Saucer

A saucer-shaped aircraft and ring-shaped technology, applied in aircraft, vertical take-off and landing aircraft, motor vehicles, etc., can solve the problems of aircraft structure complexity, low flight efficiency, poor controllability, etc., and achieve good fuselage balance and flight drive Unified force and good controllability

Inactive Publication Date: 2017-02-01
李广成
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The disc-shaped aircraft with this structure, due to the existence of components such as propellers and turbine engines, makes the aircraft structure more complicated, the aircraft is heavier, the flight efficiency is low, and the controllability is not good

Method used

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Embodiment Construction

[0014] Below in conjunction with accompanying drawing and specific embodiment the present invention is described in further detail:

[0015] combine figure 1 As shown, the saucer-shaped aircraft includes an upper fuselage 1, a lower fuselage 2, a rotary drive mechanism 3 and a power source 5.

[0016] Both the upper fuselage 1 and the lower fuselage 2 adopt a disc structure.

[0017] An organic space 6 is formed between the upper fuselage 1 and the lower fuselage 2 .

[0018] The rotation drive mechanism 3 is used to drive the upper body 1 to rotate forward. The axis of rotation of the upper fuselage 1 is the central axis of the saucer-shaped aircraft.

[0019] Under the condition of no external force, due to the conservation of angular kinetic energy, the lower fuselage 2 will rotate in the opposite direction, and the rotation axes of the upper fuselage 1 and the lower fuselage 2 coincide.

[0020] The forward direction and reverse direction here mean that when the forwar...

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PUM

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Abstract

The invention discloses a saucer-shaped aircraft. The basic structure of the saucer-shaped aircraft comprises an upper aircraft body, a lower aircraft body and a rotation driving mechanism, wherein an aircraft body space is formed between the upper aircraft body and the lower aircraft body; the rotation driving mechanism is used for driving the upper aircraft body to rotate forwards, and under the condition of no stress, the lower aircraft body can rotate reversely because of conservation of angular kinetic energy; the lower aircraft body is provided with a plurality of air flues; one end of each air flue is communicated with the aircraft body space, and the other end of each air flue is communicated with atmosphere; each air flue is internally provided with a turbofan respectively; an annular magnetic suspension guide rail is arranged between the upper aircraft body and the lower aircraft body; the power source is used for providing required power for the rotation driving mechanism, the turbofans and the magnetic suspension guide rail. Compared with the prior art, the saucer-shaped aircraft is simple in operation principle, and is high in lift force; the lift force of the aircraft and the flight driving force are integrated; the appearance of the aircraft body is a symmetrical streamline type; the aircraft body is good in balance property, can perpendicularly take off and land, hover at random and fly at a high speed; because components, such as a propeller, a turbine engine are omitted, the saucer-shaped aircraft is simple in structure, and is good in controllability.

Description

technical field [0001] The invention relates to a dish-shaped aircraft. Background technique [0002] At present, most of the saucer-shaped aircraft in the prior art realize the lifting function of the aircraft by configuring propellers and turbine engines. This kind of saucer-shaped aircraft is the same as the flight principle of existing aircraft, which is to change the upper and lower flow rates of the wings or propellers. And provide flight power. With the saucer-shaped aircraft of this structure, due to the existence of components such as propeller and turbine engine, the structure of the aircraft is relatively complicated, the aircraft is heavy, the flight efficiency is low, and the maneuverability is not good. Contents of the invention [0003] The object of the present invention is to propose a kind of saucer-shaped aircraft, and it adopts following technical scheme: [0004] A saucer-shaped aircraft, comprising an upper fuselage, a lower fuselage, a rotary drive...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C39/06B64C29/00
Inventor 李广成
Owner 李广成
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