Jet turbine engine with two counter-rotating fans attached...

F - Mech Eng,Light,Heat,Weapons – 02 – K

Patent

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Details

F02K 3/065 (2006.01) F01D 5/03 (2006.01) F02C 3/067 (2006.01) F02C 7/36 (2006.01) F02K 3/072 (2006.01)

Patent

CA 2495598

L'invention concerne un turboréacteur ayant à l'avant d'un carter intermédiaire (2) deux soufflantes (3, 5) contrarotatives solidaires d'un compresseur à basse pression (7) contrarotatif. Les pales (14) de la soufflante arrière (5) s'étendent dans le flux secondaire (F2) à partir d'une roue (15) entourant le rotor extérieur (20) du compresseur à basse pression (7). La distance (L) entre les pale; (10) de la soufflante avant (3) et les pales (14) de la soufflante arrière (5) est au moins égale à deux fois la longueur (I) de la projection axiale de la corde de tête des pales (10) de la soufflante avant (3).

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