Rear single ducted fan type composite wing manned aircraft provided with composite auxiliary wings and additional wings

A ducted fan and manned aircraft technology, applied in the field of aircraft, can solve the problems of low wing structure strength, slow horizontal flight speed, unsatisfactory controllability, etc. The effect of convenient group flight

Inactive Publication Date: 2018-11-06
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 manned aircraft provided with composite auxiliary wings and additional wings
  • Rear single ducted fan type composite wing manned aircraft provided with composite auxiliary wings and additional wings
  • Rear single ducted fan type composite wing manned aircraft provided with composite auxiliary wings and additional wings

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Embodiment Construction

[0033] The present invention will be further described below in conjunction with the accompanying drawings.

[0034] Such as figure 1 Shown, a rear single ducted fan type compound wing manned aircraft with compound auxiliary wing and additional wing is characterized in that, by rear single ducted fan type compound wing aircraft, propeller thrust assembled on both sides of its wing Self-powered composite ailerons, additional wings 114 and manned cabin 112; wherein, the rear single-duct fan type composite wing aircraft includes a body 101, a composite lift wing 102 fixedly installed on both sides of the body 101, and a propeller 106 wherein, wherein, the body 101 is set to a deck platform; the composite lift wing 102 has a built-in self-enclosed duct fan 104, and the outside of the composite lift wing 102 is designed with a wing hinge 1028; the propeller 106 is a duct fan Propeller; the front end of the propeller thrust self-powered composite aileron is provided with a propelle...

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Abstract

The invention discloses a rear single ducted fan type composite wing manned aircraft provided with composite auxiliary wings and additional wings. The rear single ducted fan type composite wing mannedaircraft provided with the composite auxiliary wings and the additional wings is characterized by comprising a rear single ducted fan type composite wing aircraft as well as propeller thrust self-powering composite auxiliary wings, additional wings and manned cabins which are assembled on two sides of wings of the aircraft. The rear single ducted fan type composite wing manned aircraft has the characteristics that the take-off and landing distance is short, the flight speed is high, the wing structure strength is high, the wings can store energy, the flight energy consumption is low, the hangtime is long, the safety is high and the like, the auxiliary wings adopt composite lift force, and the application range of power is ensured.

Description

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

Claims

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Application Information

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IPC IPC(8): B64C27/22B64C9/12B64C11/00
CPCB64C27/22B64C9/12B64C11/00
Inventor任曲波
OwnerJIANGSU CHANGTAN ROBOT CO LTD