Propellant system with integrated pylon for aircraft

Details Propellant system with integrated pylon for aircraft Propellant system with integrated pylon for aircraft

B - Operations, Transporting

64

D

B64D 29/06 (2006.01)

Patent

CA 2602176

Système propulsif comprenant un turboréacteur à double flux, et une nacelle (10) dont une partie cylindrique aval (20) est rigide et est fixée à son extrémité amont sur un carter intermédiaire du moteur, cette partie cylindrique aval (20) comprenant également une poutre longitudinale (26) de fixation de tiges (28) d'accrochage du moteur sur une partie (22) d'un avion.

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