发明名称 Slip joint duct system
摘要 Various joints within a duct assembly to allow relative movement between portions of a fluid system which are interconnected by this duct assembly are disclosed. This duct assembly is particularly suited for interconnecting a rocket fuel tank and rocket engine of a space travel vehicle. In any case, this duct assembly includes a pair of duct suctions, each of which includes a gimbal on an end thereof. The opposite ends of these two duct sections are disposed in a telescope-like arrangement with a slip joint therebetween to allow the duct sections to move at least generally axially relative to each other. This slip joint includes a pair of longitudinally spaced bushings, between which are disposed a plurality of annular seals. The bushings inhibit contain between the two duct sections by maintaining the same in spaced relation.
申请公布号 US2002170285(A1) 申请公布日期 2002.11.21
申请号 US20020190269 申请日期 2002.07.03
申请人 DEAN MICHAEL B.;ZEGLER FRANK C. 发明人 DEAN MICHAEL B.;ZEGLER FRANK C.
分类号 F02K9/60;F16J15/16;F16J15/18;F16L27/08;F16L27/12;(IPC1-7):F02K9/60 主分类号 F02K9/60
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