Patent Assignment
Reel/Frame 027015/0397
Change of Name
Recorded: 2011-10-04
Pages: 12
Assignor
MESSIER-BUGATTI
Executed: 2011-04-30
Assignee
MESSIER-BUGATTI-DOWTY
INOVEL PARC SUD, VELIZY VILLACOUBLAY, 78140, FRANCE
Covered Properties
(88)
Device for Controlled Braking of a Wheel Train with Temperature Comparison
Patent:
5,217,282 →
Application:
07/831,676 →
Safety Locking Device Having a Rocking Hook
Patent:
5,257,840 →
Application:
07/949,134 →
Safety Locking Device Having a Tilting Hook
Patent:
5,344,197 →
Application:
07/968,403 →
System for Powering the Driving Actuator of an Aircraft Undercarriage
Patent:
5,284,083 →
Application:
07/979,256 →
Catch Device for Locking Aircraft Landing Gear in the Raised Position
Patent:
5,288,037 →
Application:
08/011,856 →
Method of Burnishing Metal Parts, in Particular Light Alloy Wheels, and Apparatus for Implementing Said Method
Patent:
5,329,684 →
Application:
08/014,737 →
Method of Controlling an Electrohydraulic Braking Apparatus for an Aircraft Wheel Set, and an Apparatus for Implementing Said Method
Patent:
5,417,477 →
Application:
08/187,913 →
Electro-Hydraulic Braking System for the Wheels of an Aircraft
Patent:
5,397,173 →
Application:
08/207,178 →
Reinforcement Device for Carbon Brake Disks, and a Brake Disk Fitted with Such Devices
Patent:
5,560,452 →
Application:
08/436,860 →
Safety Device for a System Transported on Board a Vehicle, in Particular an Aircraft
Patent:
5,538,117 →
Application:
08/436,865 →
Arrangement of Carbon Brake Disks for an Aircraft Brake Unit and a Method of Assembling Disks in Such an Arrangement
Patent:
5,992,577 →
Application:
08/959,987 →
Apparatus for Braking a Set of Aircraft Wheels
Patent:
6,193,326 →
Application:
09/227,191 →
Axial Piston Pump of the Type Having Intersecting Axes
Architecture for the Hydraulic Braking System of an Aircraft
Safety Locking Device for Electromechanical Equipment and Aircraft Wheel Brake Equipped Therewith
Latch Device, in Particular for Latching an Airplane Landing Gear or an Airplane Landing Gear Hatch
Latch Device, in Particular for Latching an Airplane Landing Gear or an Airplane Landing Gear Hatch, and a Method of Operating Said Device
Hydraulic System Architecture for Controlling Steering
Hydraulic System Architecture for Controlling Steering
Hydraulic Circuit Architecture
Passive device for increasing the transmission efficiency of radio-frequency systems
Brake System for Braking Aircraft Wheels
Electromagnetic Brake
Device Providing Protection Against Untimely Braking
Actuator for an Electromechanical Brake, a Brake Including Such an Actuator, a Vehicle Including at Least One Such Brake, and a Method of Implementing Said Actuator
Landing Gear, a Brake, a Brake-and-Wheel Assembly for an Airplane, and a Method of Maintaining Such Landing Gear
Method of Managing Brake System Architecture for an Airplane Fitted with Brakes Having Electromechanical Actuators, and an Architecture Applying the Method
Electromechanical Actuator for a Vehicle Brake, the Vehicle Brake Including Such an Actuator, and a Method of Maintaining Such an Actuator
Architecture for an Airplane Braking System Including Two Computers and Capable of Withstanding Two Breakdowns, and a Method of Managing Such an Architecture
Protection method in a vehicle brake system having electric brakes
Application:
11/117,353 →
Publication:
US 2006/0152080
Apparatus for Preventing Untimely Braking in a Brake Having Electromechanical Actuators
Method of Servo-Control in a Braking System Having Electric Brakes
Distributed Architecture for a System for Managing Aircraft Landing Gear
A Tachometer with Independently Mountable Rotary and Stationary Parts for an Aircraft Wheel
Method of Servo-Control in a Braking System Having Electric Brakes
Method of Managing an Electromechanical Brake Actuator in Particular for Aircraft
Electromechanical aircraft brake with tiltable actuators
Force-Measurement Cell and a Connection Pin Fitted with Such a Cell
Aircraft Undercarriage Including a Plurality of Electromechanical Actuators, and a Method of Testing It
Axle End Equipment for a Vehicle, in Particular an Aircraft
Telescopic Actuator with a Main Rod and an Auxiliary Rod, and a Method Making Use Thereof
