发明名称 |
Premix combustor with flow constricting baffle between combustion and dilution zones |
摘要 |
A combustion liner for a gas turbine combustion apparatus has a wall of circular cross-section defining a primary air entrance at its upstream end, providing means for introduction of fuel near the upstream end, having a convergent-divergent fuel prevaporization zone, a reaction zone, and a dilution zone.
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申请公布号 |
US3938324(A) |
申请公布日期 |
1976.02.17 |
申请号 |
US19740531874 |
申请日期 |
1974.12.12 |
申请人 |
GENERAL MOTORS CORPORATION |
发明人 |
HAMMOND, JR., DEAN C.;QUINN, RONALD E. |
分类号 |
F23R3/16;F23R3/26;F23R3/30;(IPC1-7):F02C7/22 |
主分类号 |
F23R3/16 |
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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