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公开(公告)号:US4659038A
公开(公告)日:1987-04-21
申请号:US657601
申请日:1984-10-04
CPC分类号: B64C39/024 , B64C3/56 , F42B10/16 , B64C2201/046 , B64C2201/102 , B64C2201/165 , B64C2201/201
摘要: The deployment of folded down wings in an aircraft following, for example, rocket assisted launching from the container is carried out through gas pressure springs with strong attenuation in the final phase, the springs being releasably coupled to the wings for being jettisoned upon completion of deployment.
摘要翻译: 在飞机后面展开折叠的机翼,例如从容器的火箭辅助发射通过在最后阶段具有强衰减的气体压力弹簧进行,弹簧可释放地联接到机翼,以在完成展开后被放弃 。
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公开(公告)号:US4645142A
公开(公告)日:1987-02-24
申请号:US564476
申请日:1983-12-21
申请人: Michael Soelter
发明人: Michael Soelter
CPC分类号: B60V1/16 , B64D1/14 , F16F9/0418 , B64D2201/00
摘要: One end of a hose is affixed to the underside of the object which may descend and whose impact has to be cushioned while the other end of the hose is pulled through the first end, the two ends are separately fastened permitting filling of the hose; a second hose may be inserted in the first one to provide separate filling spaces, one being the interior of the second hose and the other one being the gas space between the two hoses whereby different pressures permit selection of the resilient characteristics of the cushion.
摘要翻译: 软管的一端固定到物体的下侧,该下侧可能下降,并且其冲击必须被缓冲,同时软管的另一端被拉过第一端,两端分别固定,允许填充软管; 可以在第一软管中插入第二软管以提供单独的填充空间,一个是第二软管的内部,另一个是两个软管之间的气体空间,由此不同的压力允许选择衬垫的弹性特性。
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