发明名称 Combustor liner construction for gas turbine engine
摘要 Floating panel heat shields 26 cover the walls of a combustor with a portion of the cooling air 32 passing upstream. The dome heat shield 36 has a lip 42 overlapping a portion of the wall hot shield 26. Dome 16 at location 44 deflects cooling flow 32 forcing it inwardly against lip 42 to improve cooling of lip 42.
申请公布号 US5012645(A) 申请公布日期 1991.05.07
申请号 US19870081083 申请日期 1987.08.03
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 REYNOLDS, HAROLD G.
分类号 F02C7/18;F23R3/00;F23R3/06;F23R3/10;F23R3/42 主分类号 F02C7/18
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