发明名称 |
A conduit for bleed air in a gas turbine engine |
摘要 |
A cowl cavity 26 is defined between a core engine cowl 25 and an engine inner casing 24. A core fairing 34 is provided at the forward end of the engine inner casing 24 and has a radially outer surface 36 which, with the cowl 25, provides an airwashed surface of a bypass duct 22. A plenum 44 is provided within the cowl cavity 26 and receives air from bypass flow B through openings 46 in the surface 36. Conduits 48 extend from a partition 42 defining the plenum 44 to distribute air to locations and components within the engine. |
申请公布号 |
EP2497908(A3) |
申请公布日期 |
2015.03.18 |
申请号 |
EP20120156803 |
申请日期 |
2012.02.24 |
申请人 |
ROLLS-ROYCE PLC |
发明人 |
BADCOCK, GAWAIN CHARLES RAYDON;GOULDS, ROBERTS;BEWICK, CLARE LINDSAY;PEACE, RICHARD |
分类号 |
F01D11/00;F01D25/14;F02C7/18;F02C9/18 |
主分类号 |
F01D11/00 |
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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