发明名称 INTERCOOLED GAS TURBINE ENGINE
摘要 A gas turbine engine having improved output horsepower and a method of achieving it. The engine has, in order, a low pressure compressor, a high pressure compressor, a combustor, a high pressure turbine and a low pressure turbine. The high pressure turbine is drivingly connected to both compressors with a speed reducing gear box therebetween. An intercooler between the compressors reduces the horsepower requirement of the high pressure compressor. Flow from the combustor is sufficiently heated to enable the high pressure turbine to drive both compressors with the output horsepower of the low pressure turbine devoted to the engine load.
申请公布号 CA2093683(C) 申请公布日期 2002.10.15
申请号 CA19932093683 申请日期 1993.04.08
申请人 发明人 FARRELL, WILLIAM MILLER;LEONARD, GARY LEE
分类号 F02C3/10;F02C3/107;F02C7/143;(IPC1-7):F02C3/00 主分类号 F02C3/10
代理机构 代理人
主权项
地址