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An ion wind solid state aircraft and a control method thereof

An aircraft, ion wind technology, applied in the field of aircraft, can solve the problem of unable to achieve attitude control and so on

Pending Publication Date: 2019-09-13
HEFEI INSTITUTES OF PHYSICAL SCIENCE - CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, the existing ion wind aircraft use the Bifeld-Brown effect force generator only as a power source to drive the body to glide or hover, and cannot achieve attitude control with full degrees of freedom in pitch, roll, and yaw.

Method used

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  • An ion wind solid state aircraft and a control method thereof
  • An ion wind solid state aircraft and a control method thereof
  • An ion wind solid state aircraft and a control method thereof

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Embodiment Construction

[0031] The present invention will be further described below in conjunction with accompanying drawing:

[0032] Such as Figure 1-Figure 5 A kind of ionic wind solid-state aircraft shown, comprises fuselage 5 and first force generator 1, the second force generator 2, the 3rd force generator 3 that are arranged successively along fuselage 5 periphery and all tilt towards fuselage 5 and the fourth force generator 4; the four end angles of the fuselage 5 are respectively connected with the first force generator 1, the second force generator 2, the third force generator 3 and the fourth force generator through a connecting rod 6 The generators 4 are connected; the first force generator 1, the second force generator 2, the third force generator 3 and the fourth force generator 4 have the same structure, and all include small electrodes 7 arranged sequentially from top to bottom And the large electrode 8 and a number of uniformly distributed columns connected between the small elec...

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Abstract

The invention relates to an ion wind solid state aircraft and a control method thereof. The aircraft includes a fuselage and a first force generator, a second force generator, a third force generatorand a fourth force generator that are sequentially arranged along the outer circumference of the fuselage and both are inclined toward the fuselage. The first force generator, the second force generator, the third force generator and the fourth force generator have the same structure, and each includes a small electrode, a large electrode and columns. The small electrode is connected to a positiveelectrode of a high voltage power supply, and the large electrode is connected to a grounding electrode of the high voltage power supply. The ion wind solid state aircraft of the invention is based on the Bifeld-Brown effect, and through the four inclined force generations, a single Bifeld-Brown effect force generator can generate a two-dimensional effect, namely: the propulsive force that causesthe body to rise upwards and the yaw moment that causes the body to spin, thereby achieving a controlled flight of full-degree of freedom of pitch, roll and yaw.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to an ion wind solid-state aircraft and a control method thereof. Background technique [0002] Aviation aircraft is an indispensable means of transportation in modern society and is widely used in military and civilian fields. Traditional aviation aircraft include: fixed-wing, rotary-wing, and flapping-wing aircraft, which generally use fuel-powered, electric-powered engines to drive propellers, turbofans, flapping wings and other movable parts to generate propulsion, or use chemical fuel combustion injection to form Propulsion enables flight. This type of aircraft has many defects such as complicated mechanism, low energy conversion efficiency, and high noise. [0003] The ion wind solid-state aircraft is a new type of aircraft without moving parts. Due to the use of the Bifeld-Brown effect force as the propulsion force, it has the characteristics of high energy conversion effi...

Claims

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Application Information

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IPC IPC(8): B64C17/00
CPCB64C17/00
Inventor 陈池来马贺李山刘友江胡俊徐青王晗
Owner HEFEI INSTITUTES OF PHYSICAL SCIENCE - CHINESE ACAD OF SCI
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