Patent Assignment
Reel/Frame 032813/0001
Change of Name
Recorded: 2014-05-02
Pages: 21
Assignor
EUROCOPTER
Executed: 2014-01-07
Assignee
AIRBUS HELICOPTERS
AEROPORT INTERNATIONAL MARSEILLE PROVENCE, MARIGNANE CEDEX, 13725, FRANCE
Covered Properties
(303)
Mould for a Composite Material Part Coated with a Stripping Product
Method for Regulating the Flow Rate of Fuel to a Turboshaft Engine in Acceleration or in Deceleration
Method of Optimizing Braiding Control Parameters for a Sheath for Shielding a Bundle of Electrical Conductors, and a Bundle as Obtained in This Way
On-Board Device for Measuring the Mass and the Position of the Center of Gravity of an Aircraft
Undercarriage with Anticrash and Antiresonance Skids for a Rotary Wing Aircraft, and an Aircraft
Rotorcraft Blade Provided with a Tiltable Flap
Rotary Flap
Composite Anti-Crash Structure with Lateral Retention, for an Aircraft
Blade Having an Integral Cuff, and a Rotorcraft Rotor Provided with Such a Blade
Flying Control Device for a Rotorcraft
Balancing the Power of Two Turboshaft Engines of an Aircraft
System for Detecting Obstacles in the Vicinity of a Touchdown Point
Device for Interconnecting First and Second Control Sticks of an Aircraft in Roll and in Pitch
Method and an Instrument for Determining the Limiting Parameter of a Turboshaft Engine
Method and a System for Diagnosing an Aircraft from Measurements Performed on the Aircraft
Method and a Device for De-Icing an Aircraft Wall
Aircraft Firewall
Method and a system for determining and indicating a sound nuisance level outside an aircraft
Hybrid Positioning Method and Device
Device for Opposing Sloshing in a Flexible Tank
Mechanical Transmission System with a Magnetic Damper for a Rotorcraft
Magnetically-Damped Supercritical Transmission System
Absorbent Covering
Method and a System for Processing and Displaying Images of the Surroundings of an Aircraft
Patent:
8,373,590 →
Application:
11/962,143 →
To Rotorcraft Rotors Fitted with Inter-Blade Dampers
Method and a Device for Controlling the Ground Clearance of an Aircraft
Electric Actuator for Aircraft Flight Control
Rotorcraft Blade Provided with a Radial Segment and with at Least One Forwardly-and/or Rearwardly-Swept Segment
Crimping System with Integrated Monitoring
Rotorcraft Control System
Hydraulic Distributor Provided with a Device for Detecting Seizing
Fast Hybrid Helicopter with Long Range and Proportional Drive to the Rotor and the Propeller
Method and Apparatus for Controlling and Regulating a Rotorcraft Turbine Engine
Blade Provided with a Horizontally-Wound Spar, and a Method of Fabricating Such a Spar
Fast Hybrid Helicopter with Long Range and an Optimized Lift Rotor
Fast Hybrid Helicopter with Long Range with Longitudinal Trim Control
Emergency Beacon
Method of Testing an Electronic System
Method and a Device for Bonding a Metal Fairing to the Leading Edge of an Airfoil
Flexible Disk, a Flexible Coupling Provided with Such a Flexible Disk, a Mounting Flange Provided with Such a Flexible Coupling, and a Transmission Shaft Fitted with Such a Mounting Flange
Compensation Actuator for a Rotorcraft Flight Control
Foldable Step for a Vehicle, and a Vehicle Provided with Such a Step Unit
Method for Regulating the Flow Rate of Fuel to a Turboshaft Engine in Acceleration or in Deceleration
Method and a Device for Obtaining a Predictive Vertical Speed of a Rotorcraft
Method and a Device for Detecting and Signaling That a Rotorcraft Is Approaching the Vortex Domain
Vehicle Damper
Retraction Cylinder and Rotorcraft Undercarriage Furnished with Such a Retraction Cylinder
Aircraft Provided with a Silent Shrouded Rotor
Energy Adsorber Device That Adapts Automatically to the Weight It Supports
Rotorcraft Blade, a Rotorcraft Rotor Provided with Said Blade, and a Method of Fabricating Said Blade
Turboengine Air Intake Provided with a Controlled Filter System
