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

A propeller and composite wing technology, applied in the field of aircraft, can solve the problems of low structural strength of the wing, unsatisfactory controllability, and slow horizontal flight speed, etc., to achieve the goal of expanding the wing area, increasing the lift force, and fast flying speed Effect

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 propeller type composite wing manned aircraft provided with composite auxiliary wings and additional wings
  • Rear single propeller type composite wing manned aircraft provided with composite auxiliary wings and additional wings
  • Rear single propeller 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 to Figure 5 As shown, the rear single propeller compound wing manned aircraft with compound ailerons and additional wings comprises a rear single propeller compound wing aircraft and non-thrust self-powered composite ailerons 1031 that are movably installed on both sides of the compound lift aircraft; 111. Engine mounting position.

[0035] Wherein, the rear single propeller compound wing aircraft includes a body 101, a compound 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 compound lift The 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;

[0036] The non-thrust self-powered composite aileron 1031 is provided with a self-enclosed ducted fan 104, and one or both sides o...

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Abstract

The invention discloses a rear single propeller type composite wing manned aircraft provided with composite auxiliary wings and additional wings. The aircraft comprises a rear single propeller type composite wing aircraft as well as no-thrust self-powering composite auxiliary wings, additional wings and manned cabins which are assembled on two sides of wings of the aircraft, wherein the additionalwings are mounted on outer sides of the no-thrust self-powering composite auxiliary wings through wing hinges in a foldable manner, and the manned cabins are mounted below a body. The rear single propeller 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 hang time is long and the like, large-area composite lift wings can play a role of a glider under the emergency condition, the flight safety of the aircraft is greatly improved, and safety of people and materials is guaranteed.

Description

technical field [0001] The invention relates to an aircraft, in particular to a rear single propeller 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 disad...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/22B64C11/00B64C9/12
CPCB64C27/22B64C9/12B64C11/00
Inventor 任曲波
Owner JIANGSU CHANGTAN ROBOT CO LTD
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