panel Assembly
Application:
12/438,174 →
Publication:
US 2010/0077690
A Method of Forming a Panel Assembly of a Ventral Fairing of an Aircraft
Self-Stabilised Stiffener Enabling Element Recovery
Process for Manufacturing a Panel Made of a Thermoplastic Composite
Device That Makes It Possible to Improve the Effectiveness of the Acoustic Treatments in a Pipe of an Aircraft Power Plant
Machining Means for Ceiling Fixed Parts
Fixed Support for Parts in Machine Tools
Application:
12/441,190 →
Publication:
US 2010/0044941
Locking and Unlocking System for the Cockpit Door of an Aircraft and Door with Such a System
Jet Engine Nacelle for an Aircraft and Aircraft Comprising Such a Nacelle
Device and Method for Supplying Electrical Power to at Least One Induction Machine on Board an Aircraft
Aircraft Fuselage Made from Longitudinal Panels and Method of Producing Such a Fuselage
Application:
12/444,972 →
Publication:
US 2010/0032523
Method and Devices for Projecting Two-Dimensional Patterns Onto Complex Surfaces of Three-Dimensional Objects
System for Electrical Generation, Conversion, Distribution, and Starting on Board an Aircraft
A Continuous-Angle Weaving System
Method and Aids for Modelling 3D Objects
Method and Aids for Relative Positioning of Objects During a Design Phase
Process for Transmitting Data Between at Least One Cockpit Display Screen and at Least One Remote Client System
Thrust Force Take-Up Device for an Aircraft Engine Pylon Engine Mounting Structure, Comprising Lateral Link Rods with Integral Spreader Bar Stops
Piloting Method and Device Avoiding the Pilot Induced Oscillations
Device for Precharging a Voltage Converter, and an Assembly and Aircraft Including Such a Device
Airplane with Rear Engines
Computer Maintenance System for an Aircraft with Remote Terminal
Method and System for Automatically Managing a Convoy of Aircraft During a Taxiing
Method and Device for Generating a Taxiing Speed for an Aircraft of a Convoy
Method and Device for Fault Auto-Detection in an on-Board System
Fluid Ejection Device
Application:
12/483,402 →
Publication:
US 2010/0288516
Device for Counting Oscillations of an Oscillating Temporal Signal
Hybrid Method for Estimating the Ground Effect on an Aircraft
Aircraft Nacelle Which Includes Thrust Reverser System and Aircraft Incorporating at Least One Such Nacelle
Nacelle for Aircraft Comprising Means of Reversing Thrust and Aircraft Comprising at Least One Such Nacelle
Device for interaction with a display system, in particular for an avionics display system
Method and Device for the Detection of a Thrust Dissymmetry of an Aircraft During a Braking
Method and Device to Assist in the Driving of a Vehicle, in Particular of an Aircraft, for the Avoidance of Obstacles
Aircraft with retracted front landing gear
Fuselage Arrangement for Airplane
Airplane with a Modifiable Surface of Vertical Empannage
On-Board Aeronautical System with Dynamic Reconfiguration, Associated Method and Aircraft Carrying Such a System
Sail Wing Aircraft Which Includes an Engine Mounted on a Pylon
Aircraft Leading Edge
Acoustic Coating for an Aircraft Incorporating a Frost Treatment System by Joule Effect
Aircraft with Rear Annular Tail
Device and Method for Monitoring the Particle Contamination in Flowing Hydraulic Fluids
Aircraft Fuselage
Section of Aircraft Fuselage and Aircraft Including One Such Section
Aircraft Cabin Window Assembly Method
Nacelle with a Displacement Device for Aircraft Jet Engine and Aircraft Including Such Nacelle
Acoustic Treatment Device for Turbine and Combustion Noises
Device and Method for Measuring the Flow Speed and Direction of a Gaseous Fluid
Method for Monitoring Authorized and Unauthorized Persons Within a Security Perimeter Around an Apparatus
Aircraft Nacelle That Incorporates a Device for Reversing Thrust
Tuneable Antenna for Electromagnetic Compatibility Tests
Process for Assembling Two Assemblies, Such as Aircraft Fuselage Assemblies
Coating for Acoustic Treatment Integrating the Function of Frost Treatment with Hot Air
Acoustic Panel
Electronic Card and Aircraft Including Same
Rear Lower Aerodynamic Fairing for the Attachment Device of an Aircraft Engine
Energy Storage Aerodynamic Braking Device and Method
Aircraft Landing Gear Provided with at Least One Noise Reducing Means
