发明名称 PIPE SUPPORT STRUCTURE FOR AIRCRAFT
摘要 <P>PROBLEM TO BE SOLVED: To provide a pipe support structure for an aircraft capable of preventing preload. <P>SOLUTION: This pipe support structure for an aircraft for supporting a pipe arranged to extend in an X-direction includes: a translation mechanism for supporting the pipe so that the pipe can be translated in parallel; and an angle adjustment mechanism for supporting the pipe so that the angle thereof can be adjusted. The translation mechanism includes: an eccentric sleeve for allowing the pipe to be inserted therethrough and adjusting the position of the pipe in the Z-direction orthogonal to the X-direction; and a Y-direction adjustment mechanism for adjusting the position of the eccentric sleeve in the Y-direction orthogonal to both the X-direction and the Z-direction. The angle adjustment mechanism includes: a first member supporting the pipe and having a first curved surface; and a second curved surface having a shape corresponding to the shape of the first curved surface, is in sliding contact at the second curved surface thereof with the first curved surface, and supports, on the second curved surface thereof, the first member. The first curved surface and the second curved surface are formed so that a cross-sectional shape by the X-Z plane becomes a circular arc-like shape, and the angle of the pipe is adjusted by sliding the first curved surface with respect to the second curved surface. <P>COPYRIGHT: (C)2012,JPO&INPIT
申请公布号 JP2012092890(A) 申请公布日期 2012.05.17
申请号 JP20100239961 申请日期 2010.10.26
申请人 MITSUBISHI HEAVY IND LTD 发明人 MINAMI KEISUKE
分类号 F16L3/16;B64D37/00;F16L3/02;F16L27/04 主分类号 F16L3/16
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