发明名称 GEAR RETRACT BRAKING SYSTEM AND METHOD
摘要 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 t he landing gear wheels and landing gear position. The control component generat es braking instructions based on the monitored speed of the wheels and position of the landing gear.
申请公布号 CA2446515(A1) 申请公布日期 2004.05.06
申请号 CA20032446515 申请日期 2003.10.24
申请人 THE BOEING COMPANY 发明人 SUNDQUIST, BETH L.;MAXWELL, SCOTT D.;GOWAN, JOHN J.;NGUYEN, TU-LUC H.
分类号 B64C25/10;B64C25/42;B64C25/44;(IPC1-7):B64C25/42 主分类号 B64C25/10
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