发明申请
US20090104020A1 SYSTEM FOR DELIVERING AIR FROM A MULTI-STAGE COMPRESSOR TO A TURBINE PORTION OF A GAS TURBINE ENGINE 有权
将空气从多级压缩机输送到气体涡轮发动机的涡轮机部分的系统

SYSTEM FOR DELIVERING AIR FROM A MULTI-STAGE COMPRESSOR TO A TURBINE PORTION OF A GAS TURBINE ENGINE
摘要:
A system for providing air from a multi-stage to a turbine includes a turbine having a high pressure input port and a low pressure input port. The system also includes a compressor having at least one high pressure extraction air output and at least one low pressure extraction air output. A valve is fluidly connected to the at least one high pressure extraction air output, at least one low pressure extraction air output and low pressure input port of the turbine. The valve is selectively operated to fluidly connect the at least one low pressure extraction air output with the low pressure input port during normal operating conditions and fluidly connect the at least one high pressure extraction air output and the low pressure input port during a turn down condition or below design temperature operation to enhance turbine engine performance.
信息查询
0/0