发明名称 ASSEMBLY AND METHOD FOR OPERATING ROTATABLE MEMBER AROUND ROTARY SHAFT ROTATABLY, AIRCRAFT, ASSEMBLY FOR CONTROLLING AIRCRAFT, AND CANARD ASSEMBLY FOR AIRCRAFT
摘要 PROBLEM TO BE SOLVED: To provide a device and a method for operating a rotatable member. SOLUTION: In one embodiment, the assembly for operating the rotatable member includes an extendable actuator having a first end part and a second end part and a driving member having a first part pivotally coupled to the second end part and a second part non-pivotally coupled to the rotatable member. The second part of the driving member is arranged apart from the first part. The driving member has a third part arranged apart from the first and second parts in orientation in which they are not arranged in parallel in the same linear order. This assembly includes a reaction link having a fixed end pivotally coupled to the first end part of the extendable actuator and a driving end pivotally coupled to the third part of the driving member. COPYRIGHT: (C)2005,JPO&NCIPI
申请公布号 JP2004323012(A) 申请公布日期 2004.11.18
申请号 JP20040133508 申请日期 2004.04.28
申请人 BOEING CO:THE 发明人 JONES KELLY T
分类号 B64C13/24;B64C1/00;B64C5/04;B64C5/16;B64C9/02;B64C13/30;B64C39/12;(IPC1-7):B64C13/24 主分类号 B64C13/24
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