发明名称 |
Flow sleeve impingement cooling baffles |
摘要 |
A combustor assembly for a turbine engine includes a combustor liner, a flow sleeve and a baffle ring. The flow sleeve surrounds the combustor liner. An annulus is formed between the flow sleeve and the combustor liner. A plurality of row of cooling holes are formed in the flow sleeve. The baffle ring radially surrounds the combustor liner and is located in the annulus. |
申请公布号 |
US8291711(B2) |
申请公布日期 |
2012.10.23 |
申请号 |
US20080179671 |
申请日期 |
2008.07.25 |
申请人 |
CHOKSHI JAISUKHLAL V.;SMITH CRAIG F.;FIGUEROA CARLOS G.;GEORGE LARRY C.;UNITED TECHNOLOGIES CORPORATION |
发明人 |
CHOKSHI JAISUKHLAL V.;SMITH CRAIG F.;FIGUEROA CARLOS G.;GEORGE LARRY C. |
分类号 |
F02C1/00 |
主分类号 |
F02C1/00 |
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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