发明名称 Bleed air and hot section component cooling air system and method
摘要 Combined bleed air and hot section component cooling air systems for gas turbine engines and methods of operating combined bleed air and hot section component cooling air systems are disclosed. An example system may include a high-pressure bleed air line receiving high-pressure bleed air; a precooler receiving at least some of the high-pressure bleed air and discharging cooled high-pressure bleed air; a pressure regulator receiving at least some of the cooled high-pressure bleed air and discharging pressure-regulated cooled bleed air to a pneumatic systems supply line; and/or a hot section component cooling air line connected upstream of the first pressure regulator and configured to convey at least some of the cooled high-pressure bleed air to a hot section component for use as hot section component cooling air.
申请公布号 US9222411(B2) 申请公布日期 2015.12.29
申请号 US201213537284 申请日期 2012.06.29
申请人 General Electric Company 发明人 Sennoun Mohammed El Hacin
分类号 F02C7/14;F01D25/12;F02C6/08;F02C7/18 主分类号 F02C7/14
代理机构 General Electric Company 代理人 General Electric Company ;Andes William Scott
主权项 1. A combined bleed air and hot section component cooling air system for a gas turbine engine, the combined bleed air and hot section component cooling air system comprising: a high-pressure bleed air line configured to receive high-pressure bleed air from a high-pressure stage of a compressor; a first precooler operatively connected to the high-pressure bleed air line to receive at least some of the high-pressure bleed air, transfer heat from the high-pressure bleed air to ambient air, and discharge cooled high-pressure bleed air; a high-pressure discharge line operatively connected to the first precooler to receive the cooled high-pressure bleed air; a first pressure regulator in the high-pressure discharge line, the first pressure regulator being configured to receive at least some of the cooled high-pressure bleed air and discharge pressure-regulated cooled bleed air; a pneumatic systems supply line operatively connected to the high-pressure discharge line downstream of the first pressure regulator to receive the pressure-regulated cooled bleed air; and a hot section component cooling air line operatively connected to the high-pressure discharge line upstream of the first pressure regulator and configured to convey at least some of the cooled high-pressure bleed air to a hot section component for use as hot section component cooling air, further comprising an intermediate-pressure bleed air line configured to receive intermediate-pressure bleed air from an intermediate stage of the compressor and supply the intermediate-pressure bleed air to the first precooler, the first precooler being configured to receive the intermediate-pressure bleed air, transfer heat from the intermediate-pressure bleed air to ambient air, and discharge cooled intermediate-pressure bleed air; an intermediate-pressure discharge line operatively connected to the first precooler to receive the cooled intermediate-pressure bleed air; a second pressure regulator in the intermediate-pressure discharge line, the second pressure regulator being configured to receive at least some of the cooled intermediate-pressure bleed air and discharge pressure-regulated cooled bleed air to the pneumatic systems supply line.
地址 Schenectady NY US