Aircraft

Details Aircraft Aircraft

B - Operations, Transporting

64

D

244/13

B64D 33/04 (2006.01)

Patent

CA 1204095

ABSTRACT OF THE DISCLOSURE An aircraft includes a fuselage portion 10, a wing 14 attached to the fuselage by means of an intermediate wing root portion 15. The intermediate wing root portion 15 comprises upper and lower surfaces diverging rearwardly to a region of maximum divergence. The aft region of the intermediate wing root portion is cut away to receive propulsion jet outlet means 16, which is located adjacent and between a rearward region of the wing and the fuselage. The outlet means is shaped to lie within a rearward projection of the region of maximum divergence, thus to reduce or eliminate the drag induced by the outlet means. The outlet means is preferably swivellable to a position in which it generates a lift component.

392823

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