System and a Method for Dynamically Balancing a Blade
Rotorcraft Blade Provided with a Spar Incorporating a Fastener Attachment, and a Method of Fabricating Such a Spar
Method of Optimizing a Ducted Anti-Torque Rotor of a Rotorcraft, in Particular a Helicopter, to Minimize Acoustic Annoyance, and a Ducted Anti-Torque Rotor Obtained Thereby
Helicopter Provided with a Plurality of Lift Elements Each Provided with a Respective Tab for Controlling the Angles of Incidence of Its Blades
Helicopter Provided with a Plurality of Lift Elements for Controlling the Angles of Incidence of Its Blades
Power Transmission Gearbox Presenting a Modifiable Speed of Rotation at Its Outlet, and a Corresponding Method of Operation
Rigid Hydraulic Control Shaft and a Control System for Varying the Pitch of a Propeller
Aircraft Flight Control
Automatic Configuration-Tracking Apparatus, and a Method and a System for Such Tracking
Hybrid Helicopter That Is Fast and Has Long Range
Energy Absorber Element
Crashworthy Seat for a Vehicle
Power-Assisted Control System for a Rotorcraft
Breakable Coupling Device, and an Associated Trim Actuator
Blade for Reducing the Drag Movements of Said Blade, and a Method of Reducing Such a Drag Movement
Blade Provided with a Resonator to Reduce the Drag Movements of Said Blade, and a Method Implemented by Said Blade
Diagnostic Method for Locating a Failure in a Complex System, and a Device for Implementing Said Method
Hybrid Engine Installation and a Method of Controlling Such an Engine Installation
Method of Organizing Aircraft Maintenance
Adapting Selective Terrain Warnings as a Function of the Instantaneous Maneuverability of a Rotorcraft
Leaktight Frame for a Window and a Mechanical Assembly Provided with Such a Frame
Cable-Cutter Device
Method of Jettisoning an External Load Carried by an Aircraft, and an Associated Device
Drive Device for Driving First and Second Lift Rotors of a Rotorcraft Having Twin Rotors in Tandem
Method of Inspecting the Integrity of an Avionics System, and an Inspection Device for Implementing Said Method
Method of Ensuring the Integrity of Flight Data and a System for Implementing Said Method
Rotary Actuator Incorporating a Force Relationship, and a Method of Reducing Angular Slack in Such a Rotary Actuator
Hydraulic Valve, a Hybrid Helicopter Provided with Such a Hydraulic Valve, and a Method Implemented by the Hydraulic Valve
Method and System for Estimating the Angular Speed of a Mobile
Fastener Tool for Fastening a Transmission Shaft, and a Balancing Bench Including Such a Tool
Coupling with Slack-Takeup, a Rotor, and a Rotary Wing Aircraft
Powerplant and a Method of Driving a Mechanical System via Said Powerplant
Method of Determining and Displaying Flying Indications and a Flight Indicator for Implementing Said Method
Method and a Device for Optimizing the Operation of Propulsive Propellers Disposed on Either Side of a Rotorcraft Fuselage
Tooling for Holding Thin Metal Parts Making Up a Hollow Structure in Order to Enable Them to Be Friction-Welded Together
Application:
12/724,455 →
Publication:
US 2010/0269326
Method of Assembling Metal Parts by Friction Welding, with the Welding Temperature Being Controlled Using Thermally Conductive Elements
Blade Provided with a Drag Damper, and a Rotor Provided with Such a Blade
Concentrated-Mass Device for Reducing Vibration Generated by a Rotorcraft Lift Rotor, and a Rotor Hub Fitted with Such a Device
Drive Control and Regulation Method and System for a Hybrid Helicopter
Device for Assisting in Piloting a Hybrid Helicopter, a Hybrid Helicopter Provided with Such a Device, and a Method Implemented by Said Device
Method of Controlling a Hybrid Helicopter in Yaw, and a Hybrid Helicopter Provided with a Yaw Control Device Suitable for Implementing Said Method
Distributed-Mass Device for Reducing Vibration Generated by a Rotorcraft Lift Rotor, and a Rotor Hub Fitted with Such a Device
