发明名称 |
COMBUSTOR FOR TURBINE ENGINE |
摘要 |
<p>A turbine engine includes an annular combustor having a combustion chamber defined between an annular outer wall and an annular inner wall. A diffuser case substantially encloses the annular outer and inner walls. A fuel nozzle extends through the diffuser case to an outlet that provides fuel to an interior chamber of the combustor. In one embodiment, front portions of the inner and outer walls curve toward one another and overlap to form an annular gap or manifold through which fuel is distributed to the combustion chamber.</p> |
申请公布号 |
EP1828683(B1) |
申请公布日期 |
2013.04.10 |
申请号 |
EP20040822059 |
申请日期 |
2004.12.01 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SUCIU, GABRIEL L.;NORDEEN, CRAIG A.;KRAMER, STEPHEN |
分类号 |
F02C3/073;F02K3/068;F23R3/10;F23R3/28;F23R3/50 |
主分类号 |
F02C3/073 |
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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