发明名称 |
Tri-passage diffuser for a gas turbine |
摘要 |
<p>In a gas turbine having a transition region between a combustor and turbine stage including a transition piece duct extending between a combustor liner and the turbine stage; an impingement sleeve surrounding the transition piece, the impingement sleeve having a plurality of apertures therein; and a compressor diffuser (28) directing compressor discharge air into the transition region, an improvement wherein the diffuser includes a pair of outer walls (30,32) flaring outwardly in a direction of compressor discharge air flow; and a pair of baffles (34,36) within a flow area defined by the pair of outer diffuser walls which divide the flow area into three discrete flow passages (54,56,58). One passage (54) has a substantially radial flow component; a second passage (56) has both radial and axial flow components; and a third passage (58) has a substantially axial flow component. <IMAGE></p> |
申请公布号 |
EP0789195(A1) |
申请公布日期 |
1997.08.13 |
申请号 |
EP19970300477 |
申请日期 |
1997.01.27 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
LIN, EDWARD J. C.;WARREN, RICHARD EDWIN, JR.;VANDERVORT, CHRISTIAN L. |
分类号 |
F02C7/00;F02K3/077;F04D29/54;F23R3/04;(IPC1-7):F23R3/04 |
主分类号 |
F02C7/00 |
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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