发明名称 Aircraft gas turbine engine with a liquid-air heat exchanger
摘要 PCT No. PCT/EP96/02553 Sec. 371 Date Apr. 27, 1998 Sec. 102(e) Date Apr. 27, 1998 PCT Filed Jun. 13, 1996 PCT Pub. No. WO97/02984 PCT Pub. Date Jan. 30, 1997A turboprop engine having an oil cooler which is disposed in the engine pod and upon which cooling air acts. The oil cooler is disposed in a flow duct which at the rear opens into the environment and at the front can be connected alternately to an air-inlet opening or to the feed duct of the compressor of the aircraft gas turbine.
申请公布号 US6000210(A) 申请公布日期 1999.12.14
申请号 US19980983033 申请日期 1998.04.27
申请人 BMW ROLLS ROYCE GMBH 发明人 NEGULESCU, DIMITRIE
分类号 B64D33/10;F02C7/14;(IPC1-7):F02C7/14 主分类号 B64D33/10
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