Aeronautics and astronautics – Aircraft – heavier-than-air – Helicopter or auto-rotating wing sustained – i.e. – gyroplanes
Patent
1995-10-16
1998-01-06
Grant, William
Aeronautics and astronautics
Aircraft, heavier-than-air
Helicopter or auto-rotating wing sustained, i.e., gyroplanes
244134D, B64D 1512
Patent
active
057045674
ABSTRACT:
A blade de-icer for rotary wing aircraft comprises magnets placed around rotor mast and coils with laminated plates installed at the blade cuff of each rotor blade, in sufficient proximity to produce a high voltage, high current pulse every time a magnet and a coil pass each other while the rotor is turning. Electrically conductive cable or wire carries the current down each rotor blade to heating elements which melt any accreted ice on the blade. In one embodiment, magnetic metals are used. In another embodiment, electromagnets are used. In each embodiment, difficult switches for turning the de-icer on and off are provided.
REFERENCES:
patent: 2429061 (1947-10-01), Hunter
patent: 2444557 (1948-07-01), Eaton
patent: 2491172 (1949-12-01), Forsyth
patent: 2678181 (1954-05-01), Geyer et al.
Bush Freddie M.
Grant William
Lamming John H.
The United States of America as represented by the Secretary of
Tischer Arthur H.
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