Patent Assignment
Reel/Frame 034663/0976
Change of Name
Recorded: 2014-12-18
Pages: 18
Assignor
EUROCOPTER
Executed: 2014-01-07
Assignee
AIRBUS HELICOPTERS
AEROPORT INTERNATIONAL MARSEILLE PROVENCE, MARIGNANE CEDEX, 13725, FRANCE
Covered Properties
(251)
Method and Device for Providing Electrical Continuity of Cable Shielding
Patent:
5,558,539 →
Application:
08/327,433 →
Flow-Straightener Vane for Counter-Torque Device with Ducted Rotor and Ducted Flow-Straightening Stator, for Helicopter
Patent:
5,619,797 →
Application:
08/422,314 →
Flow-Straightener Vane Made of Composite, Flow-Straightener Including It, for a Counter-Torque Device with Ducted Rotor and Ducted Flow-Straightening Stator, and Method for Manufacturing Them
Patent:
5,605,440 →
Application:
08/466,296 →
Pitch-Control Devices for Hingeless Rotors
Patent:
5,562,415 →
Application:
08/539,651 →
Flap Stops Device with Retractable Upper Stops Ring, and Rotor Head Including It
Patent:
5,588,801 →
Application:
08/539,692 →
Device for Controlling the Pitch of the Blades of a Rotorcraft Rotor
Patent:
5,599,167 →
Application:
08/540,070 →
Device for Controlling the Pitch of the Blades of a Rotorcraft Rotor
Patent:
5,624,232 →
Application:
08/540,130 →
Process for Producing Composite Panels
Patent:
5,635,013 →
Application:
08/555,429 →
Element Made of Composite Material with Assembly (Assemblies) for Electrical Continuity Through the Element
Patent:
5,863,667 →
Application:
08/570,217 →
Device for Illuminating a Set of Equipment Items Which Are Mounted on a Common Support
Patent:
5,702,171 →
Application:
08/571,240 →
Anti-Crash Seat with Harness for an Aircraft
Patent:
5,692,705 →
Application:
08/571,654 →
Process for the Production of a Shielding Sheath on a Bundle of Electrical Conductors
Patent:
5,718,041 →
Application:
08/571,792 →
Method and Device for Simultaneous Identification and Correction of Errors Due to Magnetic Perturbations and to Misalignments in the Measurements of a Magnetometer
Patent:
5,654,635 →
Application:
08/573,372 →
Hingeless Rotor with Intermediate Pitch-Control Rings
Patent:
5,788,462 →
Application:
08/573,781 →
Bidirectional Antivibration Suspension Device for Helicopter Rotor
Patent:
5,788,182 →
Application:
08/575,365 →
Device for Actuating a Controlled Member for an Aircraft, Particularly Such as a Fly-by-Wire Helicopter
Patent:
6,128,554 →
Application:
08/576,199 →
Force-Gradient Cyclic Stick System for a Helicopter
Patent:
5,746,398 →
Application:
08/577,130 →
Rudder Bar System with Force Gradient for a Helicopter
Patent:
5,738,310 →
Application:
08/577,131 →
Device and Machine for Connecting Connection Elements into Connectors
Application:
08/583,271 →
System for Minimizing the Dynamic Excitation of a Helicopter
Patent:
5,732,905 →
Application:
08/613,512 →
Method and Device for Simultaneous Identification and Correction of Errors in the Measurements of a Magnetometer
Patent:
5,682,335 →
Application:
08/631,703 →
Vibration Damping Apparatus for Helicopter Rotor
Patent:
5,639,214 →
Application:
08/634,872 →
Device for Damping the Drag of the Blades of a Rotor
Patent:
5,636,970 →
Application:
08/644,846 →
System for Detecting and Monitoring the Rotational Speed of at Least One Rotor and the Rotational Speed of at Least One Motor of a Rotary-Wing Aircraft, Such as a Helicopter
Patent:
5,831,429 →
Application:
08/658,672 →
Rotary-Wing Aircraft of the Compound Type, and Rear Structural Element for Such an Aircraft
Patent:
5,738,301 →
Application:
08/678,750 →
De-Icing Connectiion Installation for Rotorcraft Rotor
