Convergent flap bearing with integral hold-down device

Fluid sprinkling – spraying – and diffusing – Reaction motor discharge nozzle – With means controlling amount – shape or direction of...

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244216, B64C 1500, B64C 938

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active

047843268

ABSTRACT:
An exhaust nozzle of the type utilized with high performance supersonic aircraft is disclosed. The exhaust nozzle is variable between convergent and convergent/divergent geometries, as well as in aperture size. A bearing guiding segments of the nozzle is held within a roller track by an integral hold-down bracket.

REFERENCES:
patent: 4456178 (1984-06-01), Jones et al.
patent: 4552309 (1985-11-01), Szuminski et al.

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