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Personal vertical take-off and landing air vehicle

A vertical take-off and landing, aircraft technology, applied in the field of aircraft, can solve problems such as traffic jams, and achieve the effect of easy parking

Pending Publication Date: 2018-06-19
SHANGHAI JIAO TONG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, in economically developed cities and regions, traffic jams are becoming more and more serious, which brings a lot of inconvenience to people's lives.
However, traditional public transportation is difficult to solve the above problems. Therefore, safe, economical and flexible personal flying vehicles have become the expectation of more and more people.

Method used

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  • Personal vertical take-off and landing air vehicle

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Embodiment 1

[0024] Such as figure 1 , image 3 with Figure 5 As shown, the present embodiment includes: a spindle-shaped fuselage 1, folding wings 2, steering engine 3 and noise reduction equipment, wherein: the noise reduction equipment is arranged in the spindle-shaped fuselage 1 and is connected with the aircraft electronic control system, and the steering engine 3. It is arranged at the tail of the spindle-shaped fuselage 1 and connected by a pin shaft. The folding wing 2 is arranged on both sides of the spindle-shaped fuselage 1. The folding wing 1 is fixed with a four-blade rotor 4;

[0025] The folding wings 2 on both sides of the spindle-shaped fuselage 1 are connected by connecting rods, and the connecting rods are fixed on the rotating mechanism in the spindle-shaped fuselage 1; Wing fixed end 21 and the wing expansion end 22 that is hingedly connected with wing fixed end 21;

[0026] The steering motor 3 rotates around the pin shaft within 90° below the horizontal axis of t...

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Abstract

The invention provides a personal vertical take-off and landing air vehicle, and belongs to the technical field of air vehicles. The personal vertical take-off and landing air vehicle comprises a spindle-shaped fuselage, folding wings, a steering engine and noise reduction equipment, wherein the noise reduction equipment is arranged in the spindle-shaped fuselage and connected with an air vehicleelectrical control system, the steering engine is arranged at the tail of the spindle-shaped fuselage, and the steering engine is connected with the tail of the spindle-shaped fuselage through a pin shaft; the folding wings are arranged on the two sides of the spindle-shaped fuselage, and four blade rotor wings are fixed to the folding wings in the width direction; the folding wings on the two sides of the spindle-shaped fuselage are connected through a connecting rod, and the connecting rod is fixed to a rotating mechanism of the spindle-shaped fuselage; the folding wings comprise wing fixingends connected with the connecting rod and wing unfolding ends in hinged connection with the wing fixing ends; and the steering engine rotates around the pin shaft within the range of 90 degrees below a horizontal axis of the spindle-shaped fuselage. According to the personal vertical take-off and landing air vehicle, the wings can be folded, the thrust direction can be changed, and the personalvertical take-off and landing air vehicle has the advantage of low noise and is suitable for urban traffic demands.

Description

technical field [0001] The invention relates to a technology in the field of aircraft, in particular to a vertical take-off and landing personal aircraft. Background technique [0002] Transportation is an important part of modern society, especially commercial railways and aviation have provided passengers with more and more comfortable and flexible choices in long-distance travel. However, in economically developed cities and regions, traffic jams are becoming more and more serious, which brings a lot of inconvenience to people's lives. However, traditional public transportation is difficult to solve the above problems, so safe, economical and flexible personal flying vehicles have become the expectation of more and more people. Contents of the invention [0003] Aiming at the shortcomings of the prior art, such as large floor space or insufficient battery life and short flight range, the present invention proposes a vertical take-off and landing personal aircraft, the ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C3/56B64C27/28
CPCB64C3/56B64C27/28
Inventor 罗佳杰杜博涵宋文滨
Owner SHANGHAI JIAO TONG UNIV
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