发明名称 Inflatable restraint for missiles and missile canisters
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.
申请公布号 US7735440(B2) 申请公布日期 2010.06.15
申请号 US20020283242 申请日期 2002.10.30
申请人 LOCKHEED MARTIN CORPORATION 发明人 CORBOY GRANT W.;SHAFFER MICHAEL J.;MAHESHWARI MAHENDRA
分类号 B63B1/00;B63B5/00;F42B39/22;F42B39/24 主分类号 B63B1/00
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