Patent:
5,769,606 →
Application:
08/679,218 →
Installation for Affording Electrical Continuity for Rotorcraft Rotor
Patent:
5,716,193 →
Application:
08/679,220 →
Device for Antivibratory Suspension of a Helicopter Rotor
Patent:
5,782,430 →
Application:
08/682,712 →
Method and Device for Reducing the Vibration Generated on the Structure of a Helicopter
Patent:
5,816,533 →
Application:
08/683,383 →
Device for Damping the Vibrations of a Structure Subjected to Dynamic Stresses
Patent:
5,814,963 →
Application:
08/728,036 →
Method for Manufacturing a Variable-Pitch Composite Blade for a Helicopter Rotor
Patent:
6,035,531 →
Application:
08/741,172 →
Method of Making a Composite
Patent:
5,855,709 →
Application:
08/749,349 →
Blade with Shielding for Enhanced Protection Against Lightning, for Rotorcraft Rotor
Patent:
5,800,129 →
Application:
08/757,965 →
Blade with Shielding for Enhanced Protection Against Lightning, for Rotorcraft Rotor
Patent:
5,863,181 →
Application:
08/757,967 →
Device for Reducing the Vibrations on the Structure of a Helicopter
Patent:
5,775,637 →
Application:
08/762,614 →
Eye Protection Device
Patent:
5,828,437 →
Application:
08/769,006 →
Device for Folding a Rotorcraft Rotor Blade
Patent:
5,782,606 →
Application:
08/769,061 →
Sealing Device for Rotating Shaft
Patent:
5,820,132 →
Application:
08/769,075 →
Device for Guiding, Driving, and Locking a Slot-in Module of Electrical or Electronic Equipment in a Cabinet
Patent:
5,909,935 →
Application:
08/769,076 →
Device for Heating an Aerofoil
Patent:
6,031,214 →
Application:
08/796,588 →
Suspension Device for a Transmission Box of a Rotary-Wing Aircraft
Patent:
5,813,626 →
Application:
08/832,105 →
Method and Device for Reducing the Effect of the Vibration Generated by the Driveline of a Helicopter
Patent:
5,895,012 →
Application:
08/832,783 →
Aircraft Flight Indicator
Patent:
5,886,649 →
Application:
08/870,401 →
Flight Indicator for a Helicopter
Patent:
5,915,273 →
Application:
08/870,403 →
Device for Reducing the Vibrations Generated by a Lift Rotor of a Rotary-Wing Aircraft
Patent:
6,045,090 →
Application:
08/873,696 →
Horizontal Speed Indicator for Rotary-Wing Aircraft
Patent:
5,952,570 →
Application:
08/879,365 →
Device for Locking the Blades of a Rotor, at Least in Terms of Pitch
Patent:
5,951,251 →
Application:
08/891,072 →
"Monitoring of the Wear of Sliding Electrical Contacts and Its Application to the State-Dependent and/or Predictive Maintenance of a Device Having Sliding Electical Contacts"
Patent:
6,034,531 →
Application:
08/892,106 →
Process for the Production of a Shielding Sheath on a Bundle of Electrical Conductors
Patent:
6,066,800 →
Application:
08/926,500 →
Method of Folding the Blades of a Main Rotor of a Rotary-Wing Aircraft, and Apparatus for Implementing the Method
Patent:
6,047,924 →
Application:
08/953,985 →
Blade with Swept-Back Tip for the Rotary Wings of an Aircraft
Patent:
6,000,911 →
Application:
08/972,274 →
Flight Indicator with Testing Means for a Helicopter
Patent:
5,908,485 →
Application:
08/974,077 →
Flight Control System for Rotary-Wing Aircraft, Especially for a Helicopter
Patent:
6,070,829 →
Application:
08/976,502 →
Power Margin Indicator for a Rotary-Wing Aircraft, Especially a Helicopter
Patent:
6,195,598 →
Application:
08/977,610 →
Device for Heating an Aerofoil
Patent:
5,947,418 →
Application:
08/978,045 →
Resistive Elements for Heating an Aerofoil and Device for Heating an Aerofoil Incorporating Such Elements
Patent:
5,971,323 →
Application:
