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Zero backward thrust composite wing aircraft with ducted fan composite ailerons

A ducted fan and composite wing technology, applied in the field of thrustless composite wing aircraft and aircraft equipment, can solve the problems of low wing structure strength, slow horizontal flight speed, and unsatisfactory controllability, etc. The effect of wing area, fast flight speed, and convenient cluster flight

Inactive Publication Date: 2018-11-16
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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  • Zero backward thrust composite wing aircraft with ducted fan composite ailerons
  • Zero backward thrust composite wing aircraft with ducted fan composite ailerons
  • Zero backward thrust composite wing aircraft with ducted fan composite ailerons

Examples

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Embodiment Construction

[0029] The present invention will be further described below in conjunction with the accompanying drawings.

[0030] Such as Figure 1 to Figure 5 As shown, a non-rear-thrust compound wing aircraft with a ducted fan compound aileron is composed of a non-rear thrust type compound-wing aircraft and a ducted fan thrust self-powered compound aileron assembled on both sides of its wing; wherein , the non-rear-thrust type composite wing aircraft includes a body 101, a compound lift wing 102 fixedly installed on both sides of the body 101; wherein, the body 101 is set as a deck platform; the compound lift wing 102 Built-in self-enclosed ducted fan 104, the outer side of composite lift wing 102 is designed with wing hinges (1028); the front end of the ducted fan thrust self-powered compound auxiliary wing is provided with ducted fan propeller 1063, and the ducted fan thrust is self-supplied A self-enclosed ducted fan 104 is arranged inside the energy composite aileron, and one or bot...

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PUM

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Abstract

The invention provides a zero backward thrust composite wing aircraft with ducted fan composite ailerons. The zero backward thrust composite wing aircraft with the ducted fan composite ailerons comprises an aircraft body and composite lift wings which are fixedly mounted on the two sides of the aircraft body, wherein the aircraft body is arranged as a deck platform; self-sealing ducted fans are embedded in the composite lift wings; wing hinges are designed on the external sides of the composite lift wings; ducted fan propellers are arranged at the front ends of ducted fan thrust self-energizedcomposite ailerons; the self-sealing ducted fans are arranged in the ducted fan thrust self-energized composite ailerons; electricity, liquid and gas ports and the wing hinges are arranged on one sides or two sides of the ducted fan thrust self-energized composite ailerons; and the ducted fan thrust self-energized composite ailerons are movably connected with the composite lift wings through thewing hinges. The zero backward thrust composite wing aircraft with the ducted fan composite ailerons has the characteristics 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, the safety is high and so on; and the ailerons adopt compositelift forces to guarantee appropriate power.

Description

technical field [0001] The invention relates to an aircraft, in particular to a thrustless composite wing aircraft with a ducted fan composite auxiliary wing, and 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 high energy cons...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/20B64C27/26B64C37/02
CPCB64C27/20B64C27/26B64C37/02B64U50/14
Inventor 任曲波
Owner JIANGSU CHANGTAN ROBOT CO LTD
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