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发明名称
FAIL-SAFE ADJUSTMENT SYSTEM FOR ADJUSTING SERVO TABS OF AN AIRCRAFT, COMPRISING A CONTROL MECHANISM WITH A FIXED ROTATIONAL AXIS AND ASSOCIATED CONTROL METHOD
摘要
申请公布号
EP2328806(B1)
申请公布日期
2012.09.19
申请号
EP20090741872
申请日期
2009.05.05
申请人
AIRBUS OPERATIONS GMBH
发明人
RICHTER, MARTIN;FLEDDERMANN, ANDREAS
分类号
B64C13/42
主分类号
B64C13/42
代理机构
代理人
主权项
地址
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