发明授权
- 专利标题： Orbital maneuvering vehicle end effectors
- 专利标题（中）： 轨道机动车终端执行器
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申请号： US942159申请日： 1984-12-16
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公开(公告)号： US4718709A公开(公告)日： 1988-01-12
- 发明人: W. Neill Myers , John C. Forbes , Wayne L. Barnes
- 申请人： W. Neill Myers , John C. Forbes , Wayne L. Barnes
- 申请人地址： DC Washington
- 专利权人： The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
- 当前专利权人： The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
- 当前专利权人地址： DC Washington
- 主分类号： B25J15/10
- IPC分类号： B25J15/10 ; B64G1/64 ; B64G4/00 ; B66C1/10 ; B25J3/00
摘要：
An end effector device (A) for grasping and holding an article such as a handle (18) of a space telescope is disclosed. The device includes a V-shaped capture window (74) defined as inclined surfaces (76, 78) in parallel face plates (22, 24) which converge toward a retainer recess (54) in which the handle is retained. A pivotal finger (30) meshes with a pair of pivoted fingers (26, 28) which rotate in counterrotation. The fingers rotate to pull a handle within the capture window into recess (54) where latches (50) lock handle (18) in the recess. To align the capture window, plates (22, 24) may be cocked plus or minus five degrees on base (64).
公开/授权文献
- US6097479A Critical angle sensor 公开/授权日：2000-08-01
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