Rear single-duct fan type combined wing manned aircraft

A ducted fan and composite wing technology, which is applied to the rear single ducted fan type composite wing manned aircraft and aircraft equipment field, can solve the problem of low wing structure strength, unsatisfactory controllability, slow horizontal flight speed, etc. problem, to achieve the effect of high wing structure strength, convenient cluster flight, and fast flight speed

Inactive Publication Date: 2018-09-18
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-duct fan type combined wing manned aircraft
  • Rear single-duct fan type combined wing manned aircraft
  • Rear single-duct fan type combined wing manned aircraft

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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 As shown, a rear single duct fan type compound wing manned aircraft is characterized in that it comprises a rear single duct fan type compound wing aircraft, and the manned cabin is installed below the body.

[0025] Wherein, the rear single-duct fan type composite wing aircraft includes a body 101, a composite 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 The compound lift wing 102 has a built-in self-enclosed ducted fan 104, and the outside of the compound lift wing 102 is designed with a wing hinge 1028; The composite lift wing 102 is respectively set as a magnetic suction type automatic interlock interface male head 1026 and a magnetic suction type automatic interlock interface female head 1027; The interlocking interface female heads 1027 have the sa...

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PUM

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Abstract

The invention provides a rear single-duct fan type combined wing manned aircraft which is composed of a rear single-duct fan type combined wing aircraft and a manned cabin. The rear single-duct fan type combined wing aircraft comprises an aircraft body, combined lift force wings fixedly installed on the two sides of the aircraft body and a ducted fan propeller. The aircraft body is arranged to bea deck platform. Self-closed ducted fans are arranged in the combined lift force wings, and wing hinges are designed on the outer sides of the combined lift force wings. The manned cabin is installedbelow the aircraft body. The rear single-duct fan type combined wing manned aircraft has the beneficial effects of being short in take-off and landing distance, high in flight speed, high in wing structural strength, capable of storing energy through the wings, low in flight energy consumption, long in hang time, high in safety and the like.

Description

technical field [0001] The invention relates to an aircraft, in particular to a rear single-duct fan-type compound-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 ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/22B64C27/20
Inventor 任曲波
Owner JIANGSU CHANGTAN ROBOT CO LTD
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