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Flying saucer

A technology of flying saucer and saucer frame, applied in the field of flying saucer, can solve the problems of complex structure of air supply device, poor stability of aircraft, increase of aircraft manufacturing cost and self-weight, etc.

Pending Publication Date: 2020-03-24
杨义华
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] In recent years, many aircrafts that can take off and land vertically have appeared one after another, such as: a jet aircraft that can take off and land vertically, patent number: 2013100717433 Although this technology can achieve hypersonic flight, the structure of the air supply device of the aircraft is complicated, which greatly increases the aircraft's Manufacturing cost and self-weight, when flying at supersonic speed, the stability of the aircraft is poor when the aircraft makes a large-angle turn

Method used

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  • Flying saucer

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Embodiment Construction

[0024]The object of the present invention is achieved in that when the flying saucer takes off, first the flying spray nozzle in the bottom rotating cylinder is pushed out outwards, and the take-off nozzle is adjusted under the fixed jet valve of the engine to make it hermetically connected. Then start the driving motor on the bottom surface of the flying saucer, the driving motor drives the rotary air supply valve of the engine to rotate, and at the same time drives the air supply acceleration device in the central shaft below to start working, connecting the top plane with the circular air supply pipe to increase the intake air The supply pressure of the device through the longitudinal air supply pipe ... the control valve ... enters the pressurized air storage tank below. When the rotary air supply valve speed of the engine reaches 3000 rpm, the air supply and oil supply devices of the engine start to work, and then the take-off nozzle starts to spray air downward. At the s...

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Abstract

A flying saucer comprises a flying saucer body, the dish rack is provided with a conical signal transmitter-receiver; the aircraft comprises an acceleration air inlet device, a front windward power supply device, a direction air supply receiver, an air supply acceleration device, a center shaft, a pressurization air storage tank, a windward power supply air storage tank, an oil storage tank, an air supply system, an oil supply system, a starting system, rotary air supply, an air injection control valve, a control system, two engines, a take-off nozzle, a flight nozzle, auxiliary nozzles, a cab, passenger compartments and take-off wheels. The dish rack comprises a dish top face, a cylindrical frame, a dish bottom face and a rotating cylinder. A dish top surface is arranged above the dish rack, a cylindrical frame is arranged in the middle, and a dish bottom surface is arranged below the dish rack. The top face and the bottom face of the plate are each provided with a plane part, a rotating cylinder, an engine installation face and a slope part. The acceleration air inlet device comprises a conical signal transceiver, a circular-truncated-cone-shaped acceleration air inlet hole, a cylindrical air inlet hole, a connecting face, a front windward power supply device and an air supply half pipe.

Description

technical field [0001] The invention relates to a flying saucer and belongs to the technical field of aviation equipment. Background technique [0002] In recent years, many aircrafts that can take off and land vertically have appeared one after another, such as: a jet aircraft that can take off and land vertically, patent number: 2013100717433 Although this technology can achieve hypersonic flight, the structure of the air supply device of the aircraft is complicated, which greatly increases the aircraft's Manufacturing cost and self-weight, when flying at supersonic speed, the stability of the aircraft is poor when the aircraft is turning at a large angle. Contents of the invention [0003] In order to solve the problems existing in the prior art, the present invention relates to a kind of air supply device that can provide high-pressure gas for the flying saucer engine when it takes off, and has a simple structure and no energy consumption for supercharging. The butterf...

Claims

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Application Information

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IPC IPC(8): B64C39/00B64D27/16
CPCB64C39/001B64D27/16
Inventor 杨义华杨雪静杨济东
Owner 杨义华
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