Variable Ratio Crank for a Manual Flight Control Linkage of a Rotary Wing Aircraft
Mechanical Device for Combining First and Second Control Orders, and an Aircraft Provided with Such a Device
Method of Assisting Piloting, Piloting Assistance Means, and a Piloting Assistance Device for a Rotorcraft Using Said Piloting Assistance Means to Implement Said Piloting Assistance Method
Device and a Method for Starting a Turbine Engine Fitted to a Helicopter, Making Use of an Electrical Energy Source That Includes Discharge Booster Members
Method of Assisting Piloting at Low Altitude
Insulating Coating with Mass Amplification
Variable Damping of Haptic Feedback for a Flight-Attitude Changing Linkage of an Aircraft
Method of Reducing or Even Eliminating the Vibration of a Rotorcraft Lift and Propulsion Rotor, and an Airfoil Assembly and a Rotor Implementing Said Method
Frequency Adapter and Return Means Suitable for Being Arranged in Such a Frequency Adapter
Application:
12/850,694 →
Publication:
US 2011/0052395
Reusable Rotorcraft Bumper, and a Rotorcraft Having Such a Bumper
Stripping Composition for a Mold for Making a Composite Material Part, and Method of Preparing
Assisted Piloting Method and Device for an Aircraft for Use in the Event of a First Limit Indicator Breaking Down
Highly Representative Real-Time Simulation of an Avionics System
Seat for Powered Aircraft, the Seat Incorporating Means for Protecting Its Passenger in the Event of a Crash
Mechanism for Attenuating Torque Pulsations Between an Engine and a Rotorcraft Rotor Driven by the Engine
Set of Cyclic Swashplates for Controlling the Pitch of Blades of a Main Rotor, and a Rotor Provided with Such a Set
Device for Reducing Vibration Generated by Rotorcraft Rotor, and Rotorcraft Provided with Such Device
Honeycomb-Structured Floor Panel for a Vehicle Incorporating a Fastener Element
Filter Mechanism for Filtering Vibration in Aircraft
Air Inlet for an Aircraft Turbine Engine, an Aircraft Provided with Such an Air Inlet, and a Method of Optimizing the Operation of an Aircraft Turbine Engine with the Help of an Air Inlet
Long-Range Aircraft with High Forward Speed in Cruising Flight
Power Plant, a Helicopter Including Such a Power Plant, and a Method Implemented by Said Power Plant
Tail Skid for Protecting a Structural Element of an Aircraft, an Aircraft Provided with Such a Tail Skid, and an Anti-Overturning Method Implemented by Said Tail Skid
Method of Obtaining a Local Terrain Elevation Database from Detector Means on Board a Vehicle
Method of Using Telemetry to Detect at Least One Suspended Threadlike Object, the Object Lying in the Detection Field of a Telemeter Mounted on Board a Vehicle
Aircraft Provided with a Device for Assisting the Pilot When Carrying an External Load with a Sling, and a Method Implemented by Said Device
Application:
12/959,646 →
Publication:
US 2011/0137497
Method of Increasing the Safety of a Power Plant, and a Power Plant Suitable for Implementing the Method
Aircraft Undercarriage Having a Rocker Lever with a Swivel and Hinged Twin Wheels
Vibration Damper Mechanism, and a Flying Machine Including a Carrier Structure and a Rotor Provided with Such a Mechanism
Rotor Carrier Structure with a Damper Device for Avoiding Unstable Coupling Between Resonant Vibration Modes
Method for Manufacturing Electrically Non-Conductive Painted Substrate
Method of Fabricating a Painted Substrate That Is Electrically Non-Conductive
Locking Device for Locking a Structural Element Against an Adjacent Structure, an Aircraft Provided with Said Device, and an Extraction Method Implemented by Said Device
Device for Filling a Tank by Gravity or Under Pressure
Method and a Device for Draining a Tank, and a Tank and an Aircraft Fitted with Such a Device
Turning-Stabilized Estimation of the Attitude Angles of an Aircraft
