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Fluid-driven centrifugal force difference aircraft

A fluid-driven, centrifugal force technology used in the field of aircraft to solve problems such as unstable flight and inability to fly

Inactive Publication Date: 2019-06-21
徐航
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Existing aircraft are all driven by aerodynamic force to lift into the air. In bad weather, the airflow is unstable, and the flight will be unstable. In outer space, there is no way to fly because there is no air.

Method used

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  • Fluid-driven centrifugal force difference aircraft
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Examples

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Effect test

Embodiment 1

[0016] A fluid-driven centrifugal force difference aircraft, comprising a body 2 and at least one variable centrifugal force power unit installed on the body 2, the variable centrifugal force power unit includes a forced track groove that can change the radius of fluid movement, so that the movement of the fluid A centrifugal force difference is generated, and the resulting centrifugal force difference is used as the flight power of the aircraft.

[0017] The power source of fluid movement is directly driven by mechanical force or driven by electromagnetic force outside the forced track groove. The simplest structure is to set a variable centrifugal force power unit on the body.

Embodiment 2

[0019] Such as figure 1 As shown, as a structural design directly driven by a specific mechanical force in Embodiment 1, the variable centrifugal force power unit includes a drive motor installed on the body and a forced track body 1 installed on the body 2, and the forced track body 1 is provided with a forced track groove, the output shaft of the driving motor 4 is located in the forced track groove and the impeller 5 is installed, and a high-density fluid is set in the forced track groove, which is driven by the impeller 5 for high-speed flow.

[0020] The fluid is several solid spheres or liquid.

[0021] The forced track body 1 is provided with a track sealing cover 3 outside the forced track groove, or the forced track body 1 is set as a pipe containing a forced track groove. The impeller 5 is connected to the output shaft of the driving motor 4 and is driven by the motor to rotate at high speed. The impeller 5 drives the high-density fluid (solid ball or liquid) in the...

Embodiment 3

[0024] As a further structural design of Embodiment 2, the cross-section of the body is one of circular, elliptical or polygonal.

[0025] Such as figure 1 As shown, four variable centrifugal force power units are provided, and the body cross-section is a quadrilateral, and the variable centrifugal force power units are evenly distributed on four sides of the body cross-section.

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Abstract

The invention discloses a fluid-driven centrifugal force difference aircraft, comprising an airframe and at least one variable centrifugal force power unit mounted on the airframe; the variable centrifugal force power unit comprises a forced rail slot capable of changing the moving radius of fluid, so as to enable the movement of the fluid to generate a centrifugal force difference, and the generated centrifugal force difference is used as the flying power of the aircraft. According to the fluid-driven centrifugal force difference aircraft, by driving the fluid to move in the forced rail slotcapable of changing the moving radius of fluid, the movement of the fluid generates the centrifugal force difference, the generated centrifugal force difference is used as the flying power of the aircraft, and a different aircraft structure is given.

Description

technical field [0001] The invention relates to an aircraft, in particular to a fluid-driven centrifugal force difference aircraft. Background technique [0002] Existing aircrafts are all driven by aerodynamic force to lift into the air. In bad weather, the airflow is unstable, and the flight will be unstable. In outer space, there is no way to fly because there is no air. If there is an aircraft that is not bound by air, this phenomenon can be changed. The inventor proposed several structures in the previous application. The centrifugal force power unit installed on both sides of the aircraft frame is driven by two sets of transmission devices, so that the centrifugal force power unit can continuously adjust the rotation radius of the centrifugal force generating device while rotating. , so that a centrifugal force difference is generated between the devices, and the centrifugal force difference is used as the driving force to drive the aircraft. In order to find a bette...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D27/02
Inventor 徐航
Owner 徐航
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