Device for Balancing the Power Supplied by Power Generators
Process for Verifying the Coherence Between Aircraft Take-Off Parameters and an Available Runway Length
Method and Device for Assisting in the Preparation and Management of Missions in an Aircraft
Interactive Device for Control of Utility Systems in an Aircraft
Method and Device for Assisting in the Control of the on-Board Systems in a Aircraft
Hybrid Acars Communication System
Method and Device for Assisting in the Diagnostic and in the Dispatch Decision of an Aircraft
Method and Device for Sharing Data Between on-Board Systems in an Aircraft
Cooling System for Aircraft Electric or Electronic Devices
Application:
12/540,505 →
Publication:
US 2010/0071881
Cooling System for Aircraft Electric or Electronic Devices
Application:
12/540,512 →
Publication:
US 2010/0084118
Window, in Particular a Window for an Aircraft Cabin
Method of Regulating a Harmonization Compensation Between Video Sensor and Head Up Display Device, and Corresponding Devices
Aircraft with Its Fuselage Suspended Under the Wing
Method and Device for Encapsulating Applications in a Computer System for an Aircraft
Support Method and Device for Assisting in the Preparation and Management of Missions in Aircraft
Automatic Configuration Method for Control Keys and a Control Device for Display Means, in Particular for an Aircraft
Engine Pylon for the Suspension of a Turbo Engine Under an Aircraft Wing
Nacelle for Double Flow Engine
Method of Communicating a Digital Signature to Certify a Transmission, Associated System and Aircraft
Activation-Deactivation Process on the Ground for an Aircraft Traffic Alert and Collision Avoidance System
Application:
12/557,910 →
Publication:
US 2010/0114491
Method and Device for Aiding the Piloting of an Aircraft During a Landing
Fastener Assembly for Transport Vehicle
Method and Device for Limiting the Number of Alarms Generated by an Anti-Collision System on Board an Airplane
Method and Device for Preventing Useless Alarms Generated by an Anti-Collision System on Board an Airplane
Primary Structure for Aircraft of Composite Material with Improved Crash Resistance and Associated Energy-Absorbing Structural Element
Methods and Devices for Managing Maintenance Information in an Aircraft
System for Managing the Heat Fluxes of an Aircraft
Manufacturing Process for a Section of Aircraft Fuselage in Composite Material
Central Section of Aircraft with Ventral or Belly Fairing Capable of Movement
Section of Aircraft Fuselage in Composite Material with a Constant Internal Profile
Device for the Manufacturing of a Piece of Composite Materiel with Complex Shape
Method and Device for Processing Configuration Reports
Application:
12/572,484 →
Publication:
US 2010/0100875
Method and Device for the Energy Protection of an Aircraft
Method and System for Meteorological Monitoring Aboard an Aircraft
Method of Operating an Item of on-Board Equipment, Associated Equipment and Aircraft Comprising Such Equipment
Floor Made Out of Composite Material and Process for Manufacturing Such a Floor
System for Fixing
Airplane with Flat Rear Fuselage Said Queue-De-Morue Empennage
Method and Device of Terrain Avoidance for an Aircraft
Method for Improving the Performance of an Aircraft
Device for Deflection and Retention of Aircraft Engine Debris
Application:
12/594,055 →
Publication:
US 2010/0101205
Method and Device for Managing Communication Channels for Data Exchange from an Aircraft
Device for Attaching an Aircraft Engine and Aircraft Comprising at Least One Such Device
Process for the Production of an Acoustically Resistive Structure, the Acoustically Resistive Structure Thus Obtained, and Coating Using Such a Structure
Aircraft Hold and Aircraft Equipped with Such a Hold
Device for Attaching a Lift Member to the Fuselage of an Aircraft
Method for Making a Structural Part of a Composite Material Having a Calibrated Thickness and Structural Part Thus Obtained
Aircraft Navigation Aid Device
Aircraft Engine Attachment Pylon Having a Rear Engine Attachment Provided with a Self-Locking Nut
Attachment Pylon for Aircraft Having a Rear Engine Attachment Beam Offset from the Caisson
Device for Attaching an Aircraft Engine and Aircraft Comprising at Least One Such Device
