发明申请
US20100054926A1 SYSTEM AND METHOD FOR THERMAL MANAGEMENT OF A GAS TURBINE INLET 审中-公开
一种气体涡轮机入口热管理系统及方法

SYSTEM AND METHOD FOR THERMAL MANAGEMENT OF A GAS TURBINE INLET
摘要:
A thermal management system includes: a turbine assembly including an inlet housing, a compressor in fluid communication with the inlet housing, a power turbine in fluid communication with the compressor, and an exhaust assembly in fluid communication with the power turbine; and at least one heat pipe having a first portion disposed in thermal communication with the inlet housing and a second portion disposed in thermal communication with the exhaust assembly, the at least one heat pipe configured to transfer thermal energy from the exhaust assembly to at least one of input gas entering the inlet housing and at least one component of the inlet housing.
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