Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Rear single propeller type compound wing cargo aircraft with thrust-free compound ailerons

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

Inactive Publication Date: 2018-11-06
JIANGSU CHANGTAN ROBOT CO LTD
View PDF3 Cites 0 Cited by
  • 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

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Rear single propeller type compound wing cargo aircraft with thrust-free compound ailerons
  • Rear single propeller type compound wing cargo aircraft with thrust-free compound ailerons
  • Rear single propeller type compound wing cargo aircraft with thrust-free compound ailerons

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0032] The present invention will be further described below in conjunction with the accompanying drawings.

[0033] Such as Figure 1 to Figure 5 Shown, a kind of rear single-screw type composite wing cargo aircraft with non-propelling compound aileron, comprises rear single-screw type composite wing aircraft, the non-thrust self-powered composite aileron 1031 that is movably installed in the compound lift aircraft both sides is formed; Engine Installation position 111,; Cargo storehouse is installed in the below of body.

[0034] 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 hinge 1025 is designed on the outside of the composite lift wing 102;

[0035] The non-thrust self-powered composite aileron 1031 is provided with ...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention relates to a compound lift aircraft with an expansion platform. The compound lift aircraft comprises a rear single propeller type compound wing aircraft, thrust-free self-powered compound ailerons assembled on two sides of the rear single propeller type compound wing aircraft and a cargo bin, wherein the rear single propeller type compound wing aircraft comprises a body, compound lift wings fixed on two sides of the body and a propeller; the body is arranged to be a deck platform; self-closing ducted fans I are arranged in the compound lift wings, and hinges are designed on outersides of the compound lift wings; self-closing ducted fans II are arranged in the thrust-free self-powered compound ailerons, electro-hydraulic gas ports and the hinges are arranged on one side or two sides of each thrust-free self-powered compound aileron, and the thrust-free self-powered compound ailerons are movably connected with the compound lift wings through the hinges; the cargo bin is mounted below the body. The aircraft has the characteristics of short take-off and landing distance, high flight speed, high wing structural strength, energy storable wings, low flight energy consumption, long hang time, high safety and the like.

Description

technical field [0001] The invention relates to an aircraft, in particular to a rear single propeller composite wing cargo aircraft with a non-thrusting composite auxiliary 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 disadvantages o...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/22B64C27/20B64C5/00B64C9/00B64C3/00
Inventor 任曲波
Owner JIANGSU CHANGTAN ROBOT CO LTD
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com