Aircraft spraying system and method
US4175701A · kind A · utility
9Cited by
9References
18Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | May 15, 1978 |
| Grant date | Nov 27, 1979 |
| Priority date | — |
| Expiry date | May 15, 1998 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF02C6/08
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
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.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.