发明名称 MODULAR ENGINE, SUCH AS A JET ENGINE, WITH A SPEED REDUCTION GEAR
摘要 The present invention relates to an engine (1) with a modular structure comprising a plurality of coaxial modules (A, B, C) with, at one end, a first module (A) comprising a power transmission shaft (3) and a speed reduction gear (7), said power transmission shaft being driven via the speed reduction gear (7) by a turbine shaft (2) secured to one (C) of said coaxial modules that is separate from the first module, the speed reduction gear comprising a drive means (8 and 9) fixed to the turbine shaft (2) and to a journal (13) of a shaft of a low-pressure compressor rotor (1a), characterized in that it comprises a first nut (16) for fastening the drive means to the journal and a second nut (14) for fastening the drive means to the turbine shaft.
申请公布号 EP3071792(A1) 申请公布日期 2016.09.28
申请号 EP20140806028 申请日期 2014.11.06
申请人 SAFRAN AIRCRAFT ENGINES 发明人 BRAULT, MICHEL GILBERT ROLAND;NOWAKOWSKI, NATHALIE
分类号 F01D5/02;F02C7/32;F02C7/36 主分类号 F01D5/02
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