发明名称 INCORPORATION OF PUMPS INTO A GEARBOX APPENDED TO AN AIRCRAFT ENGINE
摘要 This gearbox for an aircraft engine, to be fixed to the engine of same in order to withdraw a part of the power from same and transmit it to equipment including, in particular, fuel or lubricant pumps, is original in that at least some of the pumps are housed inside the gearbox housing (31, 36), which simplifies the structure of the device and the assembly of same, and makes it possible to save components and reduce the space requirement. The pump (32) is driven by the shaft (38) of a toothed wheel (39) of the drivetrain of the gearbox so as to drive the moving parts of same that are responsible, in particular, for compressing and discharging fluid.
申请公布号 WO2014181069(A1) 申请公布日期 2014.11.13
申请号 WO2014FR51075 申请日期 2014.05.09
申请人 HISPANO SUIZA 发明人 PRUNERA-USACH, STÉPHANE;BECK, GUILLAUME;PELTIER, JORDANE
分类号 F02C7/06;F02C7/32 主分类号 F02C7/06
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