发明名称 |
GAS TURBINE ENGINES WITH HEATED CASES |
摘要 |
A case for a gas turbine engine includes a case body defining an axially extending core flow path, a radially extending bleed air duct coupling the core flow path in fluid communication with the external environment, and a structure-supporting member spanning the bleed air duct. A lubricant conduit is connected to the case body and is in thermal communication with the structure-supporting member. |
申请公布号 |
EP3034835(A1) |
申请公布日期 |
2016.06.22 |
申请号 |
EP20150200195 |
申请日期 |
2015.12.15 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
CLARKSON, STEVEN;VAN NESS, DANIEL L.;REMBISH, PAUL THOMAS |
分类号 |
F02C7/047;F01D17/10;F02C9/18;F04D27/02 |
主分类号 |
F02C7/047 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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