Variable area nozzle with fixed convergent-divergent walls and r

Details Variable area nozzle with fixed convergent-divergent walls and r Variable area nozzle with fixed convergent-divergent walls and r

1994-04-11

1996-01-09

Thorpe, Timothy S.

Power plants

Reaction motor

With thrust direction modifying means

23926525, F02K 130

Patent

active

054818680

ABSTRACT:
A variable area convergent-divergent nozzle for use as an attitude control thruster on a VTOL aircraft is formed by a curved wall forming a chamber a convergent section a throat section and a divergent section and a pair of parallel side plates, one of the side plates being movable to alter the area of the nozzle.

REFERENCES:
patent: 3154917 (1964-11-01), Williamson
patent: 3194014 (1965-07-01), Wilson
patent: 3973731 (1976-08-01), Thayer
patent: 4522357 (1985-06-01), Bains et al.
patent: 4690329 (1987-09-01), Madden
patent: 5098022 (1992-03-01), Thaye
patent: 5110047 (1992-05-01), Toews

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