Patent Assignment
Reel/Frame 040851/0908
Change of Name
Recorded: 2016-12-08
Pages: 14
Assignor
MESSIER-BUGATTI-DOWTY
Executed: 2016-06-28
Assignee
SAFRAN LANDING SYSTEMS
7, RUE GÉNÉRAL VALÉRIE ANDRÉ, INOVEL PARC SUD, VELIZY VILLACOUBLAY, 78140, FRANCE
Covered Properties
(216)
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 →
Method for Densifying the Edges and Surfaces of a Preform Using a Liquid Precursor
Patent:
5,981,002 →
Application:
09/020,523 →
Apparatus for Braking a Set of Aircraft Wheels
Patent:
6,193,326 →
Application:
09/227,191 →
Friction Element in Composite Carbon/Carbon-Silicon Carbide Material and Method for Manufacturing Same
Patent:
6,221,475 →
Application:
09/284,402 →
Method for Producing Ring-Shaped Fibrous Structures, in Particular for Making Parts in Composite Material
Patent:
6,319,348 →
Application:
09/381,943 →
Composite Foam, Articles, and Methods of Formation
Patent:
6,726,962 →
Application:
09/857,949 →
System for Automatically Controlling the Spreading of a Textile Sheet
System for Presenting a Textile Sheet Automatically
Axial Piston Pump of the Type Having Intersecting Axes
Smooth-table circular needling machine
Patent:
6,367,130 →
Application:
09/900,260 →
Feeding a needling machine with a continuous spiral strip
Patent:
6,363,593 →
Application:
09/900,275 →
Method of monitoring the needling of fiber structures in real time, and needling apparatus for implementing the method
Patent:
6,360,412 →
Application:
09/900,276 →
Circular needling machine provided with a device for automatically removing preforms
Patent:
6,347,440 →
Application:
09/900,372 →
Architecture for the Hydraulic Braking System of an Aircraft
Wheel Assembly Provided with a Pressure Sensor
Method for Densifying Porous Substrates by Chemical Vapour Infiltration with Preheated Gas
Gas Preheater and Process for Controlling Distribution of Preheated Reactive Gas in a Cvi Furnace for Densification of Porous Annular Substrates
Patent:
6,572,371 →
Application:
10/139,553 →
Method and Installation for Advancing a Needled Fiber Plate
Safety Locking Device for Electromechanical Equipment and Aircraft Wheel Brake Equipped Therewith
Method and an Installation for Subjecting Carbon Fabrics to High Temperature Heat Treatment and to Densification by Chemical Vapor Infiltration
Making a Needled Fiber Preform for Fabricating a Composite Material Part
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
Aircraft Landing Gear Having an Independent Low-Noise Fairing System
Hydraulic System Architecture for Controlling Steering
Hydraulic System Architecture for Controlling Steering
Wheel Arrangement Having a Pressure Sensor
Hydraulic Circuit Architecture
Passive device for increasing the transmission efficiency of radio-frequency systems
Wheel Assembly Equipped with a Tachometer
Actuator with Torque Limiter
Actuator with Two Motors, a Differential Reducer and a Torque Limiter
One Piece Shim
Controlling or Modeling a Chemical Vapor Infiltration Process for Densifying Porous Substrates with Carbon
Brake System for Braking Aircraft Wheels
Composite Articles
Electromagnetic Brake
One Piece Shim
Method of Fabricating a Helical Two-Dimensional Fiber Sheet
Retractable Landing Gear for Aircraft
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
Clutch or Brake Device Formed of Composite Foam
Landing Gear Having a Gas Vessel, and Methods of Maintaining Such Landing Gear
Method of Measuring the Compression of a Shock Absorber, and an Airplane Undercarriage Constituting an Application Thereof
Apparatus for Preventing Untimely Braking in a Brake Having Electromechanical Actuators
Method of Servo-Control in a Braking System Having Electric Brakes
Deep Hole Boring Head and Deep Hole Boring Method for Boring a Production Piece
Distributed Architecture for a System for Managing Aircraft Landing Gear
Method of Fabricating a Helical Fiber Sheet
A Tachometer with Independently Mountable Rotary and Stationary Parts for an Aircraft Wheel
Fabricating Three-Dimensional Annular Fiber Structures
Method of Servo-Control in a Braking System Having Electric Brakes
Device and Method for Determining the Weight and/or a Characteristic Value of the Position of the Centre of Gravity of an Aircraft
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
Method of Fabricating a Lug on a Structural Element of Composite Material, in Particular a Connecting Rod
Method of Fabricating a Composite Material Connecting Rod
Telescopic Actuator with a Main Rod and an Auxiliary Rod, and a Method Making Use Thereof
Sealing Device for a Gas Inlet to an Oven or the Like
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
Method of Making a Fiber Preform for Manufacturing Parts of a Composite Material of the Carbon/Carbon Type Incorporating Ceramic Particles, and Products Obtained Thereby
Architecture for a Hydraulic System for Operating Aircraft Landing Gear
Architecture for a Hydraulic System for Operating Aircraft Landing Gear
Aircraft Brake Particularly Adapted for Mounting on a Conical Axle
