发明名称 |
COMBUSTOR FUEL NOZZLE ARRANGEMENT |
摘要 |
The fuel nozzles(12a) in the combustor of a gas turbine engine are concentrically disposed in two tiers about the circumference of the dome (10a) and are arranged in a triangular pattern with the air swirl orientation providing an increased intensity of combustion so as to enable a reduction in combustor size and weight while increasing temperature rise and the overall thrust-to-weight ratio of the engine. |
申请公布号 |
IL92977(D0) |
申请公布日期 |
1991.06.10 |
申请号 |
IL19900092977 |
申请日期 |
1990.01.05 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
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分类号 |
F23R3/28;F23D11/12;F23R3/14;F23R3/16;F23R3/50 |
主分类号 |
F23R3/28 |
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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