08/978,046 →
Installation for Mounting an Engine on a Deck and for Connecting Its Output Shaft to at Least One Driven Mechanism
Patent:
6,019,313 →
Application:
08/978,049 →
Rotor with Folding Blades, for the Rotary Wings of an Aircraft
Patent:
6,176,679 →
Application:
09/006,504 →
Flight Control Device for an Aircraft, in Particular a Helicopter
Patent:
6,059,225 →
Application:
09/056,301 →
Device for Suspending an Aircraft Tank
Patent:
6,019,316 →
Application:
09/078,269 →
Anticrash Armor-Plated Modular Seat
Patent:
6,073,884 →
Application:
09/078,284 →
Rotorcraft Rotor with Fixed Flap Stops on Blades and Hub, and with Determined Pitch-Flap Law
Patent:
6,120,251 →
Application:
09/096,153 →
Method and Device for Locating Faults and Malfunctions in a Complex System
Patent:
6,295,488 →
Application:
09/099,187 →
Aircraft Position Indicator Device
Patent:
6,108,595 →
Application:
09/102,618 →
Device for Folding of a Helicopter Rotor Blade
Patent:
6,036,442 →
Application:
09/114,229 →
Blade Pitch Locking Device for a Main Rotor of a Rotary-Wing Aircraft
Patent:
6,032,899 →
Application:
09/114,233 →
Blade with Shielding for Enhanced Protection Against Lighting, for Rotorcraft Rotor
Patent:
6,102,662 →
Application:
09/115,538 →
Method and Device Operating by Interpolation in a Discrete Spectrum to Determine Characteristics of a Signal and Application Thereof
Patent:
6,347,286 →
Application:
09/116,800 →
Adhesive Composition for Hot Bonding and a Bonding Process Enabling Its Use
Patent:
6,194,499 →
Application:
09/122,630 →
Element Made of Composite Material Including Electrical Continuity Through the Element
Patent:
6,126,061 →
Application:
09/137,704 →
Swash-Plate Device for Controlling the Pitch of Rotor Blades with Non Rotating Plate Stop Track and Pin
Patent:
6,033,182 →
Application:
09/154,655 →
Alternating Current-Starting Device for a Helicopter Turbine Engine Unit
Patent:
6,242,881 →
Application:
09/162,950 →
Rotor Head Pendular Resonator
Patent:
6,062,818 →
Application:
09/164,142 →
Method and Device for Decoupling of the Behavior of an Aircraft,Particularly a Helicopter
Patent:
6,195,599 →
Application:
09/166,428 →
Device for Controlling a Helicopter Hybrid Countertorque System
Patent:
6,290,171 →
Application:
09/167,613 →
Device for Control of an Aerodynamic Steering Surface of a Helicopter
Patent:
6,142,413 →
Application:
09/167,614 →
Device for Operating a Controlled Member on a Rotary-Wing Aircraft, Particularly a Helicopter
Patent:
6,772,054 →
Application:
09/190,318 →
Device for Reducing the Vibration in the Cabin of a Rotary-Wing Aircraft, Especially a Helicopter
Patent:
6,067,853 →
Application:
09/190,369 →
Combined Altitude and Height-Above-Ground Indicator for an Aircraft
Patent:
6,204,779 →
Application:
09/191,371 →
Combined Altitude and Height-Above-Ground Indicator for an Aircraft
Patent:
6,232,890 →
Application:
09/191,372 →
Swash-Plate Device for Controlling the Pitch of Rotor Blades with Cylindrical Runners Sliding on Non-Rotating Pillars
Patent:
6,102,659 →
Application:
09/199,238 →
Device for Controlling an Aerodynamic Surface for Balancing a Helicopter in Terms of Pitch
Patent:
6,123,291 →
Application:
09/200,927 →
Swash-Plate Device for Controlling the Pitch of the Blades of a Rotor with Rotary Guided Parts on Slides Translated Along the Rotor Axis
Patent:
6,074,168 →
Application:
09/203,731 →
Method for Manufacturing a Variable-Pitch Composite Blade for a Helicopter Rotor
Patent:
6,056,838 →
Application:
09/207,352 →
Flight Control Indicator for Aircraft
