Aircraft spraying system and method

Details Aircraft spraying system and method Aircraft spraying system and method

1978-05-15

1979-11-27

Love, John J.

Fluid sprinkling, spraying, and diffusing

Processes

Of discharge modification of flow varying

239171, B05B 1702

Patent

active

041757017

ABSTRACT:
An aircraft spraying system and method drives a turbine motor by pressurized bleed airflow from the working cycle of a turbomachinery-type propulsion engine driving the aircraft, and a control system regulates the pressure of bleed air flow to the motor to vary the rate of liquid distributed from the aircraft.

REFERENCES:
patent: 2924040 (1960-02-01), White et al.
patent: 3061247 (1962-10-01), Hyde
patent: 3351305 (1967-11-01), Warner
patent: 3362643 (1968-01-01), Larson et al.
patent: 3455511 (1969-07-01), Fedorenko
patent: 3494423 (1970-02-01), Stansbury et al.
patent: 3547000 (1970-12-01), Haberkorn et al.
patent: 3604509 (1971-09-01), Sachnik
patent: 3774871 (1973-11-01), Semmes et al.

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