发明名称 Combustion chamber of gas turbine with starter film cooling
摘要 A combustion chamber of a gas turbine includes starter film cooling of a combustion chamber wall 4 and several circularly arranged burners 7 with local maxima and minima in the intensity of the starter film 3 being provided around the circumference of the combustion chamber wall 4.
申请公布号 US7124588(B2) 申请公布日期 2006.10.24
申请号 US20030403055 申请日期 2003.04.01
申请人 ROLLS-ROYCE DEUTSCHLAND LTD & CO KG 发明人 GERENDAS MIKLOS;EBEL MICHAEL
分类号 F02C1/00;F02G3/00;F23R3/06 主分类号 F02C1/00
代理机构 代理人
主权项
地址