Triple axis thrust vectoring exhaust nozzle

Details Triple axis thrust vectoring exhaust nozzle Triple axis thrust vectoring exhaust nozzle

1988-05-24

1989-11-07

Kashnikow, Andres

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

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

60228, 23926541, 23926543, 244 52, F02K 112

Patent

active

048786179

ABSTRACT:
A variable area, convergent-divergent (10) nozzle for directing the flow of exhaust gas from an aircraft turbine engine to achieve thrust vectoring about yaw, pitch and roll axes includes a convergent section (16) and a divergent section (18) each comprised of hingedly connected planar members (201-214, 301-322) selectively positioned by actuators (101-114) for defining deformable gas directing flow ducts.

REFERENCES:
patent: 2593420 (1952-04-01), Diehl
patent: 3007304 (1961-11-01), Wotton et al.
patent: 3133412 (1964-05-01), Westley
patent: 3174582 (1965-03-01), Duthion et al.
patent: 3615052 (1971-10-01), Tumavicus
patent: 3976160 (1976-08-01), Hoch et al.
patent: 4707899 (1987-11-01), Singer

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