Integrated propellant system that includes a by-pass engine

Details Integrated propellant system that includes a by-pass engine Integrated propellant system that includes a by-pass engine

B - Operations, Transporting

64

D

B64D 29/00 (2006.01) F02C 7/20 (2006.01)

Patent

CA 2602141

Système propulsif intégré à moteur à turboréacteur, comprenant une structure cylindrique aval de nacelle en deux parties dont l'une (26) est fixe et comprend une poutre (20) de fixation de moyens d'accrochage sur l'avion, et dont l'autre (40) est mobile entre une position de service et une position d'ouverture facilitant la maintenance.

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