Method of Managing the Braking of an Aircraft by Predicting Its Movements on an Airport
Power Distribution Architecture for Actuating Moving Elements of an Aircraft in Sequence
Passive Device for Increasing the Transmission Efficiency of Radio-Frequency Systems
Hydraulic control valve in the form of a cartridge
Application:
11/798,840 →
Publication:
US 2007/0267078
Architecture for a Hydraulic System for Operating Aircraft Landing Gear
Architecture for a Hydraulic System for Operating Aircraft Landing Gear
Wheel-and-brake assembly for aircraft
Application:
11/878,821 →
Publication:
US 2008/0302613
Aircraft Brake Particularly Adapted for Mounting on a Conical Axle
Method of Distributing Braking Within at Least One Group of Brakes of an Aircraft
Method of Adaptive Braking Control for a Vehicle
Method for Managing the Wheel Steering Control of an Aircraft
Electromechanical Actuator for a Vehicle Brake, the Vehicle Brake Including Such an Actuator, and a Method of Maintaining Such an Actuator
Method of Controlling a Vehicle Brake with Torque Correction
Device for Connecting a Tire of an Aircraft Wheel to a Pneumatic Unit of the Aircraft
Method of Feeding Energy to Actuators Associated with an Aircraft Undercarriage
Method of Distributing Braking Between the Brakes of an Aircraft
Method of Managing the Power Supply to a Non-Reversible Actuator for a Vehicle Wheel Brake
Method of Controlling a Vehicle Brake with Compensation for Expansion
Aircraft Filter Device with a Member for Keying and Driving the Cartridge
Cartridge Filter for Aircraft
Actuator with a Main Rod and an Auxiliary Rod
Method of Collecting Information Relating to a Movable Airfoil Surface of an Aircraft
Application:
12/438,633 →
Publication:
US 2009/0289147
Method of Surface Treating a Mechanical Part Made of High-Strength Steel, and a Sealing System Obtained by Implementing Said Method
Telescopic Actuator with a Main Rod and an Auxiliary Rod
Application:
12/566,307 →
Publication:
US 2010/0071490
Wheel Bar and a Wheel Specially Adapted Therefor
Stabilizer for Stabilizing the Disks of a Heat Pack, in Particular When the Heat Pack Is Packaged in a Container
Container for Receiving a Stack of Brake Disks, in Particular Aircraft Brake Disks
Application:
12/623,174 →
Publication:
US 2010/0122922
Power Distribution Architecture for Distributing Power to Electromechanical Actuators of an Aircraft
Method of Controlling a Vehicle Brake with Adaptive Torque Correction
Method of Managing the Steering Control of an Aircraft Undercarriage
Method of Taxiing an Aircraft
Braking System Architecture for an Aircraft Fitted with Electromechanical Brakes
Mechanically-Operating Actuator with Hydraulic Damping
Control Network for Single- or Multi-Motor Actuators, the Network Being Particularly Adapted to Aviation Applications Such as Powering the Motors of Landing-Gear Hook Units
Architecture for an Electromechanical Braking System
Power Supply Architecture for Aircraft Brakes Fitted with Electromechanical Actuators
Locking Device with Catches and a Rotary Locking Sleeve
Method of Managing the Braking of an Aircraft, and a Corresponding Braking System
Aircraft Wheel-and-Brake Set Fitted with a Rotary Drive Device
Method of Managing Parking Braking in a Braking System for a Vehicle Fitted with Electric Brakes
An Asymmetrical Electric Braking Architecture for Aircraft
Electric Braking Circuit Provided with Means for Controlling Members for Blocking the Pushers of Electromechanical Actuators Fitted to an Aircraft Brake
Application:
12/996,280 →
Publication:
US 2011/0079471
Hydraulic Braking Architecture for Aircraft Having Brakes with Half-Cavities
Application:
13/019,787 →
Publication:
US 2011/0187180
Method of Managing a Ground Connection of an Aircraft
Method of Managing a Turning Movement of an Aircraft Taxiing on the Ground
Device for Connecting a Tire of an Aircraft Wheel to a Pneumatic Unit of the Aircraft
Electric Actuator Including Two Current-Controlled Voltage Inverters Powering an Electric Machine, and Reconfigurable in the Presence of a Defect
Related Assignments
(2)
Other recorded transfers of the patents in this record — the chain of ownership.