发明名称 |
ELECTRIC FLIGHT CONTROL SYSTEM FOR AIRCRAFT ELEVATORS |
摘要 |
<p>The invention relates to an electric flight control system for aircraft elevators. According to the invention, the flight control system can be controlled in terms of load factor or rate of pitch. The inventive system comprises built-in protections in relation to load factor, incidence and pitch attitude.</p> |
申请公布号 |
WO2006024745(A1) |
申请公布日期 |
2006.03.09 |
申请号 |
WO2005FR01950 |
申请日期 |
2005.07.27 |
申请人 |
AIRBUS FRANCE;LAVERGNE, FABIEN;VILLAUME, FABRICE |
发明人 |
LAVERGNE, FABIEN;VILLAUME, FABRICE |
分类号 |
B64C13/50;G05D1/06;(IPC1-7):G05D1/06 |
主分类号 |
B64C13/50 |
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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