FIELD: aeronautical engineering. SUBSTANCE: device has protector 2 with chamber 3 and conducting elements 7 and 8 connected in series. Protector is secured on outer surface of metal cover 4. When current pulse passes through band conducting elements, it is converted into pulse of force which breaks ice on outer surface of flying vehicle. EFFECT: reduction of aerodynamic drag of flying vehicle through reduced thickness of protector. 4 dwg
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Authors
Dates
1995-08-20—Published
1990-05-18—Filed