发明名称 METHOD AND APPARATUS FOR GAS TURBINE ENGINE TEMPERATURE MANAGEMENT
摘要 A turbine engine includes a turbine, a compressor for compressing air and a combustor for receiving the compressed air through an inlet passage and operable to burn fuel therewith to deliver hot exhaust gas to the turbine. Also included is a wheel space defined proximate to the combustor. Further included is a cooling air passage extending between the compressor and the wheel space. Yet further included is a valve assembly having a valve member disposed in the cooling air passage and operable to admit a cooling air to the wheel space in response to a condition therein.
申请公布号 US2013305740(A1) 申请公布日期 2013.11.21
申请号 US201313951907 申请日期 2013.07.26
申请人 GENERAL ELECTRIC COMPANY 发明人 MORGAN REX ALLEN;DAVI MICHAEL ALAN;GAZZILLO CLEMENT;JORDAN HAROLD LAMAR
分类号 F02C7/12 主分类号 F02C7/12
代理机构 代理人
主权项
地址