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Foldable manned vehicle

A kind of aircraft, folding technology, applied in the field of transportation, can solve the problems of high cost, aircraft crash and death, unsuitable for low-altitude flight, etc., and achieve the effect of saving space and energy

Active Publication Date: 2016-06-29
NORTH CHINA INST OF AEROSPACE ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] With the continuous development of the economy and the continuous improvement of people's living standards, more and more people are pursuing the comfort and enjoyment of life. Private jets are usually used by people as their own means of air transportation, but most of these private jets are expensive. , and bulky, not suitable for low-altitude flight, and most of them have only one engine and are not equipped with parachutes. Once damaged, tragic accidents will occur

Method used

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Embodiment Construction

[0017] The present invention will be further described below in conjunction with specific embodiments. The exemplary embodiments and descriptions of the present invention are used to explain the present invention, but not as a limitation to the present invention.

[0018] Such as figure 1 , figure 2 Shown, a kind of collapsible manned aircraft includes flight support 1, first motor 2, first propeller 3, auxiliary platform 4, first rectangular hinge support 5, auxiliary support 6, second motor 7, second Propeller 8, hydraulic cylinder 9, cylindrical pin 10, parachute release device 11, manned platform 12, second rectangular hinge support 13, the first motor 2 is fixed on the flight support 1. The first propeller 3 is connected to the output shaft of the first motor 2 , and the axis of the first propeller 3 coincides with the output shaft of the first motor 2 . The auxiliary platform 4 is fixed on the flight support 1 and is provided with a first rectangular hinge support 5 a...

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Abstract

The invention relates to a foldable manned vehicle which comprises a flying support, a first motor, a first propeller, an auxiliary platform, a rectangular hinge support, an auxiliary support, a second motor, a second propeller, a hydraulic cylinder, a columnar pin, a parachute releasing device, a manned platform and a second rectangular hinge support. The first motor is fixed on the flying support, the first propeller is connected with an output shaft of the first motor, the auxiliary platform is fixed on the flying support, the auxiliary support is hinged on the auxiliary platform through the first rectangular hinge support, the second motor is fixed at the tail end of the auxiliary support, the second propeller is connected with an output shaft of the second motor, one end of the hydraulic cylinder is hinged to the second rectangular hinge support on the auxiliary platform while the other end of the same is hinged on the auxiliary support, and the manned platform is fixed below the flying support. The foldable auxiliary support is arranged, so that space is saved; each propeller can be controlled solely, the second propeller on the auxiliary support can be used according to needs, and the objective of saving energy sources is achieved.

Description

technical field [0001] The invention relates to a manned aircraft, in particular to a foldable manned aircraft, which belongs to the field of transportation. Background technique [0002] With the continuous development of the economy and the continuous improvement of people's living standards, more and more people are pursuing the comfort and enjoyment of life. Private jets are usually used by people as their own means of air transportation, but most of these private jets are expensive. , and are bulky, not suitable for low-altitude flight, and most of them have only one engine and are not equipped with parachutes. Once damaged, tragic accidents will occur. Contents of the invention [0003] In view of the above problems, the present invention provides a foldable manned aircraft, which has multiple engines and a parachute release device, so it is highly safe, can take off and land vertically, has less space after folding, and is suitable for low-altitude flight of the pub...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/08B64C1/30
CPCB64C1/30B64C27/08
Inventor 吕玉梅李东阳陈丽缓韩旭黄坤
Owner NORTH CHINA INST OF AEROSPACE ENG
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