Removable Support for Optional External Equipment on an Aircraft, and an Aircraft Provided with Such a Support
Overall Optimization of the Configuration of a Meshed Wireless Network of Rf Devices in an Aircraft
Application:
13/028,665 →
Publication:
US 2011/0208973
Anti-Crash Seat for a Vehicle
Method of Fabricating a Honeycomb Structured Panel
Rotary Wing Aircraft Provided with an Emergency Undercarriage
Blade with Adaptive Twisting, and a Rotor Provided with Such a Blade
Method and a Device for Flying Safely at Low Altitude in an Aircraft
Mechanical Assembly Provided with Means for Monitoring for a Structural Anomaly, a Gearbox Provided with Such a Mechanical Assembly, and a Method of Monitoring for a Structural Anomaly
Rotary Wing Blade, a Rotary Wing Including Such a Blade, and an Aircraft
Application:
13/050,242 →
Publication:
US 2011/0236208
Blade Damper, and a Rotor Fitted with Such a Damper
Control Architecture and Process for Porting Application Software for Equipment on Board an Aircraft to a Consumer Standard Computer Hardware Unit
Method of Controlling and Regulating the Deflection Angle of a Tailplane in a Hybrid Helicopter
Energy Absorber System for an Undercarriage, and an Aircraft Provided with Said Energy Absorber System
Landing Gear Provided with Energy Absorber Means, an Aircraft Provided with Said Landing Gear, and a Method of Landing
Device for Reducing the Vibration Generated by a Rotorcraft Lift Rotor, and a Rotor Hub Provided with Such a Device
Method of Controlling a Buoyancy System for an Aircraft, and a Control System Implementing Said Method
Simplified Flight Control System Including a Declutchable Friction Device
Rotor Provided with a Device for Protecting It Against Lightning, and an Aircraft Provided with Such a Rotor
Electrical Power Supply and Control Device for Equipment of a Rotor, and an Aircraft Fitted with Such a Device
Handling an Insert to Implant It in a Cellular Panel and to Withdraw It from the Panel
Application:
13/111,153 →
Publication:
US 2011/0290774
Aircraft Power Plant, an Aircraft, and a Method of Using a Piston Engine in a Power Plant Having a Conventional Gearbox
Method of Monitoring the Effectiveness of a Damper, and a Device for Implementing Said Method
Inertial Measurement Device and an Aircraft Including Such a Device
Device for Damping the Vibration of a Structure
Method of Avoiding a Grid Clogging, a Grid and an Air Intake Implementing Such a Method
Method and a Rotary Wing Aircraft That Are Optimized So as to Minimize the Consequences for the Occupants of Said Aircraft of an Off-Specification Emergency Landing
Communications Network That Is Distributed, Modular, and Configurable for an on-Board Avionics System
Application:
13/167,171 →
Publication:
US 2012/0008697
Method and an Aircraft Provided with a Swiveling Tail Rotor
Electrical Architecture for a Rotary Wing Aircraft with a Hybrid Power Plant
Piloting Assistance Method for Aircraft
Method of Minimizing the Attitude Hump Phenomenon and a Rotary Wing Aircraft Provided with Stabilizer Means Therefor
Hydraulic Actuator with a Limit Force Detector Device
Method and a Device for Synthesizing an Electrical and Electronic Architecture
Method and a Device for Optimizing the Utilization of an Engine
Method of Activating Protection Means for Protecting an Occupant of an Aircraft, and an Aircraft Implementing Said Method
Rotary Wing Aircraft Provided with Propulsion Means, and a Method Applied by Said Aircraft
Blade with Minimized Vulnerability
Flexible Coupling Means
Stepped Instrument Panel for Aircraft
An Aircraft Undercarriage
De-Icing System for a Fixed or Rotary Aircraft Wing
Skid Landing Gear and an Aircraft Provided with Such Landing Gear
Method of Fabricating a Spar for a Rotorcraft Blade
Aircraft Provided with a Tail Plane Including Means for Combating Flutter
Aircraft Provided with Hoist Means, and an Associated Method
