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Rear single ducted fan type composite wing aircraft with zero thrust composite ailerons

A ducted fan and composite wing technology is applied in the field of aircraft equipment and rear single ducted fan-type composite wing aircraft, which can solve the problems of low wing structure strength, slow horizontal flight speed, and unsatisfactory controllability, etc. Achieve the effect of expanding the wing area, fast flight speed, and reducing one-time investment

Inactive Publication Date: 2018-09-07
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
  • Rear single ducted fan type composite wing aircraft with zero thrust composite ailerons
  • Rear single ducted fan type composite wing aircraft with zero thrust composite ailerons

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Embodiment Construction

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

[0028] Such as figure 1 As shown, a rear single-duct fan-type compound-wing aircraft with no-thrust composite auxiliary wing is characterized in that the rear single-duct fan-type compound-wing aircraft and the non-thrust self-powered compound wing assembled on both sides of its wing Aileron composition;

[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 composite lift wing 102 has a built-in self-enclosed ducted fan 104, and a wing hinge 1028 is designed on the outside of the composite lift wing 102; the propeller 106 is a ducted fan propeller;

[0030] The non-thrust self-powered composite aileron is provided with a self-enclosed ducted fan 104, and one or both sides of the ...

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Abstract

The invention provides a rear single ducted fan type composite wing aircraft with zero thrust composite ailerons. The rear single ducted fan type composite wing aircraft with the zero thrust compositeailerons comprises a rear single ducted fan type composite wing aircraft and zero thrust self-energized composite ailerons which are assembled on the two sides of the rear single ducted fan type composite wing aircraft, wherein the rear single ducted fan type composite wing aircraft comprises an aircraft body, composite lift wings and a propeller, wherein the composite lift wings are fixedly mounted on the two sides of aircraft body; the aircraft body is arranged as a deck platform; self-sealed ducted fans are embedded in the composite lift wings; wing hinges are designed on the external sides of the composite lift wings; self-sealed ducted fans are arranged in the zero thrust self-energized composite ailerons; electricity, liquid and gas ports and wing hinges are arranged on one sides ortwo sides of the zero thrust self-energized composite ailerons; and the zero thrust self-energized composite ailerons are movably connected with the composite lift wings through the wing hinges. Therear single ducted fan type composite wing aircraft with the zero thrust composite ailerons has the advantages that the take-off and landing distance is short, the flying speed is high, the wing structural strength is high, the wing can store energy, the flying energy consumption is low, the aircraft can stay in the air for long time and so on; and the large-area composite lift wings can have effects of a glider in case of emergency so that 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-thrust compound auxiliary wing, 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...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/22B64C27/20B64C3/00B64C1/00B64C9/00
CPCB64C27/22B64C1/00B64C3/00B64C9/00B64C27/20
Inventor 任曲波
Owner JIANGSU CHANGTAN ROBOT CO LTD
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