Variable area convergent-divergent nozzle

Details Variable area convergent-divergent nozzle Variable area convergent-divergent nozzle

B - Operations, Transporting

64

C

B64C 15/02 (2006.01) B64C 15/14 (2006.01) F02K 1/06 (2006.01) F02K 3/02 (2006.01)

Patent

CA 2118989

11 ABSTRACT VARIABLE AREA CONVERGENT-DIVERGENT NOZZLE A variable area con-di 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.

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