Air-space-ground effect wing helicopter

Abstract

The invention discloses an air-space-ground effect wing helicopter which comprises a propeller outer ring assembly, servo motors capable of being installed on an aircraft body are arranged on the two sides of the outer ring assembly, a center shaft type aircraft jet engine is fixed to the center of an upper supporting frame of the outer ring assembly, and a pipeline type center shaft is fixed to the center of a lower supporting frame of the outer ring assembly. A cylindrical blade connecting and fixing ring is arranged at the top of each blade, a vertical resistance-increasing lower nozzle is arranged on the rear lower portion of each blade, detachable fan-shaped blades are arranged on the outer side of each cylindrical blade connecting and fixing ring, and blade connecting and fixing rings are arranged at the top of each group of blades. The lower portion of the inner wall of each connecting and fixing ring is provided with a forward thrust horizontal auxiliary nozzle, the upper edge and the lower edge of each connecting and fixing ring are provided with magnetic force driving systems which make contact with the magnetic force driving systems, the upper supporting frame and the lower supporting frame are provided with induction electromagnets, and the connecting portions of the blades and the connecting and fixing rings are provided with horizontal main nozzles. The middle section of the lower portion of each rotor blade is provided with a plurality of resistance-increasing connecting and fixing rings which are hollow. And the lower part of the inner wall of the resistance-increasing connecting and fixing ring is provided with a forward thrust horizontal auxiliary nozzle.

Description

technical field [0001] The invention relates to a propeller-type aerial lifting power device that utilizes electromagnetic drive and various jet engines to drive or drive propellers alone. Background technique [0002] Existing traditional rockets take too long to prepare for the launch of the spacecraft before flight, and cannot be launched at any time. Moreover, the thrust of the existing rockets has basically reached the limit and cannot meet the needs of future space launches. The spacecraft after the rocket is launched can only play the role of ferrying, and cannot launch and return to the earth or other planets maneuverably, and launch and land. too fast, unfavorable control, etc. [0003] The existing ground-effect-wing aircraft cannot fly high, and the weather and geographical conditions are high, and the kinetic energy of the body needs to be used to achieve ground-effect flight, and cannot spin to stop or helicopter. [0004] Existing helicopters use complex mech...

AI Technical Summary

Problems solved by technology

[0002] The preparation time before the flight of the existing traditional rocket launch spacecraft is too long, and it cannot be launched at any time

Moreover, the thrust of existing rockets has basically reached its limit and cannot meet the needs of future space launches. The spacecraft after rocket launch can only play the role of ferry, and cannot be launched maneuverably and return to the earth or other planets. The speed is too fast, unfavorable control, etc.

[0003] Existing ground-effect wing aircraft cannot soar high in the sky, and the weather and geographical conditions require high requirements. It needs to use the kinetic energy of the body to achieve ground-effect flight, and cannot spin-stop or helicopter

[0004] Existing helicopters use complex mechanically driven propellers to obtain lift. The wings require high strength and should be broken, and the flight speed is slow, the flight altitude is low, and the weather conditions are high.

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