Patent:
5,986,580 →
Application:
09/209,238 →
Device for Coaxially Coupling Two Shafts, Especially for a Helicopter
Patent:
6,168,530 →
Application:
09/211,502 →
Blade for Rotary Wing Aircraft
Patent:
6,142,738 →
Application:
09/216,920 →
Gyroplane Rotor with Double-Plate Hub and External Pitch Control
Patent:
6,203,277 →
Application:
09/242,218 →
Indicator for Monitoring the Path of an Aircraft in a Horizontal Plane
Patent:
6,111,525 →
Application:
09/244,957 →
Composite Material Variable Pitch Blade for Helicopter Rotor and Manufacturing Process of Such a Blade
Patent:
6,227,805 →
Application:
09/271,419 →
Flight Control System for an Aircraft, Particularly for a Helicopter,
Patent:
6,259,975 →
Application:
09/295,259 →
Simplified Anti-Vibration Suspension Device with Top Dampers for a Helicopter
Patent:
6,145,785 →
Application:
09/298,499 →
Simplified Anti-Vibration Suspension Device for a Helicopter
Patent:
6,164,915 →
Application:
09/298,553 →
Method and Device for Assistance with the Maintenance of an Aircraft, Especially of a Helicopter
Patent:
6,246,341 →
Application:
09/312,608 →
Detection Device
Patent:
6,191,689 →
Application:
09/312,612 →
System for Monitoring the Operation of an Aircraft, Especially a Helicopter
Patent:
6,400,282 →
Application:
09/312,613 →
System for Monitoring the Operation of an Aircraft, Especially a Helicopter
Patent:
6,150,959 →
Application:
09/312,710 →
Heating Device with Resistive Elements for an Aerodynamic Profile
Patent:
6,338,455 →
Application:
09/318,364 →
Rotor Aircraft Rotor Blade with Static and Dynamic Balancing Device and Balancing Process of a Blade
Patent:
6,196,066 →
Application:
09/351,077 →
De-Icing Connection Systems for Rotor Aircraft Rotor
Patent:
6,216,979 →
Application:
09/351,417 →
Blade Profile for Aircraft Rotor and Rotor Comprising Same
Patent:
6,361,279 →
Application:
09/355,353 →
Device for Aiding the Piloting of an Aircraft, Especially a Rotary-Wing Aircraft and in Particular a Helicopter
Patent:
6,255,965 →
Application:
09/401,855 →
Device and Process for Reducing the Vibration Generated on the Structure of a Rotary-Wing Aircraft, Particularly a Helicopter
Patent:
6,311,924 →
Application:
09/407,375 →
Device for Reducing the Vibration Generated on the Structure of a Rotary-Wing Aircraft
Patent:
6,279,704 →
Application:
09/407,718 →
Process and Device for Aiding the Maintenance of a Complex System, Especially an Aircraft
Patent:
6,219,597 →
Application:
09/407,957 →
Antivibration Device Intended to Reduce the Transmission of Vibration Between Two Bodies, and Applications
Patent:
6,247,684 →
Application:
09/458,668 →
Anti-Vibration Suspension Device Having a Torsion Spring, for a Helicopter
Patent:
6,283,408 →
Application:
09/468,166 →
Device for Assisting with Retrimming an Aircraft Control
Patent:
6,276,640 →
Application:
09/471,134 →
Aircraft flight control device
Patent:
6,338,454 →
Application:
09/572,439 →
Blade for the Rotary Wings of an Aircraft
Patent:
6,364,615 →
Application:
09/573,983 →
Anti-vibration suspension device with torsion springs between vibrators and structure, for a helicopter
Patent:
6,325,327 →
Application:
09/589,707 →
Device for Lubricating a Step-Up/Down Mechanical Assembly
Patent:
6,446,755 →
Application:
09/616,626 →
Indicator of a Variable for Aircraft
Process and Device for Reducing the Spectral Line Noise Inside an Aircraft, Especially a Rotating-Wing Aircraft, in Particular a Helicopter
Flight Control System for a Rotary-Wing Aircraft, Particularly for a Helicopter