Aircraft Power Plant, an Aircraft, and a Method of Piloting Said Aircraft
Method of Controlling an Overspeed Safety System for Aeroengines and a Control Circuit for Implementing Said Method
Method of Controlling a Buoyancy System for an Aircraft, a Buoyancy System Implementing Said Method, and an Aircraft
Fabricating Parts with Composite Material Reinforcement Having a Single Crossing Line
Rotorcraft Structural Element for Reducing Aerodynamic Drag
Blade for a Helicopter Anti-Torque Device
Aircraft Provided with a Swiveling Tail Rotor, and an Associated Method
Predicting Time to Maintenance by Fusion Between Modeling and Simulation for Electronic Equipment on Board an Aircraft
Removable Fastener Device Equipped with Attachment Means for Attaching an External Load and with Fastener Means for Fastening Said Attachment Means to an Aircraft, an Associated Aircraft, and an Associated Method
Protective Device for Protecting an Occupant of a Vehicle, a Seat, and an Associated Vehicle
Blade and Method of Fabricating Said Blade
Lead-Lag Damper Device to Limit an End-of-Stroke Force Peak
Fastener Device, a Seat Provided with Said Device, and a Vehicle
Method of Optimizing the Loading of Loads in a Vehicle
Vehicle Panel Provided with a Movable Window, and an Associated Vehicle
Cyclic Stick for Mechanically Transmitting Commands for Controlling a Rotorcraft, the Stick Having a Lever Arm That Is Amplified Selectively in the Event of an Emergency
Method of Measuring Height and Detecting Obstacles, a Radioaltimeter, and an Aircraft
Emergency Piloting by Means of a Series Actuator for a Manual Flight Control System in an Aircraft
Electrical Power Supply Device for a Resistor Element, and an Electrical System Provided with Said Device and Said Resistor Element
Application:
13/425,746 →
Publication:
US 2012/0241434
Method and a Device for Assisting the Piloting of an Aircraft, and an Aircraft
Weatherproof Surround for Safely Jettisoning a Removable Panel
Control Lever for Controlling a Rotary Wing, a Mechanical Control System Including Said Control Lever, and an Aircraft
Passing from a Non-Synchronized State Between an Engine and a Rotor to a Synchronized State
Rotor Damper Device, and an Associated Rotor and Aircraft
Device for Launching and Recovering a Drone, and an Associated Aircraft
Device and a Method for Constructing a Flight Path in Order to Reach a Destination
Electrical Power Supply Device for Electrically Powering at Least One Item of Equipment on a Rotary Rotor of an Aircraft, and an Aircraft
Aircraft Provided with a Device for Reducing Vibration, and a Method Therefor
Method of Determining the Static Force Developed by a Servo-Control
Twist Mechanism for Twisting a Rotor Blade for a Rotorcraft, and a Blade
Technical Method, a Maintenance Device, and an Aircraft
Piloting Assistance System and an Aircraft
Rotary-Wing and Fixed-Wing Aircraft
Rotor Blade and an Aircraft
Primary Flight Controls
Method of Automatically Controlling a Rotary Wing Aircraft Having at Least One Propulsion Propeller, an Autopilot Device, and an Aircraft
Method of Controlling a Group of Engines, and an Aircraft
Piloting Assistance Method, a Piloting Assistance Device, and an Aircraft
Rotorcraft Having Lighting Equipment with a Plurality of Headlights Operated for Landing, Winching, and Searching
Energy-Absorbing Element and Related Pretensioning Flange
Architecture for Feeding Fuel to a Power Plant for Driving a Rotary Wing of a Rotorcraft
Device for Fastening a Nut to the Surface of a Body by Means of an Assembly Plate
Fast, Long-Range Aircraft
Control Method for an Overspeed Safety System, and an Associated System and Aircraft
System for Controlling Pitch Variation of the Blades of a Propeller, a Propeller, and an Aircraft
Method of Regulating the Propulsive Speed of a Hybrid Helicopter
Surface-Area Safety Means and a Vehicle
Hybrid Aircraft Having a Rotary Wing
