Aircraft for short landing and takeoff distance

Aeronautics and astronautics – Aircraft – heavier-than-air – Airplane and fluid sustained

Patent

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Details

244 42DA, B64C 1506

Patent

active

039387607

ABSTRACT:
Aircraft for short landing and takeoff distance is provided with engines providing jet flow above the wing. Flap structure aft of the engine can be swung up on an axis near the trailing wing edge, to deflect jet flow in down direction.

REFERENCES:
patent: 2974899 (1961-03-01), Fowler
patent: 3260477 (1966-01-01), Grahame
patent: 3285538 (1966-11-01), Burnelli
patent: 3614028 (1971-10-01), Kleckner

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