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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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