Gear retract braking system and method

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 25/42 (2006.01) B64C 25/10 (2006.01) B64C 25/44 (2006.01)

Patent

CA 2446515

A method and system for braking aircraft landing gear wheels after initialization of landing gear retraction. The system includes monitors, controlling components, measurement components, a fault recording memory, fault annunciation components, wheel braking system and brakes. The monitors monitor speed of the landing gear wheels and landing gear position. The control component generates braking instructions based on the monitored speed of the wheels and position of the landing gear.

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