发明授权
- 专利标题: Inflatable restraint for missiles and missile canisters
- 专利标题(中): 导弹和导弹罐充气限制
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申请号: US10283242申请日: 2002-10-30
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公开(公告)号: US07735440B2公开(公告)日: 2010-06-15
- 发明人: Grant W. Corboy , Michael J. Shaffer , Mahendra Maheshwari
- 申请人: Grant W. Corboy , Michael J. Shaffer , Mahendra Maheshwari
- 申请人地址: US MD Bethesda
- 专利权人: Lockheed Martin Corporation
- 当前专利权人: Lockheed Martin Corporation
- 当前专利权人地址: US MD Bethesda
- 代理机构: Schwegman, Lundberg & Woessner, P.A.
- 主分类号: B63B1/00
- IPC分类号: B63B1/00 ; B63B5/00
摘要:
An inflatable restraint, and method of using the same, is used to provide support and shock isolation for missiles, torpedoes, missile canisters or the like in naval vessels. The inflatable restraint features a structural collar, at least one inflatable bladder and at least one interference member. The interference member is attached to the inside of the structural collar and the interference member is fully adjustable to ensure a snug fit during the loading of the missile, torpedo or missile canister into the structural collar. Once the missile, torpedo, missile canister or the like is properly inserted into the structural collar, the at least one inflatable bladder, which is also attached to the inside of the structural collar, is inflated to restrain the object. The pressure of the inflatable bladder may be regulated to provide variable spring constants and stiffness.
公开/授权文献
- US20030226771A1 Inflatable restraint for missiles and missile canisters 公开/授权日:2003-12-11
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