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
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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 |
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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