发明名称 Motorbromssystem för en gasturbin samt förfarande för motorbromsning av en gasturbin
摘要 Method and arrangement for providing a gas turbine ( 1 ) having a first compressor ( 2 ), a combustion chamber ( 16 ) and a first turbine ( 11 ), the turbine being adapted to drive the compressor via a first shaft ( 10 a, 10 b). The gas turbine also has a bleed valve ( 12 ) arranged upstream of the first turbine for conducting part of a gas compressed by the compressor past it during engine braking. The invention also relates to a method for engine-braking a gas turbine.
申请公布号 SE520272(C2) 申请公布日期 2003.06.17
申请号 SE20010001266 申请日期 2001.04.06
申请人 VOLVO AERO CORP 发明人 LARS SUNDIN;BERTIL JOENSSON
分类号 F01D15/02;F01D21/00;F02C3/10;F02C6/00;F02C6/20;F02C7/08;F02C7/36;F02C9/18;F02C9/22;F02C9/28;(IPC1-7):F02C9/18 主分类号 F01D15/02
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