发明名称 METHOD OF TAKING OFF AUXILIARY POWER FROM AN AIRPLANE TURBOJET, AND A TURBOJET FITTED TO IMPLEMENT SUCH A METHOD
摘要 Producing the electrical power need for equipment on board an airplane. Auxiliary power is taken off by means of a shaft driven by the high pressure turbine and, when idling, the efficiency of the low pressure turbine is degraded so as to enable the high pressure turbine to operate at a speed that is sufficient for delivering the required auxiliary power.
申请公布号 US2010000223(A1) 申请公布日期 2010.01.07
申请号 US20080031194 申请日期 2008.02.14
申请人 SNECMA 发明人 COLOTTE BAPTISTE BENOIT;GALIVEL JEAN PIERRE;ZSIGA ZOLTAN
分类号 F02C9/00;F01D7/00;F02C6/04 主分类号 F02C9/00
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