发明名称 |
Pitch link for rotary wing aircraft and automatic adjuster thereof |
摘要 |
A pitch link for a rotary wing aircraft includes first and second shaft members threadingly engaged with each other. A first rod end is fixedly secured to the first shaft member and a second rod end is rotatably coupled to the second shaft member. First and second spherical bearings are mounted on the first and second rod ends, respectively. A guide member guides the first shaft member for movement in an axial direction of the first shaft with respect to the second shaft while preventing rotation of the first shaft.
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申请公布号 |
US5946981(A) |
申请公布日期 |
1999.09.07 |
申请号 |
US19970926446 |
申请日期 |
1997.09.10 |
申请人 |
KAWASAKI JUKOGYO KABUSHIKI KAISHA |
发明人 |
IDE, HIDEAKI;BANDOH, SHUNICHI;YASUHARA, HIROSHI |
分类号 |
B64C27/605;B64C27/59;B64C27/72;(IPC1-7):G05G1/00 |
主分类号 |
B64C27/605 |
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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