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

High reliability UAV landing gear retractable system

A landing gear and reliability technology, applied in the field of unmanned aerial vehicle landing gear retraction system, can solve the problems of limited driving force and inability to maintain, and achieve the effects of reasonable force form, flexible retraction and release, and reasonable force structure

Active Publication Date: 2019-11-29
BEIHANG UNIV
View PDF9 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This type of landing gear retraction system, the electric type is usually only used for small aircraft due to the limited driving force; the high-pressure gas type uses the cylinder to generate the driving force, but it needs to keep the high-pressure gas connected to maintain the landing gear in the retracted position and the lowered position. State, when there is no air pressure, it cannot maintain the corresponding state

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
  • High reliability UAV landing gear retractable system
  • High reliability UAV landing gear retractable system
  • High reliability UAV landing gear retractable system

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0030] The present invention will be described in detail below in conjunction with the accompanying drawings and embodiments.

[0031] The invention provides a high-reliability unmanned aerial vehicle landing gear retractable system, which can be used on the unmanned aerial vehicle to make the landing gear firmly and reliably locked in the lowered position during ground taxiing, take-off, and landing; Reliably locked in the retracted position; after takeoff and before landing, the landing gear can be retracted or lowered smoothly; in the no-air pressure state, the landing gear is also lowered and locked in the lowered position under the action of gravity.

[0032] Such as figure 1 , figure 2 and image 3 As shown, the high-reliability unmanned aerial vehicle landing gear retractable system provided by the present invention mainly includes a set of landing gear retractable mechanism and a set of landing gear retractable locking mechanism.

[0033] The landing gear retractab...

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 high-reliability unmanned aerial vehicle landing gear extension and retraction system, and belongs to the technical field of unmanned aerial vehicle design. The extension andretraction system includes a landing gear extension and retraction mechanism and a landing gear extension and retraction locking mechanism. The landing gear extension and retraction mechanism comprises a landing gear side plate and frame structure, a landing gear pillar and plane wheel assembly, a landing gear pillar extension and retraction rocker arm, a landing gear pillar extension and retraction actuating cylinder, a landing gear strut universal joint, an upper landing gear strut and a lower landing gear strut; and the landing gear extension and retraction locking mechanism comprises a landing gear down lock cylinder, a landing gear down lock triangle, a landing gear down lock bolt, a landing gear uplock shell, a landing gear uplock cylinder, a landing gear uplock bolt and a landing gear uplock hook. The landing gear extension and retraction system has the advantages of compact structure, reasonable force form, no driving force in a non-actuated state, and self-locking in a pressure-free extension state.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicle design, and in particular relates to an unmanned aerial vehicle landing gear retractable system. Background technique [0002] Landing gear is an accessory device used by an aircraft to support the aircraft during takeoff, landing, or taxiing on the ground, and for ground movement. With the increase of aircraft speed, in order to reduce the air resistance when the aircraft is flying, the landing gear is designed to be retractable. When the aircraft is flying in the air, the landing gear is retracted inside the body, which can greatly reduce the wind resistance of the aircraft and improve the aerodynamic performance and flight performance of the aircraft. Compared with the fixed landing gear, although the retractable landing gear increases the weight of the aircraft and complicates the structural design of the aircraft, it improves the flight efficiency and is a common configuratio...

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 Patents(China)
IPC IPC(8): B64C25/22B64C25/26
CPCB64C25/22B64C25/26
Inventor 付竟成黄俊宋磊郑浩
Owner BEIHANG UNIV
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