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A foldable composite-wing manned aircraft with double-propeller-thrust composite auxiliary wings

A dual-propeller and composite wing technology, applied in the field of aircraft, can solve problems such as low safety factor, high take-off and landing requirements, and easy crash, and achieve the effects of high wing structure strength, reduced gravity acceleration, and improved safety factor

Inactive Publication Date: 2018-12-04
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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  • A foldable composite-wing manned aircraft with double-propeller-thrust composite auxiliary wings
  • A foldable composite-wing manned aircraft with double-propeller-thrust composite auxiliary wings
  • A foldable composite-wing manned aircraft with double-propeller-thrust composite auxiliary wings

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Embodiment Construction

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

[0034] like Figure 1 to Figure 5 As shown, a foldable compound wing manned aircraft with double propeller thrust compound ailerons consists of a non-rear thrust compound wing aircraft, self-powered composite ailerons foldable and installed on both sides of its wing, and a manned warehouse 112; wherein, the non-rear-thrust type composite wing aircraft includes a fuselage 101, a composite lift wing 102 foldable and installed on both sides of the fuselage 101; wherein, wherein the fuselage 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 interior of the aileron is provided with a self-enclosed ducted fan 104, and one or both sides of the propeller thrust self-powered composite aileron are provided with an electro-hydraulic inter...

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PUM

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Abstract

A foldable composite-wing manned aircraft with double-propeller-thrust composite auxiliary wings is provided. A rear-thrust-free type composite-wing aircraft includes a fuselage and composite liftingwings mounted, in a foldable manner, at two sides of the fuselage. The fuselage is a deck platform. Self-sealing ducted fans are disposed in the composite lifting wings. Hinges are arranged at outer sides of the composite lifting wings. Front ends of propeller-thrust self-powered composite auxiliary wings are provided with propellers. Self-sealing ducted fans are disposed in the propeller-thrust self-powered composite auxiliary wings. Electro-hydraulic gas connectors and wing hinges are disposed on one or two sides of the propeller-thrust self-powered composite auxiliary wings. The composite auxiliary wings are movably connected to the composite lifting wings through the wing hinges. A manned bin is mounted at the lower part of the fuselage. The aircraft has characteristics of short take-off and landing distances, a high flight speed, high wing structural strength, a characteristic that the wings can store energy, low flight energy consumption, long flying time, high safety, and the like. Composite lifting force is adopted by the auxiliary wings, thus ensuring the adaptive range of power.

Description

[0001] Technical field Disclosed is a foldable compound wing manned aircraft with double propeller thrust compound ailerons. technical field [0002] The invention relates to an aircraft, in particular to a foldable composite wing manned aircraft with double propeller thrust compound auxiliary wings, belonging to the technical field of aircraft equipment. Background technique [0003] 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 ver...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/26B64C27/20B64C1/30
Inventor 任曲波
Owner JIANGSU CHANGTAN ROBOT CO LTD
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