Rotorcraft Yaw Piloting System Making Use of a Member of the Human-Operated Type and of a Flight Control Generator of the Objective Type
Aircraft Antenna, and an Aircraft
Aircraft Provided with a Buoyancy System for a Rotary Element
Landing Gear, an Aircraft, and a Method
Control Means for a Lifter Device, Hoist Apparatus, and an Aircraft
Fire-Protection Storage Means, a Vehicle, and a Method
Application:
13/654,658 →
Publication:
US 2013/0327548
Device for Feeding Electricity to Equipment, the Device Being Incorporated in the Floor of an Aircraft Cabin
Ball-Joint Mechanism Between a Clevis and a Connecting Rod, in Particular for Control Apparatus of a Rotorcraft
Antivibration Suspension Means for a Tie Bar of an Aircraft Power Transmission Gearbox, an Antivibration Suspension Device, and an Aircraft
Device for Varying Blade Pitch of a Lift Rotor
Method of Assisted Piloting of a Rotary Wing Aircraft Having at Least One Propulsion Propeller, an Assisted Piloting Device, and an Aircraft
Appliance for Localized Heating of a Polymer Material Surface to Be Repaired by Blowing a Hot Fluid Inside a Confinement Chamber
Anti-Torque Device with Longitudinal Thrust for a Rotorcraft
Rotor Blade
Device for Assisting the Piloting of a Rotorcraft
Rotocraft Rotor Including a Flapping Abutment Mechanism for Blades Hinged on a Hub of the Rotor
Method and a Rotary Wing Aircraft Optimized for Minimizing the Consequences of a Running Off-Specification Emergency Landing
Device for Protecting an Individual Sitting on a Seat, a Seat, and a Vehicle
Device for Reversibly Fastening a Panel to a Structure So as to Obtain a Window in That Structure, a Vehicle, and a Method
Laminated Abutment, a Rotor Provided with Such an Abutment, and an Aircraft
Aircraft Power Plant, an Aircraft, and a Method of Piloting Said Aircraft
Method and a Device for Performing a Health Check of a Turbine Engine of an Aircraft Having at Least One Such Engine
Method and a Device for Performing a Check of the Health of a Turbine Engine of an Aircraft Provided with at Least One Turbine Engine
Method of Optimizing the Performance of an Aircraft, a Device, and an Aircraft
Fluid Temperature Control Installation for Rotorcraft, Associating a System for Cooling a Power Plant with a System for Heating a Cabin
Communication Device, an Aircraft Rotor, and an Aircraft
Method of Simulating a Failure on an Aircraft
On-Board Device for Measuring the Weight of an Aircraft and the Position of Its Center of Gravity
Device and a Method of Regulating a Power Plant Including at Least One Turbine Engine, and an Aircraft
Device and a Method for Regulating a Turbine Engine, and an Aircraft
Method of Automatically Regulating a Rotorcraft Power Plant, a Rotorcraft Power Plant, and a Rotorcraft
Drainage Circuit for Draining Liquid Coming from a Power Plant of a Rotorcraft, the Circuit Incorporating an Appliance for Monitoring an Excessive Flow of the Liquid
Method of Automatically Regulating Aircraft Power Plant Gas Generator and Free Turbine Speeds as a Function of Heating, Electricity Generation, Noise Emission, and Fuel Consumption
Interface and a Method for Mounting Together a Piece of Equipment and a Rotary Drive Source in a Rotorcraft Power Plant
Method and a Device for Monitoring an Engine
Method of Providing a Volume-Mass Law for Fuel Consumption
Rotary Wing Aircraft Having a Tail Rotor, and a Method of Optimizing the Operation of a Tail Rotor
Application:
13/765,798 →
Publication:
US 2013/0264412
Rotor Blade for a Rotor of an Aircraft Designed to Minimize Noise Emitted by the Rotor
Aircraft Bench Provided with Crash-Protection Means
Method of Simultaneously Transforming a Plurality of Voice Signals Input to a Communications System
Device for Monitoring the Flapping and/or Lag Behavior of a Blade of a Rotorcraft Rotor
Method and a Device for Adapting the Man-Machine Interface of an Aircraft Depending on the Level of the Pilot's Functional State
