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

Flapping-wing-like device capable of simultaneously generating thrust and lift force

A lift and thrust technology, applied in the field of aircraft, can solve the problems of low safety, poor lift stability, poor flexibility, etc., and achieve the effect of large lift and thrust, small size and light overall weight

Inactive Publication Date: 2021-03-16
GUANGDONG GUOSHIJIAN TECH DEV CO LTD
View PDF5 Cites 1 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The flapping rotorcraft is an aircraft manufactured by imitating the flight of birds. It uses flapping wing surfaces like the wings of birds to generate lift and pulling force. At present, although many experts and scholars at home and abroad have carried out A large amount of research and experiment, but, because existing many flapping rotorcrafts can cause the lift offset that produces during rotor up and down operation process, make the development of flapping rotorcrafts still exist many technical difficulties, thus also just cause existing Flapping rotorcrafts have poor lift stability, low safety, and poor flexibility, and cannot freely change the flight direction of the aircraft

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
  • Flapping-wing-like device capable of simultaneously generating thrust and lift force
  • Flapping-wing-like device capable of simultaneously generating thrust and lift force
  • Flapping-wing-like device capable of simultaneously generating thrust and lift force

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0046] Embodiments of the present invention are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals designate the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention.

[0047] In describing the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", The orientation or positional relationship indicated by "bottom", "inner", "outer", etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying the referred device or positional relationship. Elements must hav...

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 discloses a flapping-wing-like device capable of simultaneously generating a thrust and a lift force. The device comprises a fuselage, a support assembly, two rotor wing assemblies, a driving assembly, a brake assembly, a pulling assembly, a control assembly and a take-off and landing assembly. The two rotor wing assemblies are symmetrically arranged on two sides of the fuselage; each rotary wing assembly comprises a revolution main shaft, a rotary arm, an autorotation main shaft and a rotary wing part, and through linkage cooperation of the revolution main shaft, the rotary arms, the autorotation main shaft, the rotary wing part and the driving assembly, the autorotation main shaft can also autorotate while the revolution main shaft in each rotary wing assembly drives the rotary arm and the autorotation main shaft to revolve; and continuously rotating wing pieces can generate an upward lift force, the pull assembly can provide a forward pull force or a push force for theflapping-wing-like device, the forward and upward push force and lift force are provided for take-off and landing of the flapping-wing-like device, and the technical effect of short-distance take-offand landing of the flapping-wing-like device can be achieved.

Description

technical field [0001] The invention relates to the technical field of aircraft, and more specifically relates to a flapping-wing device that simultaneously generates thrust and lift. Background technique [0002] The flapping rotorcraft is an aircraft manufactured by imitating the flight of birds. It uses flapping wing surfaces like the wings of birds to generate lift and pulling force. At present, although many experts and scholars at home and abroad have carried out A large amount of research and experiment, but, because existing many flapping rotorcrafts can cause the lift offset that produces during rotor up and down operation process, make the development of flapping rotorcrafts still exist many technical difficulties, thus also just cause existing Flapping rotorcrafts have poor lift stability, low safety, and poor flexibility, and cannot freely change the flight direction of the aircraft. [0003] Therefore, it is urgently needed by those skilled in the art to provid...

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): B64C27/22B64C33/02B64D27/24
CPCB64C27/22B64C33/02B64D27/24Y02T50/60
Inventor 王志成
Owner GUANGDONG GUOSHIJIAN TECH DEV 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