Device for control of an aircraft

Details Device for control of an aircraft Device for control of an aircraft

1976-09-13

1978-07-11

Love, John J.

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

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

B64C 1504

Patent

active

040996719

ABSTRACT:
Control apparatus for an aircraft is provided which includes a gas-controlled housing disposed downstream of a gas turbine jet propulsion supply system. A propulsion nozzle is provided at the downstream end of a tubular member extending from the control housing in alignment with a longitudinal axis of the engine system. Lateral control outlets extend in opposite lateral directions from the gas-controlled housing. The flow of gases selectively to one or both of the control outlets and to the propulsion nozzle is effected by way of two part-spherical sector control valve members which are mounted for pivotal movement about an axis running perpendicular to the longitudinal axis. The control valve members are configured for selectively blocking the flow of propulsion gases to the propulsion nozzle and the respective lateral control outlets.

REFERENCES:
patent: 2849861 (1958-09-01), Gardiner et al.
patent: 3196608 (1965-07-01), Tindale
patent: 3280560 (1966-10-01), Marchant et al.
patent: 3348380 (1967-10-01), Rees
patent: 3833187 (1974-09-01), Kahler et al.
patent: 3837411 (1974-09-01), Nash et al.
patent: 3989193 (1976-11-01), Vedova et al.

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