Model aircraft variable geometry nozzle

Details Model aircraft variable geometry nozzle Model aircraft variable geometry nozzle

1992-04-13

1993-04-06

Barefoot, Galen

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

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

244 53R, 446 56, F02K 130

Patent

active

051996430

ABSTRACT:
The present invention relates to a method and apparatus for providing an operable variable geometry exhaust nozzle for scale model jet aircraft. A multiplicity of hinged, overlapping, nozzle blades circumferentially surround the exhaust nozzle thereby providing a divergent cylindrical exhaust nozzle that may be convergingly reduced to a conical configuration by action of a remotely controlled solenoid.

REFERENCES:
patent: 2545586 (1951-03-01), Pollak
patent: 2634578 (1953-04-01), Kallal
patent: 2693078 (1954-11-01), Laucher
patent: 2865165 (1958-12-01), Kress
patent: 2974477 (1961-03-01), Egbert et al.
patent: 4196856 (1980-04-01), James
patent: 4307857 (1981-12-01), Godbersen
patent: 4502636 (1985-03-01), Nightingale et al.
patent: 4850535 (1989-07-01), Ivie

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