Power Margin Indicator for a Rotary Wing Aircraft, Particularly a Helicopter
Process of Manufacturing a Shielded and Wear-Resistant Multi-Branch Harness
Rotor with Rotor Head Vibration Suppressor Comprising Vertical Pendulums
Rotary Wing Aircraft with Electric Pitch Control
Device for Lubricating a Power Gearbox with a Variable Orientation, Particularly for a Convertible Tilt-Rotor Aircraft
Flight Control Device for an Aircraft, in Particular for a Helicopter
Damping Structure and Applications
Aircraft, Particularly a Helicopter, Transmission System
Rotary-Wing Aircraft Rotors with Automatically Folding Blades and Electrical Connection Installation for the Blades
Rotary-Wing Aircraft Rotors with Manually Folding Blades and Electrical Connection Installation
Rotary-Wing Aircraft Rotors with Manually Folding Blades and Electrical Connection Installation
Bearing Assembly for a Helicopter Rear Transmission Shaft
Convertible Aircraft with Tilting Rotors
Patent:
6,607,161 →
Application:
10/070,629 →
Device and Process for Regulating the Power of the Engines of a Rotary Wing Multi-Engine Aircraft
Asymmetric Double Row Angular Contact Ball Bearing, and Cantilever Mounting of Gears on Such a Bearing
Soundproofing Panel' in Particular Structural or Lining Panel for a Rotorcraft
System for Lubricating and Cooling a Mechanical Assembly
Fluid Inertia Drag Damper for Rotary Wing Aircraft Rotor
System for Regulating the Output of an Engine of a Helicopter
Device for Lubricating a Step-Up/Down Mechanical Assembly
Structural Assembly of Part of an Aircraft and Aircraft, Particularly Rotary-Wing Aircraft, Comprising Such a Structural Assembly
Energy-Absorbing Connecting Strut for Use as a Gearbox Suspension Strut for Rotary Wing Aircraft
Device and System for the Automatic Control of a Helicopter
Pivoting Power Transmission Unit with Peripheral Face Toothed Gearwheels of the Face Gear Type
Automatic Control Device for a Helicopter and Automatic Control System Comprising Such a Device
Process and Device for Determining in Real Time the Behavior of a Craft, in Particular of an Aircraft
Test Bench for Testing a Power Transmission Device and a Test System Comprising Such a Test Bench Provided with a Power Transmission Device
Pivoting Transmission Unit with a Device to Take Up Play Along the Pivot Axis
Test Rig and Test System for Testing a Power Transmission Device
Dual Piston Drag Damper for Rotary-Wing Aircraft Rotor
Method and Apparatus for Folding/Unfolding the Blades of a Rotary-Wing Aircraft Rotor
Rotary-Wing Aircraft Rotor with Constant Velocity Drive
Device for Monitoring at Least One Pilot in a Cockpit of an Aircraft
Constant Velocity Drive Rotary-Wing Aircraft Rotor with Torque Splitting Differential
Device for Controlling the Pitch of the Blades of a Convertible Aircraft Rotor
Process and Device for Estimating at Least the Vertical Speed of an Aircraft, in Particular of a Rotary Wing Aircraft
Device for Aiding the Locating of Failure of a Complex System
Lubricating Installation for Rocking Power Transmission Box
Tilting Transmission Gearbox Comprising a Pivoting Connection with Plain Bearings
Method and Device for Detecting Defects of at Least One Rotary Wing Aircraf Rotor
Anti-Vibratory Device with Rotary Compensation Weights
Secure Interactive 3D Navigation Method and Device
High-Damping Absorbing Coating
Method and Device for Detecting Defects of Electromagnetic Protection for Electric Harnesses
Fabric Prepreg by Two Distinct Thermosetting Matrixes
