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 US2013164115(A1) 申请公布日期 2013.06.27
申请号 US201213537284 申请日期 2012.06.29
申请人 SENNOUN MOHAMMED EL HACIN;GENERAL ELECTRIC COMPANY 发明人 SENNOUN MOHAMMED EL HACIN
分类号 F02C7/14;F01D25/12;F02C6/08 主分类号 F02C7/14
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