发明名称 |
EXHAUST DIFFUSER FOR A GAS TURBINE ENGINE EXHAUST SYSTEM |
摘要 |
<p>An exhaust diffuser for a gas turbine engine includes a diffuser inlet, a diffuser exit, an inner diffuser wall, and an outer diffuser wall. The inner diffuser wall may include a first tubular member with a flared downstream portion. The outer diffuser wall may include a second tubular member at least partially about the inner diffuser wall and with a second flared downstream portion. The outer diffuser wall and the inner diffuser wall extend between the diffuser inlet and the diffuser exit, and form a diffusing flowpath therebetween. The second flared downstream portion may include a lower section and an upper section, with the upper section extending further downstream in an axial direction than the lower section, relative to the diffuser axis.</p> |
申请公布号 |
WO2014190095(A1) |
申请公布日期 |
2014.11.27 |
申请号 |
WO2014US39038 |
申请日期 |
2014.05.21 |
申请人 |
SOLAR TURBINES INCORPORATED |
发明人 |
STANG, ULRICH E.;HAMM, HANS D. |
分类号 |
F02C7/00;F01D25/30;F02C7/20;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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