Pylon Caisson Attachment on a Wing, Gripping a Lateral Panel of the Caisson
Method and System for Starting a Turboshaft Engine by Cold Weather
Air Intake Arrangement for a Vehicle, in Particular an Aircraft
Method and Devices for Modeling Templates or Stencils for Three-Dimensional Objects with Non-Developable Surfaces and for Assisting the Transfer of Two-Dimensional Motifs Onto Those Objects
Application:
12/597,359 →
Publication:
US 2010/0060636
Acoustic Panel Having a Variable Acoustic Characteristic
Movable Air Exhaust Device for an Aircraft
Application:
12/598,795 →
Publication:
US 2010/0124875
Stairway for an Aircraft
Application:
12/599,377 →
Publication:
US 2010/0301163
System for Managing Rights of Access to Avionic Applications and Data and Method Implemented by This System
Method and Device for Monitoring a Horizontal Position of an Aircraft Rolling on the Ground
Device, System and Method of Estimating the Angle of Attack of an Aircraft
Method for Simulating a System on Board an Aircraft for Testing an Operating Software Program and Device for Implementing Said Method
Dual Flow Turboshaft Engine and Improved Hot Flow Nozzle
Device and Method for Communication Between a Portable Computer System and Items of Avionics Equipment
Method and Device of Terrain Avoidance for an Aircraft
Method and Device for Servocontrolling an Aircraft Speed-Wise in an Approach Phase
Method for Reducing the Noise Generated by a Hole Under a High Energy Gas Flow
Sound Insulating Glazing Device, in Particular for Aircraft and Soundproofing Method for Glazing
Curved structural part made of composite material and a process for manufacturing such a part
Method and System for Monitoring Parameters of an Aircraft
Method and Device for Determining Anemometric Parameters of an Aircraft
Method and Device for Optimizing the Orientation of a Laser Anemometer on an Aircraft
Hydraulic System for Transmission of Forces Between an Aircraft Turboprop and an Attachment Device
Wiper Blade with Electromagnetic Command
Water-Resist Means for Aircraft Windows
Process for Localization of a Long-Member Profile That Is Inserted Between Fibrous Support Preforms That Are Assembled for Forming a Composite-Material Part
Aircraft with Windshield Glass Plates Interchangeable Between Different Types
Closing System for an Aircraft Fan Shroud
Device and Method for Automatically Generating a Control Order for an Aircraft Control Surface
Aircraft Icing Indicator
Application:
12/632,959 →
Publication:
US 2010/0140410
Aircraft Fuselage Section
Method and Device for Communication by Address Virtualization for the Integration Simulation of Components
Method and Device for Concentrating Messages for the Integration Simulation of Components
Method and Device for Detecting Non-Regression of an Input/Output System in a Simulation Environment
Application:
12/635,194 →
Publication:
US 2010/0146337
Tool, Tool Set and Method of Setting the Pitch of the Blades of a Model Propeller
Method and Device for Determining a Reliable Position of an Aircraft
Method and Device for Determining a Consolidated Position of a Traveling Object, Particularly an Aircraft
Conveyor Device Intended in Particular for Luggage in an Aircraft Hold
Device for Moving Objects, Intended in Particular for Luggage in a Hold of an Aircraft
Multimodal Headrest for Vehicle Seat
Hold Layout Device for an Aircraft for Crew-Member Rest and Aircraft Comprising Same
De-Icing or Defogging System for Optical Instrument and Image Acquisition Device Provided with Said System
Methods and Devices for Communicating Diagnosis Data in a Real Time Communication Network
Electronic Card Able to Execute a Command Originating from a Simulation System and a Command Originating from a Diagnostic Module and Associated Simulation Method
Display System for Avionic and Non-Avionic Applications
Method and System for Managing Electrical Power Supply Outages on Board an Aircraft
Advanced Aircraft Cockpit
Current Sensor
Device for Attaching an Aircraft Engine Comprising a Thrust Force Take-Up Device with a Compact Design
Method for Debugging Operational Software of a System Onboard an Aircraft and Device for Implementing the Same
