Patent
1987-11-23
1991-05-14
Bennet, Henry A.
98 208, B60H 100
Patent
active
050146068
ABSTRACT:
A helicopter windshield defogger and/or deicer system is discussed which is connectable with a high pressure, high temperature air supply from the compression stage of a helicopter turbine engine. The system utilizes a coanda ejector type nozzle to mix and distribute high temperature bleed air and aspirated cabin air to a dispersal shroud fixed adjacent to the helicopter windshield.
REFERENCES:
patent: 3832939 (1974-09-01), Kakei et al.
patent: 4693172 (1987-09-01), Harvey
Steiner James R.
Steiner Norman F.
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