Thrust vectoring exhaust nozzle arrangement

Details Thrust vectoring exhaust nozzle arrangement Thrust vectoring exhaust nozzle arrangement

1987-04-09

1988-08-16

Kashnikow, Andres

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

With means controlling amount, shape or direction of...

60271, 23926539, B64C 938, F02K 100

Patent

active

047638400

ABSTRACT:
A two-dimensional thrust vectoring nozzle (10) includes aftward divergent flaps (26, 28) positioned by a linkage assembly (38). The assembly (38) includes a linear track (42) pivotable about a transverse axis (44) for positioning a scissors linkage pivot (52) to selectively vary the divergence angle and vertical thrust vector of the nozzle (10).

REFERENCES:
patent: 2858668 (1958-11-01), Kelley et al.
patent: 3164956 (1965-01-01), Colebrook et al.
patent: 3419218 (1968-12-01), Campbell et al.
patent: 4375276 (1983-03-01), Konarski
patent: 4519561 (1985-05-01), Timms
patent: 4605169 (1986-08-01), Mayers
patent: 4641782 (1987-02-01), Woodward

Affiliated with

Also associated with

Rating

Thrust vectoring exhaust nozzle arrangement does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-595354