Method and a Device for Assisting the Piloting of a Rotary Wing Aircraft in the Vicinity of a Landing or Takeoff Point
Pivoting Power Transmission Unit with Load Transfer via the Casing
System for Controlling the Torsional Stability of the Drivetrain of a Machine, in Particular of a Helicopter
A Device for Assisting an Airplane in Intercepting a Segment of a Flight Path Utilizing Positional and Ground Speed Indicators
Blade Pitch Control Disk Device for a Rotorcraft Rotor
Coupling Flange System for Hollow Shaft
Variable Pitch Rotor Blade for Shrouded Rotors, in Particular Helicopter Rotors
System for Lubricating and Cooling a Mechanical Assembly
Elastomeric Member Provided with Monitoring Means
Method of Tuning a Vibration Absorber
Fairing for the Rotor of a Rotorcraft
Modular Anti-Icing/De-Icing Device for an Aerodynamic Surface
Brake Device for the Rotor of a Helicopter or the Like, Associating a Main Brake Mechanism Having a Disk and a Secondary Brake Mechanism for Use in Strong Wind
Device for Providing Assistance to the Pilot of a Rotorcraft in the Event of Engine Failure
Device for Heating and/or Demisting a Vehicle
Vibration Absorber Device for a Seat in a Vehicle, in Particular an Aircraft or the Like
Convertible Aircraft Provided with Two Tilt Fans on Either Side of the Fuselage, and with a Non-Tilting Fan Inserted in the Fuselage
Device for Indicating the Vibration Level of a Vehicle
Method for Using a Steerable Tall Fin to Reduce the Vibration Generated on the Fuselage of a Helicopter
Method for Using a Tiltable Stabilizer to Reduce Vibration Generated on the Fuselage of a Helicopter
Two-Sweep Rotary Wing Blade with Limited Taper Ratio
Heater Mat Made of Electrically-Conductive Fibers
Electrical Connection for a Resistor Element Made of Electrically-Conductive Fibers
Method of Controlling Vibration Damping in a Helicopter, and Apparatus Implementing the Method
Method and Apparatus for Minimizing the Noise Emitted by a Rotorcraft During Take-Off and Landing
Composite Protection for Revealing Damage to a Core in a Vehicle Such as an Aircraft
Damping Structure and Applications
Transmission Mechanism Between Accessories and Engine Members for Driving the Rotor of a Rotorcraft, in Which the Accessories Are Drivable Selectively in Isolation or in Combination with the Rotor
Pilot Indicator for Predicting Changes in the Speed of Rotation of the Main Rotor of a Rotorcraft
Pilot Indicator for Predicting Changes in the Monitoring Parameters of a Gas Turbine Engine
Device for Indicating a Beat Level
Method of Adjusting at Least One Defective Rotor of a Rotorcraft
Optimized Method of Controlling Yaw for Rotary-Wing Aircraft, and a System for Implementing It
Coupling Capable of Accommodating Large Angular and Axial Displacements
Sum Integration Estimating of the Vertical Speed for a Rotary Wing Aircraft
Suspension System for a Rotary Wing Aircraft Engine
Active Suspension Method and Apparatus for a Rotary Wing Aircraft
On-Board System for Constructing an Aircraft Track
Autopilot System for a Helicopter
Two-Outlet Electromechanical Motor
System for Monitoring Damage to a Rotor Blade of a Rotary-Wing Aircraft
Device for Filtering Vibration Between Two Parts, and Applications Thereof
Method and Apparatus for Optimizing the Performance Envelope of an Engine
Device for Fastening Elongate Elements to a Structure
Method and Apparatus for Manufacturing a Helicopter Rotor Fairing, and a Fairing Obtained Thereby
Apparatus with Twisting Tool Having Cavities and Associated Retaining Parts for Manufacturing Electrical Harnesses
