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 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|