Rear single-propeller type composite wing manned craft

A propeller and composite wing technology, applied in the field of aircraft, can solve the problems of low safety factor, high take-off and landing requirements, easy crash, etc., and achieve the effects of high wing structure strength, reduction of gravitational acceleration, and improvement of safety factor

Pending Publication Date: 2019-11-22
JIANGSU CHANGTAN ROBOT CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The traditional fixed wing has the advantages of fast flight speed, low energy consumption, etc., but it has the disadvantages that the main wing and the horizontal tail are not connected front and rear, the wing structure is not strong, easy to be damaged, the take-off and landing requirements are high, and the take-off and landing distance is long; the traditional vertical The take-off and landing aircraft has the advantages of convenient take-off and landing, but has the disadvantages of high energy consumption, low safety factor, poor load capacity, slow horizontal flight speed, and easy crash; although the current vertical take-off and landing fixed wing has the characteristics of convenient take-off and landing , but the controllability is not ideal when flying horizontally, and there are disadvantages such as large flight resistance, high energy consumption, and low safety factor.

Method used

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  • Rear single-propeller type composite wing manned craft
  • Rear single-propeller type composite wing manned craft
  • Rear single-propeller type composite wing manned craft

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Embodiment Construction

[0023] The present invention will be further described below in conjunction with the accompanying drawings.

[0024] Such as Figure 1 to Figure 5 As shown, a rear single propeller compound wing manned aircraft includes a rear single propeller compound wing aircraft, and the manned cabin is installed below the body.

[0025] Wherein, the rear single propeller compound wing aircraft includes a body 101, a compound lift wing 102 and a propeller 106 fixedly installed on both sides of the body 101; wherein, the body 101 is set as a deck platform; the compound lift The wing 102 has a built-in self-enclosed ducted fan 104, and a wing hinge (1027) is designed on the outside of the compound lift wing 102; a wing tail (1024) is also arranged at the tail end of the compound lift wing.

[0026] As a further improvement of the present invention, the propeller 106 is a variety of power structures such as electric propellers and oil-powered propellers.

[0027] As a further improvement of...

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PUM

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Abstract

The invention relates to a rear single-propeller type composite wing manned craft which comprises a rear single-propeller type composite wing craft and a manned bin, wherein the rear single-propellertype composite wing craft comprises a craft body, the composite lift force wings fixedly installed at the two sides of the craft body and a propeller, wherein the craft body is arranged as a deck platform, the self-sealing ducted fans are arranged in the composite lift force wings, and the wing hinges are designed at the outer sides of the composite lift force wings; the wing tails are further arranged at the tail ends of the composite lift force wings, the propeller is a screw propeller, and the manned bin is arranged below the craft body. The craft has the characteristics of short take-off and landing distances, high flight speed, high structural strength of the wings, energy storage wings, low flight energy consumption, long hang time, high safety and the like.

Description

technical field [0001] The invention relates to an aircraft, in particular to a rear single propeller composite wing manned aircraft, which belongs to the technical field of aircraft equipment. Background technique [0002] Existing aircraft are mainly divided into two categories: fixed-wing and vertical take-off and landing aircraft (such as helicopters and multi-rotors). Of course, there is also a vertical take-off and landing fixed-wing product. The traditional fixed wing has the advantages of fast flight speed, low energy consumption, etc., but it has the disadvantages that the main wing and the horizontal tail are not connected front and rear, the wing structure is not strong, easy to be damaged, the take-off and landing requirements are high, and the take-off and landing distance is long; the traditional vertical The take-off and landing aircraft has the advantages of convenient take-off and landing, but has the disadvantages of high energy consumption, low safety fac...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/28
CPCB64C27/28
Inventor 任曲波
Owner JIANGSU CHANGTAN ROBOT CO LTD
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