发明名称 BUFFER SYSTEM THAT COMMUNICATES BUFFER SUPPLY AIR TO A PORTION OF A GAS TURBINE ENGINE
摘要 <p>A gas turbine engine includes a buffer system that communicates a buffer supply air to a portion of the gas turbine engine. The buffer system includes a first bleed air supply having a first pressure, a second bleed air supply having a second pressure that is greater than the first pressure, and a valve that selects between the first bleed air supply and the second bleed air supply to communicate the buffer supply air to the portion of the gas turbine engine.</p>
申请公布号 EP2809917(A1) 申请公布日期 2014.12.10
申请号 EP20130796350 申请日期 2013.01.16
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 MUNSELL, PETER, M.;STRIPINIS, PHILIP, S.
分类号 F02C7/06;F01D25/12;F01D25/18;F02C6/04;F02C6/08;F02C7/18;F02G3/00 主分类号 F02C7/06
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