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Rear single-ducted fan type composite wing freight aircraft

A technology of ducted fan and compound wing, which is applied in the field of aircraft equipment and rear single ducted fan compound wing cargo aircraft, which can solve the problems of low wing structure strength, slow horizontal flight speed, and unsatisfactory controllability, etc. , to achieve the effects of high wing structure strength, fast flight speed, and convenient group flight

Inactive Publication Date: 2018-11-09
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-ducted fan type composite wing freight aircraft
  • Rear single-ducted fan type composite wing freight aircraft
  • Rear single-ducted fan type composite wing freight 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 Shown, a rear single duct fan type compound wing cargo aircraft is characterized in that it comprises a rear single duct fan type compound wing aircraft, and the cargo compartment 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 s...

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PUM

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Abstract

The invention discloses a rear single-ducted fan type composite wing freight aircraft. The rear single-ducted fan type composite wing freight aircraft consists of a rear single-ducted fan type composite wing aircraft and a freight cabin, wherein the rear single-ducted fan type composite wing freight aircraft comprises a body, composite lift wings fixedly arranged at the two sides of the body, anda ducted fan propeller; the body is set as a deck platform; the composite lift wings are internally provided with self-closed duct fans; wing hinges are designed at the outer sides of the composite lift wings; the freight cabin is arranged under the body. The rear single-ducted fan type composite wing freight aircraft disclosed by the invention has the characteristics of short takeoff and land distance, fast flying speed, high structural strength of the wings, energy storage of the wings, low flying energy consumption, long hanging time and high safety and the like.

Description

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

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/20B64C27/26B64C37/02
CPCB64C27/20B64C27/26B64C37/02B64U50/14
Inventor 任曲波
Owner JIANGSU CHANGTAN ROBOT CO LTD
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