Airplane having engines partially encased in the fuselage

Details Airplane having engines partially encased in the fuselage Airplane having engines partially encased in the fuselage

B - Operations, Transporting

64

D

B64D 29/04 (2006.01) B64C 1/00 (2006.01) B64C 7/02 (2006.01)

Patent

CA 2732664

The invention relates to an airplane provided with dual-flow turbojet engines (12) having nacelles (16) at least partially encased in the fuselage (14), characterised in that the air intake of each engine (12) is connected to the fuselage by two boundary layer guiding walls (20), said walls (20) extending towards the upstream side of the air intake (18) and being spaced apart towards the upstream side.

Avion équipé de moteurs (12) à turboréacteur à double flux dont les nacelles (16) sont au moins partiellement encastrées dans le fuselage (14), caractérisé en ce que l'entrée d'air de chaque moteur (12) est reliée au fuselage par deux parois de guidage (20) de couche limite, ces parois (20) s'étendant vers l'amont de l'entrée d'air (18) et s'écartant l'une de l'autre vers l'amont.

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