Rear single-paddle type compound wing airplane with twin-duct thrust compound auxiliary wings and additional wings

A composite wing and auxiliary wing technology, applied in the field of aircraft, can solve the problems of low wing structure strength, slow horizontal flight speed, and unsatisfactory controllability, etc., and achieves expansion of wing area, fast flight speed, and improved lift. Effect

Inactive Publication Date: 2018-09-04
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-

Method used

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  • Rear single-paddle type compound wing airplane with twin-duct thrust compound auxiliary wings and additional wings
  • Rear single-paddle type compound wing airplane with twin-duct thrust compound auxiliary wings and additional wings
  • Rear single-paddle type compound wing airplane with twin-duct thrust compound auxiliary wings and additional wings

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Example Embodiment

[0035] The present invention will be further described below in conjunction with the drawings.

[0036] Such as Figure 1 to Figure 5 As shown, a rear single-propeller composite wing aircraft with dual ducted thrust composite ailerons and additional wings includes a rear single-propeller composite wing aircraft, propeller thrust self-powered composite ailerons and additional wings assembled on both sides of its wings 114; wherein, the rear single-propeller composite wing aircraft includes a body 101, a composite lift wing 102 fixedly installed on both sides of the body 101, a propeller 106; wherein, the body 101 is set as a deck platform; The composite lift wing 102 has a built-in self-enclosed ducted fan 104, and the outer side of the composite lift wing 102 is designed with an organic wing hinge 1028; the front end of the self-powered propeller thrust composite aileron is provided with a ducted fan thruster 1063, and the propeller thrust is self-powered The interior of the com...

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PUM

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Abstract

The invention discloses a rear single-paddle type compound wing airplane with twin-duct thrust compound auxiliary wings and additional wings. The rear single-paddle type compound wing airplane comprises an airplane body, compound lift force wings fixedly mounted on two sides of the airplane body and ducted fan propellers, wherein self-enclosed ducted fans are arranged in the compound lift force wings; wing hinges are designed on the outer sides of the compound lift force wings; the ducted fan propellers are arranged at the front ends of propeller thrust self-powered compound auxiliary wings; self-enclosed ducted fans are arranged in the propeller thrust self-powered compound auxiliary wings; electricity liquid gas connection ports and the wing hinges are arranged on both sides of the propeller thrust self-powered compound auxiliary wings which are movably connected with the compound lift force wings through the wing hinges on one sides. The rear single-paddle type compound wing airplane has the characteristics of short take-off and landing distance, high flying speed, high wing structure strength, capability of energy storage in the wings, low flying energy consumption, long hang time, high safety and the like; the auxiliary wings adopt compound lift force to guarantee an application range of power.

Description

technical field [0001] The invention relates to an aircraft, in particular to a rear single-blade compound-wing aircraft with a double-duct thrust compound auxiliary wing and an additional 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 t...

Claims

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Application Information

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IPC IPC(8): B64C27/22B64C3/54B64C5/06B64C5/00B64D27/24
CPCB64C3/54B64C5/00B64C5/06B64C27/22B64D27/24B64U30/12B64U30/20Y02T50/60
Inventor 任曲波
Owner JIANGSU CHANGTAN ROBOT CO LTD
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