Method for Automatic Script Generation for Testing the Validity of Operational Software of a System Onboard an Aircraft and Device for Implementing the Same
Application:
12/678,143 →
Publication:
US 2011/0047529
Method for Processing the Volume of Information Handled During the Debugging Phase of Operational Software Onboard an Aircraft and Device for Implementing the Same
Application:
12/678,144 →
Publication:
US 2010/0299559
Method and a System for Automatically Managing Check Lists on an Aircraft
Application:
12/684,166 →
Publication:
US 2010/0174423
Method of Determining a Stiff Value of an Aerodynamic Coefficient
Aircraft Front Portion Including a Concave Bulkhead Separating a Non-Pressurized Radome Area and a Pressurized Area
Method and System for Displaying Symbologies on an Aircraft
Flight Control System and Aircraft Comprising It
Flight Control System and Aircraft Comprising It
Aircraft Presenting Two Pairs of Wings and Fuel Tanks in Fluid Communication
Current Return Network Element for an Aircraft
Aircraft with a Reinforced Floor Structure
Vane for Aircraft Turbine Engine Receiver, Provided with Two Hollow Cores Lodged in One Another
Set of Equipment for an Aircraft Including a Video Sensor and at Least Two Head-Up Display Devices and a Processor for Alleviating Alignment Discrepancies for the at Least Two Head-Up Display Devices
Device for Installing Windshield Panes
Blade for Turbomachine Receiving Part, Comprising an Airfoil Part Including a Mechanical Fuse
Blade Retaining Device for Turbo Machine Propeller
Method and Device for Generating an Optimum Aerodynamic Configuration of an Aircraft During a Flight
Process and Device for Automatically Optimizing on the Ground the Aerodynamic Configuration of an Aircraft
Aircraft Including Data Destruction Means
Application:
12/718,676 →
Publication:
US 2010/0235567
Method and Device for Estimating at Least One Wind Characteristic on an Aircraft
Movable Main Undercarriage for an Aircraft
Methods and Devices for Automated Loading of Software, in an Apparatus Such as an Aircraft, Including the Updating of the Associated Documentation
Method for Making Uniform the Thrust Command of the Engines of an Aircraft
Methods and Devices for Managing Events Linked to the Security of the Computer Systems of Aircraft
Rest Module with a First Partial Module with Direct Access to a Possible Second Partial Module
Testing Device and Method for Checking the Operability of a Nose Wheel Steering Control Unit in an Aircraft
Method of Loading a Database on Board an Aircraft
Method and Tool for Simulation of the Aerodynamic Behaviour of an Aircraft in Flight Close to the Ground
Method of combined simulation of the software and hardware parts of a computer system, and associated system
Fly-By-Wire Control System for an Aircraft Comprising Detection of Pilot Induced Oscillations and a Control for Such a System
Method and Device for Integrating a Rf Gps Emulator in a Simulation Environment
Method of Predicting the Aerodynamic Behavior of an Aircraft Element
Method of Interacting with a Display System on Board an Aircraft
Application:
12/770,202 →
Publication:
US 2010/0287506
Method for Detecting the Opening of a Thrust Reverser for a Jet Engine of an Aircraft
Related Assignments
(25)
Other recorded transfers of the patents in this record — the chain of ownership.
Assignment of Assignors Interest.
Mar 9, 1992
From: LACABANNE, MICHEL
To: AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE
Reel/Frame 006038/0657 →
Assignment of Assignors Interest.
Mar 23, 1992
From: PORTE, ALAIN
To: AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE
Reel/Frame 006050/0615 →
Assignment of Assignors Interest.
Jul 29, 1992
From: BISSEY, BERNARD; MAFFRE, CLAUDE
To: AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE
Reel/Frame 006229/0970 →
Assignment of Assignors Interest.
Aug 21, 1992
From: BASCANS, REMI; FLEURY, CHRISTOPHE; AUTECHAUD, ERIC; N'GUYEN, CHRISTIAN
To: AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE AYANT SON SIEGE SOCIAL
Reel/Frame 006209/0880 →
Assignment of Assignors Interest.
Aug 26, 1992
From: BASCANS, REMI; FLEURY, CHRISTOPHE; AUTECHAUD, ERIC; N'GUYEN, CHRISTIAN
To: AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE AYANT SON SIEGE SOCIAL
Reel/Frame 006243/0623 →
Assignment of Assignors Interest.
