发明名称 |
Innretningsanordning for a understotte en last pa et baereelement samt anvendelse derav |
摘要 |
The thrust vector motor for a satellite has a support plate (2) with connecting arms (41-43) which are spaced around the mounting. Each arm has a flexible section (4) with one end (47) connected to the end of the support via a first connection with a single degree of freedom (9) and a second degree of freedom (48) connected to the load by a second coupling (10) with one degree of freedom. Claims include a space system using the mounting |
申请公布号 |
NO320294(B1) |
申请公布日期 |
2005.11.21 |
申请号 |
NO20010004514 |
申请日期 |
2001.09.17 |
申请人 |
SNECMA MOTEURS SA |
发明人 |
CHATENET LUC |
分类号 |
B64G1/24;B64G1/22;B64G1/26;B64G1/64;B64G1/66;F16C11/12;F16H21/46;F16M11/12 |
主分类号 |
B64G1/24 |
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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