#B64C25/44

ELECTROMECHANICAL BRAKE INTERLOCK

An electromechanical brake system is disclosed herein. The electromechanical brake system includes an electromechanical brake actuator, an electronic brake actuator controller coupled to the electrome…

DRIVE·Feb 19·1 min read

B64C25/44 GOODRICH CORPORATION

HYBRID BRAKE SYSTEMS AND METHODS FOR LOAD CELL CALIBRATION

A braking system for an aircraft may comprise: a brake assembly; a hydraulic braking subsystem having a hydraulic brake actuator configured to operate the brake assembly; an electric braking subsystem…

DRIVE·Aug 10·1 min read

B64C25/44 GOODRICH CORPORATION

HYBRID BRAKE SYSTEMS AND METHODS

A braking system for an aircraft is disclosed herein. The braking system may comprise: a brake assembly; a hydraulic braking subsystem having a hydraulic brake actuator configured to operate the brake…

DRIVE·Aug 10·1 min read

B64C25/44 GOODRICH CORPORATION

AIRCRAFT HYDRAULIC BRAKING SYSTEM AND METHOD OF CONTROLLING SAME

An aircraft hydraulic braking system having at least one hydraulic accumulator and a brake actuator. The at least one hydraulic accumulator is the sole source of pressurised hydraulic fluid in the air…

DRIVE·Mar 30·1 min read

B64C25/44 Airbus Operations Limited

MODIFIED BRAKING SYSTEMS AND METHODS DURING TAXI

A method of taxiing an aircraft may comprise: determining, via a brake controller, whether the aircraft is taxiing with a first thrust provided from a first side of the aircraft, a second thrust from …

DRIVE·Mar 2·1 min read

B64C25/44 GOODRICH CORPORATION

CONTROLLER FOR AN AIRCRAFT SYSTEM

A controller for an aircraft system of an aircraft, the aircraft system including a first actuator and a first energy supply. The controller is configured to, when the aircraft system is configured in…

DRIVE·Sep 1·1 min read

B64C25/44 AIRBUS OPERATIONS LIMITED

WHEEL BRAKING DEVICE

The invention relates to a device for braking a wheel, the device comprising: According to the invention, the control system is arranged to interrupt control of the first actuator or control of the se…

DRIVE·Aug 25·1 min read

B64C25/44 SAFRAN LANDING SYSTEMS

CONTROLLER FOR AN AIRCRAFT BRAKING SYSTEM

A controller for a hydraulic braking system for an aircraft is disclosed. The hydraulic braking system includes a first accumulator and a second accumulator, the controller configured to: receive firs…

DRIVE·Aug 25·1 min read

B64C25/44 AIRBUS OPERATIONS LIMITED

HYDRAULIC BRAKE SYSTEM

A brake system may comprise a hydraulic brake system or a hybrid brake system. The hydraulic brake system may include an inner axle disposed in an inner axle housing. The inner axle housing may includ…

DRIVE·Jul 29·1 min read

B64C25/44 GOODRICH CORPORATION

AIRCRAFT BRAKE SYSTEM

A braking system is disclosed. In various embodiments, the braking system includes a brake stack; an actuator configured to apply a compressive load to the brake stack; a servo valve coupled to a powe…

DRIVE·Jun 17·1 min read

B64C25/44 GOODRICH CORPORATION

BRAKING SYSTEM ARCHITECTURE FOR AIRCRAFT

A braking system architecture for aircraft, the architecture comprising: a brake including friction members and electromechanical actuators for exerting a braking torque on the wheel; a computer situa…

DRIVE·Jun 28·1 min read

B64C25/44 SAFRAN LANDING SYSTEMS

ELECTRIC BRAKING SYSTEM WITH POWER CONSERVATION AND METHOD OF OPERATING THE SAME

A method of operating electric brakes () on an aircraft () in a low power mode of operation includes determining if the aircraft is in a first configuration, if the aircraft is in the first configurat…

DRIVE·Feb 4·1 min read

B64C25/44 BOMBARDIER INC.

METHOD AND DEVICE FOR CONTROLLING AT LEAST ONE ACTUATOR CONTROL SYSTEM OF AN AIRCRAFT, RELATED COMPUTER PROGRAM PRODUCT AND AIRCRAFT

This method makes it possible to control an actuator control system of an aircraft to act on a force applied to the aircraft. The aircraft has an airspeed vector and a ground speed vector, and it comp…

DRIVE·Dec 23·2 min read

B64C25/44 THALES SA [FR]