F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
F02C 7/36 (2006.01) F02C 3/04 (2006.01) F02C 3/113 (2006.01) F02C 6/20 (2006.01) F02K 3/02 (2006.01)
Patent
CA 2491437
The invention relates to a turbine engine (1) with a semi-fixed turbine, particularly for aircraft driving a receiver (2) controlled so as to preserve a roughly constant rotation speed. The turbine engine, in particular via a gear system (20), drives the receiver and an LP compressor (6) with an LP turbine (14). According to the invention, the gear system has a torque control system (26) maintaining a constant ratio between the drive torque of the receiver transmitted by the gear system and the drive torque of the LP compressor transmitted by this same gear system.
Goudreau Gage Dubuc
Snecma
Snecma Moteurs
LandOfFree
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