Aeronautics and astronautics – Aircraft structure – Ice prevention
Patent
1986-02-24
1988-03-29
Peters, Jr., Joseph F.
Aeronautics and astronautics
Aircraft structure
Ice prevention
244134A, B64D 1500
Patent
active
047338342
ABSTRACT:
A deicer control circuit wherein a pressurized air source is connected to control valves and a regulating valve. Such regulating valve has a vacuum line output line that is also connected to such control valves. The control valves, on actuation by a timer, will sequence the pressure line and the vacuum line to alternately inflate and deflate the deicer units. The control valves also provide a sealing off or locking in of the pressurized deicer units in this sequence in response to a pressure sensor.
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Fiorito Lynn M.
Januszkiewicz Joseph
Peters Jr. Joseph F.
The B. F. Goodrich Company
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