Method of Distributing Braking Within at Least One Group of Brakes of an Aircraft
Compact Shock Absorber for an Aircraft Undercarriage, and an Undercarriage Including Such a Shock Absorber
Telescopic Member Having an Overridable Internal Abutment
Method of Adaptive Braking Control for a Vehicle
Method for Managing the Wheel Steering Control of an Aircraft
Method of Fabricating Carbon Fiber Reinforced Composite Material Parts
Electromechanical Actuator for a Vehicle Brake, the Vehicle Brake Including Such an Actuator, and a Method of Maintaining Such an Actuator
Brace-Locking Device for an Aircraft Undercarriage
Method of Controlling a Vehicle Brake with Torque Correction
Edge Densification for Film Boiling Process
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 Densifying Porous Articles
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
Active Element for an Electromagnetic Machine, a Method of Fabricating Such an Active Element, and an Electromagnetic Machine Including Such an Active Element
Power Control for Densification of One or More Porous Articles
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
Heat Treatment Oven with Inductive Heating
Friction Device for Controlling Force, and a Friction Damper Comprising Such a Device
3D Composite Fabric
Method of Surface Treating a Mechanical Part Made of High-Strength Steel, and a Sealing System Obtained by Implementing Said Method
Method of Fabricating a Friction Part Out of Carbon/Carbon Composite Material
Power Supply with Two Series Inverters for a Polyphase Electromechanical Actuator
Method of Making Composite Material Stiffeners
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
Power Distribution Architecture for Distributing Power to Electromechanical Actuators of an Aircraft
Part Based on C/C Composite Material, and a Method of Fabricating It
Shock-Absorber for Aircraft Landing Gear
Mechanical Component Comprising an Insert Made of Composite
Mechanical Component Comprising an Insert Made of Composite
Method of Controlling a Vehicle Brake with Adaptive Torque Correction
Method of Managing the Steering Control of an Aircraft Undercarriage
Apparatus and Method of Densifying Porous Articles
Method of Taxiing an Aircraft
Braking System Architecture for an Aircraft Fitted with Electromechanical Brakes
Mechanically-Operating Actuator with Hydraulic Damping
Process for Manufacturing a Metal Part Reinforced with Ceramic Fibres
Method for Making Parts with an Insert Made of a Metal-Matrix Composite Material
Process for Manufacturing a Metal Part Reinforced with Ceramic Fibres
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 Fabricating a Friction Part Based on C/C Composite Material
Circular Needling Machine Fed with a Fiber Sheet by a Conveyor and a Vertical Chute
Aircraft Wheel-and-Brake Set Fitted with a Rotary Drive Device
Circular Needling Table for Needling a Textile Structure Made from an Annular Fiber Preform
Method of Managing Parking Braking in a Braking System for a Vehicle Fitted with Electric Brakes
An Asymmetrical Electric Braking Architecture for Aircraft
Unlocking of a Stabilizing Member of a Folding Strut of Aircraft Landing Gear
Process for Manufacturing a Structural Part Made of an Organic Matrix Composite and Part Obtained
Electrohydraulic Actuator with a Pump Incorporated in the Piston
Method for Producing a Metallic Part Comprising Inner Reinforcements Consisting of Ceramic Fibers
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
Device for Retracting Aircraft Landing Gear
Multifunctional Electromechanical Device for Landing Gear
Method of Connecting a Composite Material Structural Element to a Tube
Hydraulic Valve
Independent Drive Device for an Aircraft
Aircraft Fitted with an Independent Drive Device
Method of Controlling the Yawing Movement of an Aircraft Running Along the Ground
Method of Managing Movement of an Aircraft on the Ground
Controlled-Friction Linear Device in Which a Press Force Is Applied Perpendicular to the Movement
Controlled-Friction Sliding Device, Such as a Damper, Which Can Operate in Two Directions
Mechanical Device for the Transmission of a Force with a Threshold
Selective Force Transmission Device and an Undercarriage Consisting of an Application Thereof
Device for Reducing Aerodynamic Noise from an Aircraft Undercarriage
Method for Manufacturing a Composite Material Connecting Rod Having Reinforced Ends
Hydraulic Circuit for Actuating an Undercarriage, and Methods of Deploying and Raising an Undercarriage Using Such a Circuit
Method of Making a Three-Dimensional Fiber Preform for Fabricating an Annular Part Out of Carbon/Carbon Composite Material
Method of Controlling a Brushless Dc Motor
Device for Braking/Driving an Aircraft Wheel
Electromechanical Telescopic Actuator
Electromechanical Actuator with Dual Excitation
Method of Limiting a Current Supplied by a Dc Power Supply
Method for Operating a Landing Gear Assembly with a Breaker Strut
Nose Gear of an Aircraft Comprising a Single Control Device for Retraction and Steering