Method and Apparatus for Manufacturing Electrical Harnesses
Antivibration Device Having Rotary Flyweights and an Epicyclic Geartrain
Device for Locking a Structure for Securing a Blade to the Hub of a Rotorcraft Rotor
Torque Limiter Having Two Mechanical Inlets
Tooling for Manufacturing Large-Section Rigid Harnesses
Rotary Wing Aircraft with Undercarriage Structure
Auxiliary Nose Undercarriage, a Force-Transmission Structure, and a Rotary Wing Aircraft
Rotocraft Rotor with Hinged Blades and Lockable Retractable Flapping Abutments
Device for Supporting an Aircraft Battery
Anti-Crash Method and System, an Undercarriage, and an Aircraft
System for Estimating the Speed of an Aircraft, and an Application Thereof to Detecting Obstacles
Method and Apparatus for Assisting the Piloting of an Aircraft at Low Altitude
Centrifugal-Effect Vibration Generator Having Coaxial Contrarotating Rotors
Reconfigurable Interconnection Device for Electrical Bundles
Protection System, a Bellows Hinge, and an Aircraft
Method of Optimizing the Performance Envelope of a Turbine Engine
Auxiliary Nose Undercarriage, a Force-Transmission Structure, and a Rotary Wing Aircraft
Method of Selectively Decoupling Solidborne Noise, a Laminated Ball Joint, a Mechanical Connection, and an Aircraft
Method and a System for Setting into Coincidence, a Technique, a Drive Device, and an Aircraft
Method and a Device for Blocking the Pitch of a Foldable Blade of a Rotorcraft Rotor
Rotorcraft Rotor with Blades Hinged in Flap and in Lag
Method and Apparatus for Diagnosing a Mechanism
Rotorcraft Blade Provided with a Flap That Is Tiltable with the Help of at Least One Main Ball Joint Having a First Shaft That Is Secured to Said Flap
Rotorcraft Blade Provided with a Tiltable Flap and a Fastener Tongue
Rotorcraft Rotors Having Twistable Blades
Removable Sensor Support for a Hollow-Rotor Helicopter
Anti-Impact Shield for a Mechanical Part
Rotary Flap
Servo-Control System for an Unbalanced Rotor Vibrator
On-Board Thermostat and a System for Detecting Excess Temperature
Device and System for Assistance Within Interception by an Aircraft of a Flight Path Segment
Aerially Transportable Tank for Storing a Composition for Discharging in Flight
Rotorcraft Skid Undercarriage and a Rotorcraft Including Such an Undercarriage
Composite Anti-Crash Structure with Controlled Buckling for an Aircraft
Method and a System for Detecting and Locating an Adjustment Error or a Defect of a Rotorcraft Rotor
Method and a Device for Processing and Displaying Aircraft Piloting Information
Shielded Electrical Harness with an Angled Connector, and Its Method of Fabrication
Method and a Device for Performing a Check on the State of Health of a Turbine Engine of a Twin-Engined Rotorcraft
Method and a Device for Providing Assistance in Piloting a Rotorcraft at Takeoff
Power Plant for a Rotary Wing Aircraft
Method of Detecting Suspended Filamentary Objects by Telemetry
Method and a Device for Measuring the Speed of an Aircraft, in Particular a Rotorcraft at Low Speed
Electrical Connection Between First and Second Metal Parts That Are Electrically Insulated from Each Other
Absorbent Structure for Attenuating Noise in Particular by a Rotor-Generator Noise, and a Rotor Duct Including Such a Structure
Device for Assisting in Piloting a Hybrid Helicopter, a Hybrid Helicopter Provided with Such a Device, and a Method Implemented by Said Device
Related Assignments
(2)
Other recorded transfers of the patents in this record — the chain of ownership.