F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
F02C 3/04 (2006.01) F02C 3/107 (2006.01)
Patent
CA 2230002
The turbine engine with an optimized compression system comprising a high-pressure turbine driving a primary high-pressure compressor also comprises at least one secondary low-pressure compressor (1) driven by the high-pressure turbine (6) through the medium of a speed reducing unit (21, 22, 23, 24). The invention has applicaitons in turboprops and turboblowers.
La turbomachine à système de compression optimisé comportant une turbine à haute pression entraînant un premier compresseur à haute pression est caractérisée en ce qu'elle comporte en outre au moins un deuxième compresseur à basse pression (1) entraîné par la turbine à haute pression (6) par l'intermédiaire d'un réducteur de vitesse (21, 22, 23, 24). L'invention s'applique notamment aux turbopropulseurs ou aux turbosoufflantes.
Goudreau Gage Dubuc
Snecma Moteurs
Societe Nationale D'etude Et de Construction de Moteurs D'aviati
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