发明公开
- 专利标题: FOIL DEPLOYMENT MECHANISM
- 专利标题(中): 扩展机制WING
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申请号: EP13783943.7申请日: 2013-10-30
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公开(公告)号: EP3063068A1公开(公告)日: 2016-09-07
- 发明人: HODGETTS, Paul
- 申请人: European Space Agency (ESA)
- 申请人地址: 8-10 rue Mario-Nikis 75738 Paris Cedex 15 FR
- 专利权人: European Space Agency (ESA)
- 当前专利权人: European Space Agency (ESA)
- 当前专利权人地址: 8-10 rue Mario-Nikis 75738 Paris Cedex 15 FR
- 代理机构: MERH-IP Matias Erny Reichl Hoffmann Patentanwälte PartG mbB
- 国际公布: WO2015062650 20150507
- 主分类号: B64G1/22
- IPC分类号: B64G1/22 ; B64G1/44
摘要:
A foil deployment mechanism comprises a first drum rotatable about a first longitudinal axis, and a second drum rotatable about a second longitudinal axis. The foil deployment mechanism further comprises a cable, the cable comprising a first section which extends from a lower part of the second drum to an upper part of the first drum, a second section which is wound around a part of the first drum facing away from the second drum, a third section which extends from a lower part of the first drum to an upper part of the second drum, and a fourth section which is wound around a part of the second drum facing away from the first drum, wherein the first section and the third section intersect each other between the first drum and the second drum when being viewed along the first longitudinal axis.
公开/授权文献
- EP3063068B1 FOIL DEPLOYMENT MECHANISM 公开/授权日:2019-01-16
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