Petrol-electric hybrid power fixed wing vertical take-off and landing unmanned plane system

An oil-electric hybrid, vertical take-off and landing technology, applied in the field of drones, can solve the problems of short voyage time, high cost, and highly professional operation, and achieve the effects of fast speed, long time, and long range

Active Publication Date: 2015-08-19
GUILIN HANGLONG KEXUN ELECTRONICS TECH
View PDF8 Cites 23 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

There are three shortcomings: high requirements for the runway, high environmental conditions for take-off, and high technical requirements for the operator
The disadvantage is that the ejection equipment is heavy, the assembly and use are more complicated and professional, and the cost is higher.
[0006] 4. Rocket-assisted take-off and parachute landing recovery method: relying on the booste

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
  • Petrol-electric hybrid power fixed wing vertical take-off and landing unmanned plane system
  • Petrol-electric hybrid power fixed wing vertical take-off and landing unmanned plane system

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0023] The principles and features of the present invention are described below in conjunction with the accompanying drawings, and the examples given are only used to explain the present invention, and are not intended to limit the scope of the present invention.

[0024] Such as figure 1 and 2 As shown, an oil-electric hybrid fixed-wing vertical take-off and landing UAV system includes a fuselage 1, a wing I2 and a wing II3, and a vertical propeller I4 and a wing motor I are arranged on the wing I2. The wing motor I drives the vertical propeller I4 to rotate, and the wing II3 is provided with a vertical propeller II5 and a wing motor II, and the wing motor II drives the vertical propeller II5 to rotate, and the vertical propeller I4 and The vertical propeller Ⅱ5 is mainly used for vertical takeoff or vertical landing of the UAV. The vertical take-off or vertical landing of the UAV does not require taxiing during take-off or landing, which reduces the environmental requireme...

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 petrol-electric hybrid power fixed wing vertical take-off and landing unmanned plane system, which comprises a fuselage, a wing I and a wing II. The wing I is provided with a vertical propeller I and a wing motor I. The wing II is provided with a vertical propeller II and a wing motor II. The front end of the fuselage is externally connected to a fixed wing horizontal propeller, the tail of the fuselage is provided with a longitudinal balance directional propeller and a longitudinal balance directional control motor, and the fuselage is internally provided with an autopilot for intelligently controlling the operation of the wing motor I, the wing motor II, a petrol power engine and the longitudinal balance directional control motor. The petrol-electric hybrid power fixed wing vertical take-off and landing unmanned plane system provided by the invention realizes the all functions of unmanned plane take-off replying on power battery vertical take-off, hovering to petrol power driven fixed wing fast flight, and return flight hovering to vertical landing petrol-electric hybrid power flight, has the capability of vertical take-off and landing and hovering, and also has the characteristics of fast speed, long voyage and long time.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to an oil-electric hybrid fixed-wing vertical take-off and landing unmanned aerial vehicle system. Background technique [0002] Due to the characteristics of fast maneuvering, low cost of use, and simple maintenance and use, UAVs have been widely used at home and abroad. But so far, due to the limitations of take-off and landing technology, the UAVs used in the world are still not fully used in actual use. In terms of fixed-wing vertical take-off and landing UAVs, there are few applications in the navies of only a few developed countries in the West, and oil-electric hybrid fixed-wing vertical take-off and landing UAVs are still blank. There are four conventional UAV take-off and landing technologies: [0003] 1. Traditional taxiing take-off and taxiing landing method: rely on the operator to control the aircraft on a spacious and straight runway to taxi to the take-off sp...

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
IPC IPC(8): B64C27/22B64D27/02
Inventor 秦子建
Owner GUILIN HANGLONG KEXUN ELECTRONICS TECH
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products

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

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap