Aircraft high-lift device brake apparatus, distributed high-lift device brake systems, and methods of actuating such distributed high-lift device brake systems, where each high-lift device brake apparatus includes an extendable high-lift device, an actuator coupled to the high-lift device that can extend or retract the extendable high-lift device, a torque tube coupled to a remote drive unit so that rotation of the torque tube activates the actuator, and a high-lift device brake that includes, in turn, a brake assembly capable of locking the associated high-lift device in its current position, a torque-based brake activator configured to activate the brake assembly when an applied torque exceeds a predetermined threshold, and a flight control brake activator configured to activate the brake assembly when the flight control brake activator receives an activation signal from the flight control system of the aircraft.
DISTRIBUTED ACTIVE BRAKES FOR AIRCRAFT HIGH-LIFT DEVICES
25.11.2021
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Distributed active brakes for aircraft high-lift devices
Europäisches Patentamt | 2022
|Active cooling of aircraft brakes
Tema Archiv | 2011
|Engineering Index Backfile | 1929
MONITORING HEALTH OF SAFETY BRAKES IN AUXILIARY LIFT DEVICES
Europäisches Patentamt | 2021
|Monitoring health of safety brakes in auxiliary lift devices
Europäisches Patentamt | 2023
|