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Rear single ducted fan type composite-wing aircraft with zero thrust composite ailerons and additional wings

A ducted fan and composite wing technology, which is applied in the field of rear single ducted fan compound wing aircraft and aircraft equipment, can solve the problems of low wing structure strength, unsatisfactory controllability, and slow horizontal flight speed, etc. To achieve the effect of expanding the wing area, increasing the lift force and flying fast

Inactive Publication Date: 2018-12-07
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 aircraft with zero thrust composite ailerons and additional wings
  • Rear single ducted fan type composite-wing aircraft with zero thrust composite ailerons and additional wings
  • Rear single ducted fan type composite-wing aircraft with zero thrust composite ailerons and additional wings

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Embodiment Construction

[0027] The present invention will be further described below in conjunction with the accompanying drawings.

[0028] like figure 1 As shown, it comprises a rear single-ducted fan-type composite wing aircraft, non-thrust self-powered auxiliary wings assembled on both sides of its wing, and additional wings 114;

[0029] 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 outer side of the compound lift wing 102 is designed with a wing hinge 1028; the propeller 106 is a ducted fan propeller; Road fan 104, one or both sides of the non-thrust self-powered aileron are provided with an electro-hydraulic interface 1036 and a wing hinge 1028, and are movably connected with the compound lift wing 102 through the wing hinge 1028; ...

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Abstract

The invention provides a rear single ducted fan type composite-wing aircraft with zero thrust composite ailerons and additional wings. The rear single ducted fan type composite-wing aircraft with thezero thrust composite ailerons and the additional wings comprises a rear single ducted fan type composite-wing aircraft, zero thrust self-energized ailerons and additional wings, wherein the zero thrust self-energized ailerons and the additional wings are assembled on the two sides of wings; the additional wings are mounted on the external sides of the zero thrust self-energized ailerons through wing hinges in a foldable manner. The rear single ducted fan type composite-wing aircraft with the zero thrust composite ailerons and the additional wings has the advantages that the taking-off and landing distance is short, the flying speed is high, the structural strength of the wings is high, the wings can store energy, the flying energy consumption is low, the hang time is long, large-compositelift wings can have effects of gliders in the case of emergency, the safety of the aircraft is greatly enhanced, and safeties of personnel and materials are guaranteed.

Description

technical field [0001] The invention relates to an aircraft, in particular to a rear single-duct fan-type compound wing aircraft with a non-propelling compound auxiliary wing and an additional wing, belonging 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 h...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/10B64C3/54B64C3/32B64C5/06B64C5/10B64D27/24
CPCB64C3/32B64C3/546B64C5/06B64C5/10B64C39/10B64D27/24B64U50/19B64U30/12B64U50/14
Inventor 任曲波
Owner JIANGSU CHANGTAN ROBOT CO LTD
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