Aug 28, 1992
From: FABRE, PIERRE
To: AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE
Reel/Frame 006241/0892 →
Assignment of Assignors Interest.
Nov 12, 1992
From: REVILLET, GEORGES; BERGE, PHILIPPE
To: SEXTANT AVIONIQUE
Reel/Frame 006296/0193 →
Assignment of Assignors Interest.
Dec 22, 1992
From: BODIN, PHILIPPE; EUGENE, MICHEL; MICHELET, LUC
To: AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE
Reel/Frame 006371/0348 →
Assignment of Assignors Interest.
Dec 22, 1992
From: TRAVERSE, PASCAL; LE TRON, XAVIER
To: AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE
Reel/Frame 006386/0850 →
Assignment of Assignors Interest.
Feb 25, 1993
From: BISSEY, BERNARD; CAZENAVE, ANDRE
To: AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE
Reel/Frame 006456/0426 →
Assignment of Assignors Interest.
Mar 17, 1993
From: EUGENE, MICHEL; RODRIGUEZ, JEAN-CLAUDE; DEBONS, RENE
To: AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE
Reel/Frame 006491/0617 →
Assignment of Assignors Interest.
Apr 12, 1993
From: PASCUAL, NATHALIE; FLEURY, CHRISTOPHE; SAGNES, GEORGES; N'GUYEN, CHRISTIAN
To: AEROSPATIALE SOCIETE
Reel/Frame 006492/0234 →
Assignment of Assignor's Interest
Jul 2, 1993
From: CAHEN, FRANCOIS
To: SEXTANT AVIONIQUE
Reel/Frame 006595/0730 →
Assignment of Assignor's Interest
Aug 11, 1993
From: RIVRON, VINCENT; VOLLARD, CECILE
To: AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE
Reel/Frame 006657/0792 →
Assignment of Assignor's Interest
Sep 8, 1993
From: SERVANTY, GUY; OBRY, PHILIPPE
To: C.A.S.O. CONCEPTION AERONAUTIQUE DU SUD-OUEST
Reel/Frame 006682/0132 →
Assignment of Assignor's Interest
Sep 20, 1993
From: TOURNIER, GILLES; BALLENGHIEN, JEAN-LUC; ROQUES, SERGE
To: AEROSPATILE SOCIETE NATIONALE INDUSTRIELLE
Reel/Frame 006871/0490 →
Assignment of Assignor's Interest
Oct 8, 1993
From: JARRIGE, MARIE CLAUDE; JARRIGE, JEAN-LUC; DELILLE, ANNIE; LAINEZ, VINCENT
To: AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE
Reel/Frame 006759/0207 →
Assignment of Assignor's Interest
Oct 14, 1993
From: MAUPILLIER, DIDIER
To: AEROSPATIALE - SOCIETE NATIONALE INDUSTRIELLE; SEXTANT AVIONIQUE
Reel/Frame 006721/0553 →
Assignment of Assignor's Interest
Oct 18, 1993
From: BLOT, PHILIPPE A; AUGEREAU, JOEL; BRETAGNE, JOEL; DITTBERNER, JEAN-JACQUES
To: SOCIETE ANONYME DITE: ACB; SOCIETE ANONYME DITE: AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE
Reel/Frame 006764/0605 →
Assignment of Assignor's Interest
Oct 27, 1993
From: COLLEU, RACHEL; FOUGERE, PIERRE
To: AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE
Reel/Frame 006742/0804 →
Assignment of Assignor's Interest
Nov 22, 1993
From: DUSART, GERARD
To: AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE
Reel/Frame 006772/0699 →
Assignment of Assignor's Interest
Dec 2, 1993
From: AVIONIQUE, SEXTANT
To: CROUZET AUTOMATISMES
Reel/Frame 006779/0822 →
Assignment of Assignor's Interest
Dec 14, 1993
From: DURAND, YVES
To: AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE
Reel/Frame 006801/0827 →
Assignment of Assignor's Interest
Jan 7, 1994
From: CAPBERN, PATRICK; CHARIERAS, JEROME; CHAUMEL, PASCAL
To: AEROSPATIALE SOCIETE
Reel/Frame 006823/0617 →
Assignment of Assignor's Interest
Feb 8, 1994
From: CAHUZAC, GEORGES J. J.
To: AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE
Reel/Frame 006861/0336 →