发明名称 |
NACELLE VENTILATION MANIFOLD |
摘要 |
A gas turbine engine comprises a core engine housing. A nacelle is positioned radially outwardly of the core engine housing. An outer bypass housing is positioned outwardly of the nacelle. There is at least one accessory to be cooled positioned in a chamber radially between the core engine housing and the nacelle. A manifold delivers cooling air into the chamber, and extends ng circumferentially about a central axis of the core engine. The nacelle has an asymmetric flow cross-section across a circumferential extent. |
申请公布号 |
EP3105438(A1) |
申请公布日期 |
2016.12.21 |
申请号 |
EP20150749596 |
申请日期 |
2015.01.20 |
申请人 |
United Technologies Corporation |
发明人 |
SUCIU, Gabriel L.;CHANDLER, Jesse M.;PAPA, Federico |
分类号 |
F02C7/18;F02C7/32 |
主分类号 |
F02C7/18 |
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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