Vectorable nozzle for aircraft

Details Vectorable nozzle for aircraft Vectorable nozzle for aircraft

1994-02-25

2000-03-14

Jordan, Charles T.

Aeronautics and astronautics

Aircraft, heavier-than-air

Fluid sustained

23926519, B64C 2900, B63H 1110

Patent

active

060361425

ABSTRACT:
A vectorable nozzle for a vertical lift aircraft comprising an array of lift flow deflecting vanes mounted in a frame hinged to an undersurface of the aircraft. The nozzle is formed by a plurality of telescopic shroud members which together with the vane frame are mounted at their forwardmost ends. The disposition of the vanes is such that the lift flow is directed downwards when the nozzle is extended. When the nozzle is retracted the flow is vectored rearwards to provide forward thrust. In this position the nozzle generates minimum aerodynamic drag from forward movement of the aircraft. The nozzle preferably is fully stowed within the aircraft, and concealed by surface doors when not in use.

REFERENCES:
patent: 3241312 (1966-03-01), Clark
patent: 3248877 (1966-05-01), Alderson et al.
patent: 3486716 (1969-12-01), Haberkorn et al.
patent: 3981451 (1976-09-01), Prior et al.
patent: 4222234 (1980-09-01), Adamson
patent: 4474345 (1984-10-01), Musgrove
patent: 4482109 (1984-11-01), du Pont
patent: 4713935 (1987-12-01), Szuminski et al.

Affiliated with

Also associated with

Rating

Vectorable nozzle for aircraft does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Vectorable nozzle for aircraft, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Vectorable nozzle for aircraft will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-161454