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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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