Flexible Coupling Means and a Mechanical Transmission
Aircraft Airfoil, and an Aircraft Provided with Such an Airfoil
Standby Instrument for an Aircraft, the Instrument Providing Flight Information, Power Margin Information, and Assistance in Piloting
Fuel Feed Network for a Rotorcraft Engine, the Network Including Means for Priming a Pump for Sucking Fuel from a Feed Tank
Device for Monitoring the Sealing of a Rotorcraft Transmission Box by Suction
Ball Joint Device
Application:
13/889,445 →
Publication:
US 2013/0308995
Electrical Power Supply Device for Powering at Least One Piece of Equipment of an Aircraft Rotor, and an Aircraft
Pitching Stabilization Means and a Rotary Wing Aircraft Including Such Means
Method of Controlling the Wing Flaps and Horizontal Stabilizer of a Hybrid Helicopter
Method of Controlling the Wing Flaps and Horizontal Stabilizer of a Hybrid Helicopter
Tank, a Fuel Storage System, and an Aircraft
Automatic Flight Control Method for a Rotorcraft Enabling the Rotocraft to Maintain a Path by Tracking Manual Flight Controls
Pressure-Filling System for Filling a Tank, and an Aircraft Including the System
Procedure and Device for the Determination of Airspeeds of a Rotorcraft in Stationary Flight and/or at Low Speeds
Hydrualic Control Valve, a Device for Adjusting Blade Pitch, and an Aircraft Provided with Such a Hydraulic Control Vavle
Device for End-to-End Coupling of a Supercritical Transmission Shaft, in Particular for Driving a Rotorcraft Rotor
Method of Fabricating a Mechanical Part, Including a Method of Predicting the Risks of Crack Initiation in the Part in a "Fretting-Fatigue" Situation
Rotorcraft Rotor Fitted with Lead-Lag Dampers Housed in Sleeves Connecting Blades to a Hub of the Rotor
Hybrid Power Supply Architecture for Supplying Mechanical Power to a Rotor and Managed from the on-Board Network of a Rotorcraft
Aircraft Rotor Fitted with a Connector Device for Connecting Electrical Power Between a Hub and Blades of the Rotor
Reversible Electrical Machine for an Aircraft
System and Method of Detecting Defects of a Rolling Bearing by Vibration Analysis
Method of Assisting a Pilot of a Single-Engined Rotary Wing Aircraft During a Stage of Flight in Autorotation
Method and a Device for Bonding a Metal Fairing to the Leading Edge of an Airfoil
Method and an Aircraft for Minimizing the Risks of the Aircraft Toppling on the Ground
Pitch Stabilizer and Rotary-Wing Aircraft Equipped with Such Stabilizer
Information Exchange System Comprising a Chain of Modules Connected Together by Hardened Digital Buses
Landing Gear Provided with a Stiffener for Increasing Its Stiffness in Roll, and an Aircraft
Method and an Active Device for Treating Noise on Board a Vehicle, and a Vehicle Provided with Such a Device
Method of Managing an Engine Failure on a Multi-Engined Aircraft Having a Hybrid Power Plant
Rotorcraft Fitted with a Mounting Structure for Jointly Mounting a Control Panel and an Avionics Rack Previously Fitted with a Unitary Cabling Assembly
Method of Automatically Triggering an Emergency Buoyancy System for a Hybrid Helicopter
Fuel Storage Device, an Aircraft, and a Method
Fuel Storage Tank, an Aircraft, and a Method
Method and a Rotary Wing Aircraft Having Three Engines
Rotary Wing Aircraft Having Two Main Engines Together with a Less Powerful Secondary Engine, and a Corresponding Method
Method of Arranging a Buoyancy System on an Aircraft, a Buoyancy System for an Aircraft, and an Aircraft
Method of Driving Rotation of a Rotorcraft Rotor by Anticipating Torque Needs Between Two Rotary Speed Setpoints of the Rotor
Method of Driving a Main Rotor of a Rotorcraft in Rotation in Compliance with a Speed of Rotation Setpoint of Variable Value
Related Assignments
(18)
Other recorded transfers of the patents in this record — the chain of ownership.