Tool for Removing Annular Elements Tightly Mounted in Holes, in Particular Blind Holes, of Parts
Method for Manufacturing a Fiber-Reinforced Metal Connecting Rod, and Resulting Connecting Rod
Hydraulic Brake Architectures for Aircrafts for Braking at Least One Wheel of the Aircraft
Method of Controlling a Cooling Device for a Machine Tool
Hydraulic Actuator with Automatic Purging at the End of Its Stroke
Method for Distributing Braking Torque Between Braked Wheels Fitted to at Least One Undercarriage of an Aircraft
Method for Powering Autonomous Drive Motors for an Aircraft
Telescopic Actuator
Method for Making a Composite Metal Part Having Inner Reinforcements in the Form of Fibers, Blank for Implementing Same and Metal Part Thus Obtained
Method for Manufacturing Composite Parts Comprising Braided Fibers
Aircraft Landing Gear of the Rocker-Arm and Deformable-Parallelogram Type
Method of Controlling the Steering of a Steerable Portion of an Aircraft Undercarriage
Method of Managing the Steering of Aircraft Wheels, in Particular in the Event of a Tire Bursting or Deflating
Method for Operating a Machine for Plaiting Reinforcing Fibers
Method of Protecting an Aircraft Landing Gear While the Aircraft Is Being Towed, and Pin for Coupling a Towing Bar to an Orientable Lower Part of a Landing Gear
Method for Managing a Braking System for an Aircraft Fitted with Electromechanical Brakes
Device for Manoeuvring, on the Ground, a Door of an Aircraft Landing Gear
Method for Manufacturing an Arm in Composite Material Comprising a Transversal Bearing Designed to Receive a Fixed or Rotating Shaft
Method of Manufacturing an Elongate Insert Made of a Metal Matrix Composite
Hydraulically Regulated Electromagnetic Actuator, and Landing Gear Fitted with Such an Actuator for Controlling Same
Device for Connecting a Gearmotor to an Aircraft Wheel in Order to Enable the Wheel to Be Driven Selectively by the Gearmotor
Method of Extending Aircraft Undercarriages in Emergency Mode
Method of Resetting the Orientation of an Aircraft Undercarriage Having a Steerable Bottom Portion
Method of Managing the Braking of an Aircraft to Limit Its Pitch
A Device for Unlocking an Undercarriage in a Deployed Position, and an Undercarriage Fitted with Such a Device
Main Landing Gear of an Aircraft, Comprising Two Walking Beams Joined to the Structure of the Aircraft in an Articulated Manner
Device for Selectively Connecting a Gearmotor to an Aircraft Wheel to Enable the Wheel to Be Driven Selectively by the Gearmotor
Method of Managing Parking Braking in a Braking System for a Vehicle Fitted with Electric Brakes
Control Box
Method of Managing a Steering Command for a Steerable Portion of Aircraft Landing Gear
Electric Brake for an Aircraft Wheel, the Brake Including an Electromechanical Actuator Fitted with a Temperature Sensor
Electromechanical Braking System for an Aircraft
Process for Manufacturing a Mechanical Member Made of a Composite Having Increased Mechanical Strength
Coupling Device Between Two Rotary Elements
Method of Using and Renovating a Disk from a Stack of Disks of a Vehicle Brake
Brake for an Aircraft Wheel
Module for Converting Voltage Between a High-Voltage Electrical Network of an Aircraft and an Energy Storage Element
Method for Braiding Reinforcing Fibres with Variation in the Inclination of the Braided Fibres
Equipment for Measuring the Inflation Pressure of a Tire of a Vehicle Wheel
Device and Method for Spreading a Cable of Carbon Fibers or Carbon Yarns
Aircraft Wheel with a Universal Drive Dog
Electromechanical Braking System Architecture
System for Maintaining a Pressing Force by the Combined Action of Two Members
Method of Managing the Braking of an Aircraft
Aircraft Wheel Fitted with Drivekey-Bolts
Method of Managing the Braking of an Aircraft
Process for Manufacturing a Composite, Generally Triangular, Structural Part
Method for Manufacturing a Structural Part Made of a Composite Material and Including a Radially Oriented Double Yoke
Anti-Lofting Deflector for Aircraft Landing Gear
Drive Device Using Needles to Drive a Helical Fiber Sheet for Needling
Method of Using and Renovating a Disk from a Stack of Disks
Device for Driving an Aircraft Wheel in Rotation
Control Box
Braking Actuator for a Hydraulic Brake of an Aircraft Wheel
Aircraft Wheel
Method for the Reconditioning and Use of Brake Discs of the Rear Stator Type with Studs, Assembled Disc and Corresponding Stack of Discs
Method of Controlling an Electric Motor for Driving Rotation of an Aircraft Wheel
Brake Actuator for an Aircraft Wheel Hydraulic Brake
Related Assignments
(3)
Other recorded transfers of the patents in this record — the chain of ownership.
Assignment of Assignor's Interest
Jan 28, 2010
From: SNECMA PROPULSION SOLIDE
To: MESSIER-BUGATTI
Reel/Frame 023861/0622 →
Change of Name
Nov 14, 2012
From: MESSIER-BUGATTI
To: MESSIER-BUGATTI-DOWTY
Reel/Frame 029295/0838 →
Change of Name
May 6, 2018
From: SAGEM DÉFENSE SÉCURITÉ
To: SAFRAN ELECTRONICS & DEFENSE
Reel/Frame 046082/0606 →