发明名称 |
Combustors and combustion systems for gas turbine engines |
摘要 |
<p>A combustion system includes a combustor having a forward annular liner having a first plurality of effusion holes, and an aft annular liner having a second plurality of effusion holes and forming a combustion chamber with the forward annular liner. The first plurality of effusion holes and the second plurality of effusion holes are adapted to receive compressed air from a compressor and contribute to a single toroidal recirculation air flow pattern in the combustion chamber. The combustion system further includes a rotary fuel slinger further adapted to receive a flow of fuel from a fuel source and to centrifuge the received fuel into the combustion chamber; and an igniter extending at least partially into the combustion chamber to ignite the fuel and compressed air in the combustion chamber, to thereby generate combusted gas.
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申请公布号 |
EP1978308(A3) |
申请公布日期 |
2013.02.20 |
申请号 |
EP20080102901 |
申请日期 |
2008.03.25 |
申请人 |
HONEYWELL INTERNATIONAL INC. |
发明人 |
CRITCHLEY, IAN L.;ZUPANC, FRANK J. |
分类号 |
F23R3/38;F23R3/06;F23R3/52 |
主分类号 |
F23R3/38 |
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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