发明名称 |
Premixed combustor |
摘要 |
A combustion system for a gas turbine engine is disclosed. Fluid transfer and premixing techniques are developed. The combustion system is specifically adapted, in one embodiment, to an engine having a centrifugal or an axial/centrifugal compressor including a pipe diffuser at the downstream end thereof. Flow transfer tubes are shown between the pipe diffuser and a radial inflow combustor.
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申请公布号 |
US4081957(A) |
申请公布日期 |
1978.04.04 |
申请号 |
US19760682945 |
申请日期 |
1976.05.03 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
COX, JR., GEORGE BENJAMIN |
分类号 |
F23R3/14;F23R3/42;(IPC1-7):F02C7/22 |
主分类号 |
F23R3/14 |
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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