发明名称 Twin-shaft turbojet engine with differential gearbox for auxiliary power drive
摘要 The turbine has electrical generators driven through a differential gear (30) having two planet wheels (31`, 32`) driven by high and low pressure rotor shafts (1, 2) of high and low pressure bodies. The wheels drive a planet gear (33) mounted in a casing (36). Transmission ratios between respective shafts and wheels are such that distribution of power between the bodies lies between 80 by 20 percent.
申请公布号 EP1541834(A1) 申请公布日期 2005.06.15
申请号 EP20040300858 申请日期 2004.12.08
申请人 SNECMA 发明人 LARDELLIER, ALAIN
分类号 F02C7/32;F02C7/36;F16H48/08 主分类号 F02C7/32
代理机构 代理人
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