发明名称 |
Interstage cooled turbine engine |
摘要 |
A gas turbine engine (10) includes a compressor, combustor (20), and high pressure (HP) turbine operatively joined together. An interstage cooling circuit is joined in flow communication from an intermediate stage of the compressor to a forward face of an HP disk supporting a row of turbine blades (44) for channeling interstage bleed cooling air thereto. |
申请公布号 |
EP1921255(A3) |
申请公布日期 |
2010.10.20 |
申请号 |
EP20070119944 |
申请日期 |
2007.11.05 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
LEE, CHING-PANG;MONIZ, THOMAS ORY;ORLANDO, ROBERT JOSEPH |
分类号 |
F01D5/08;F02C9/18 |
主分类号 |
F01D5/08 |
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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