发明名称 Liner hanger cable
摘要 A liner for a gas turbine engine includes a liner defining an inner surface exposed to exhaust gases and a duct spaced radially outward of the liner. A plurality of hanger assemblies is disposed within the radial space between the liner and the duct for supporting the liner relative to the duct. Each of the hanger assemblies includes a cable having a first end attached to the duct and a second end attached to the liner.
申请公布号 US9309834(B2) 申请公布日期 2016.04.12
申请号 US201213484837 申请日期 2012.05.31
申请人 United Technologies Corporation 发明人 Peters Donald W.
分类号 F02C7/20;F02K1/82;F01D25/28;B64D27/26 主分类号 F02C7/20
代理机构 Carlson, Gaskey & Olds, P.C. 代理人 Carlson, Gaskey & Olds, P.C.
主权项 1. A liner assembly for a gas turbine engine comprising: a liner disposed about an engine axis, the liner defining an inner surface exposed to exhaust gases; a duct spaced radially outward of the liner; and a hanger assembly supporting the liner relative to the duct, the hanger assembly including a cable extending transverse to the engine axis and having a first end attached to the duct and a second end attached to the liner, wherein the cable restricts relative radial movement between the liner and duct along a longitudinal length of the cable in only one direction.
地址 Hartford CT US