发明名称 |
GAS TURBINE ENGINE DIFFUSER COOLING AND MIXING ARRANGEMENT |
摘要 |
A diffuser for a gas turbine engine includes a diffuser housing that has a circumferential array of hollow struts that provide a cavity. The diffuser housing includes inlet and outlet apertures that are in fluid communication with the cavity. An opening on a trailing end of the struts is in fluid communication with the cavity. The diffuser housing is configured to introduce a fluid through the inlet aperture and receive a core flow through the opening. The fluid and core flow exit through the outlet aperture. |
申请公布号 |
EP3039264(A1) |
申请公布日期 |
2016.07.06 |
申请号 |
EP20140839670 |
申请日期 |
2014.07.18 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
LYONS, CHRISTOPHER B.;CHEUNG, ALBERT K. |
分类号 |
F02C7/00;F01D5/06;F01D5/08;F01D9/02;F01D17/00;F01D25/12;F02C6/08;F02C7/057;F02C7/18;F04D29/54 |
主分类号 |
F02C7/00 |
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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