FIELD: aviation.
SUBSTANCE: atmocpheric compressor jet-powered vehicle contains the fuselage (1), the wings (5) with ailerons, fin, rudders of rotation and height. The fuselage has a housing (17), wherein there is the crankshaft (18). The power modules are installed on the wings, where the rectangular cylinders (28) are mounted, having the piston (29), and the length of the cylinders is parallel to the fuselage. There are the flow channels (32) from both sides of the cylinders, which from the rear side are alternately opened or closed by the curtains (25). The counter air during the flight enters into the closed flow channels and presses on the pistons, which are moving in the cylinders across the flow channels in the forward and reverse directions, depending on the curtains position. The air goes out from the opened channels. The pistons, connected by the rods with the crankshaft, rotate it, and the rotary compressor (8) and the current generator (14) as well. The compressor captures the air from the fuselage front and discharges it into the heating chamber (12), where the air is heated from the electric heaters (13) and goes out from the nozzle (15) with high speed.
EFFECT: reduction of the drag.
2 dwg
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TWO-STROKE ENGINE OF INTERNAL HEATING OF WORKING MEDIUM | 2011 |
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RU2249541C2 |
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ASYMMETRICAL MECHANICAL ENGINE | 2005 |
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SYMMETRICAL MECHANICAL ENGINE | 2005 |
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|
RU2260699C1 |
Authors
Dates
2017-04-28—Published
2016-04-29—Filed