High pressure spray system

Aeronautics and astronautics – Aircraft structure – Material discharging and diffusing

Reexamination Certificate

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Reexamination Certificate

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06886784

ABSTRACT:
A combination of an aircraft and spraying apparatus for spraying suspensions or solutions having predetermined characteristics independent of the speed of the aircraft, the apparatus consisting of a mounting frame attached to the underside of the aircraft, a plurality of bearing braces attached to the frame and a propeller shaft mounted through the bearing braces. A full feathering propeller is mounted on the forward end with a control running to the cockpit of the aircraft, and a rotary piston type high pressure pump connected to the aft end of the propeller. The input of the pump is connected to a supply tank in the aircraft and the output is connected to a spray boom. The spray nozzles consist of high pressure impingement nozzles.

REFERENCES:
patent: 2048847 (1936-07-01), Desmet
patent: 2537251 (1951-01-01), Wilson
patent: 2665092 (1954-01-01), Sands
patent: 2924040 (1960-02-01), White et al.
patent: 3398893 (1968-08-01), Rasovich et al.
patent: 3589613 (1971-06-01), Saladin
patent: 3945572 (1976-03-01), Bockenstette, II
patent: 4034915 (1977-07-01), Garner
patent: 4090567 (1978-05-01), Tomlinson
patent: 20010019090 (2001-09-01), Horev

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