Assignment of Assignor's Interest
Sep 14, 2005
From: RENAUD, THIERRY
To: EUROCOPTER
Reel/Frame 016796/0312 →
Assignment of Assignor's Interest
Nov 22, 2005
From: LEROY, JULIE; TARDY, BERTRAND
To: EUROCOPTER
Reel/Frame 017051/0083 →
Assignment of Assignor's Interest
Jul 3, 2006
From: BOSCHET, PATRICK; PIEL, EMMANUEL
To: EUROCOPTER
Reel/Frame 017881/0537 →
Assignment of Assignor's Interest
Oct 25, 2006
From: MOUILLE, RENE
To: EUROCOPTER
Reel/Frame 018449/0246 →
Assignment of Assignor's Interest
Nov 20, 2006
From: ARNAUD, GILLES
To: EUROCOPTER
Reel/Frame 018617/0704 →
Assignment of Assignor's Interest
Feb 15, 2007
From: LORIN DE LA GRANDMAISON, FRANCOIS; MORANT, MICHEL; ARDESI, OLIVIER; GAFFIERO, JACQUES
To: EUROCOPTER
Reel/Frame 018906/0891 →
Assignment of Assignor's Interest
May 7, 2007
From: PAYEN, HERVE
To: EUROCOPTER
Reel/Frame 019259/0423 →
Assignment of Assignor's Interest
Jun 11, 2007
From: ROLLET, PHILIPPE
To: EUROCOPTER
Reel/Frame 019415/0804 →
Assignment of Assignor's Interest
Jun 12, 2007
From: BIANCHO, LAURENT; MICHEL, BERNARD; JAUME, JULIEN; GREGOIRE, FLORIAN
To: EUROCOPTER
Reel/Frame 019415/0846 →
Assignment of Assignor's Interest
Jul 17, 2007
From: FILIAS, FRANCOIS-XAVIER; SEQUEIRA, JEAN
To: EUROCOPTER
Reel/Frame 019564/0115 →
Assignment of Assignor's Interest
Jul 19, 2007
From: GAULMIN, FRANCOIS-XAVIER; IRAUDO, LLONEL
To: EUROCOPTER
Reel/Frame 019572/0785 →
Assignment of Assignor's Interest
Aug 2, 2007
From: TRAN, BANG
To: EUROCOPTER
Reel/Frame 019637/0332 →
Assignment of Assignor's Interest
Sep 11, 2007
From: GAULMIN, FRANCOIS-XAVIER; IRAUDO, LIONEL; CHANIOT, DANIEL
To: EUROCOPTER
Reel/Frame 019807/0857 →
Assignment of Assignor's Interest
Oct 3, 2007
From: GEMMATI, BERNARD
To: EUROCOPTER
Reel/Frame 019913/0644 →
Assignment of Assignor's Interest
Oct 10, 2007
From: CHANIOT, DANIEL
To: EUROCOPTER
Reel/Frame 019939/0360 →
Assignment of Assignor's Interest
Nov 9, 2007
From: BOSCHET, PATRICK; LORCET, BRUNO
To: EUROCOPTER
Reel/Frame 020094/0292 →
Assignment of Assignor's Interest
Feb 12, 2009
From: CERTAIN, BERNARD
To: EUROCOPTER
Reel/Frame 022250/0994 →
Change of Name
Dec 18, 2014
From: EUROCOPTER
To: AIRBUS HELICOPTERS
Reel/Frame 034663/0976 →