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Novel four-axis manned aircraft

An aircraft and a new type of technology, applied in the field of four-axis manned aircraft, can solve the problems of difficult storage, difficult transportation of four-axis manned aircraft, and taking up too much space.

Inactive Publication Date: 2021-07-30
GUANGDONG OCEAN UNIVERSITY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide a new type of four-axis manned aircraft to solve the problems in the above-mentioned background technology that the occupied space is too large and difficult to store, and it is difficult to transport the four-axis manned aircraft

Method used

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Embodiment Construction

[0021] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0022] see Figure 1-4 , the present invention provides a technical solution: a new type of four-axis manned aircraft, including a foldable landing gear 1, a foldable support 2, a lower end cover 3 of the four-axis manned aircraft sub-body, a fixed motor 4, and a motor cover 5 , rotating spiral wing 6, protective cover 7, fixed lithium battery 8, shock-absorbing seat cushion 9, protective tail 10, LED lighting device 11, GPS positioning system device 12, foot ...

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Abstract

The invention discloses a novel four-axis manned aircraft. The aircraft comprises a foldable undercarriage, a motor cover plate, a protective cover, a console and a four-axis manned aircraft sub-body upper end cover. The foldable undercarriage is installed at the bottom of the lower end cover of the four-axis manned aircraft sub-body, and the foldable support is installed on the lower end cover of the four-axis manned aircraft sub-body. The top end of the foldable support is connected with the fixed motor, the upper end of the motor cover plate is connected with the lower end of the fixed motor, the motor cover plate is connected with the rotating spiral wing, and the protective cover is installed on the rotating spiral wing. The novel four-axis manned aircraft has the characteristic that the console can carry people, so that the novel four-axis manned aircraft can be used as a novel traffic tool, has an entertainment effect and a function of relieving traffic jam, can effectively reduce commuting time, can be folded in a non-working state, is convenient to store, reduces occupied space, and is better in convenience and rapidness.

Description

technical field [0001] The invention relates to the technical field of four-axis aircraft, in particular to a novel four-axis manned aircraft. Background technique [0002] With the continuous development of science and technology and the continuous progress of society, people are using quadcopters more and more widely. As the most popular aircraft nowadays, quadcopters have become more and more popular among science enthusiasts and commercial companies. Attention, as early as World War II, the prototype of the manned four-axis aircraft had been designed, but because the control technology could not keep up, the aircraft could not be put into practical application due to instability. By around 2012, the international community generally believed that the four-axis aircraft The control of the quadcopter is no longer an academic research problem, but a mature technology, so the quadcopter has become possible as a new concept vehicle. In recent years, thanks to the development ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/08B64C1/06B64C25/10B64D27/24B64D47/02B64D43/00B64C27/14B64C27/20B64D11/06
CPCB64C1/063B64C25/10B64C27/08B64C27/14B64C27/20B64D27/24B64D43/00B64D47/02B64D11/0647
Inventor 纪然刘展旺王志鸿郑自强贾宝柱孙寒冰谭乐腾赖文川马浩楠
Owner GUANGDONG OCEAN UNIVERSITY
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