Aircraft wing/nacelle combination

Details Aircraft wing/nacelle combination Aircraft wing/nacelle combination

1993-12-21

1995-08-22

Barefoot, Galen L.

Aeronautics and astronautics

Aircraft power plants

Mounting

244 55, 244130, B64D 2700, B64D 2902

Patent

active

054432308

ABSTRACT:
An aircraft wing 18 and nacelle 24 combination includes a double cambered pylon 28 extending between the wing and the nacelle to support an aircraft engine 22. The pylon includes an airfoil 30 extending in a generally vertical direction having a leading edge 32 and a trailing edge 39. The airfoil is curved away from the aircraft in an axial rearward direction and a portion of the airfoil is curved toward the aircraft in the vertical direction from the nacelle toward the wing.

REFERENCES:
patent: 1990606 (1935-02-01), Junkers
patent: 3519227 (1970-07-01), Brooks
patent: 4449683 (1984-05-01), Gratzer et al.
patent: 4637573 (1987-01-01), Perin et al.
patent: 4801058 (1989-01-01), Mullins
patent: 4867394 (1989-09-01), Patterson, Jr.

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