FIELD: aviation.
SUBSTANCE: aircraft includes a control unit to output a pulsed or continuous voltages, a rectangular chamber with a shock-absorber inside with roundings between the walls. Two semicircular magnets are disposed at the chamber end rigidly connected with its side walls behind the springs of the spring valves with rounding at the end located in front of these roundings between the shock-absorber walls of the chamber. The entrances of the semicircular magnets are connected to the exits of the control unit.
EFFECT: increased speed of the aircraft.
1 dwg
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Authors
Dates
2017-04-12—Published
2016-03-14—Filed