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

Multi-rotor unmanned aerial vehicle emergency parachuting device with adaptive ejection angle adjustment function and method

A multi-rotor UAV and self-adaptive adjustment technology, applied in the field of agricultural UAV research, can solve problems such as crashes, bombings, and reducing the success rate of UAV self-rescue.

Active Publication Date: 2017-06-23
SOUTH CHINA AGRI UNIV
View PDF6 Cites 12 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, at present, due to terrain, landform, obstacles, operation and other problems, drones are prone to various sudden risks, which may even lead to crashes and bombings, causing large economic losses to users and farmers.
[0003] At present, the UAV parachute device mostly adopts the method of directly ejecting the parachute outward to implement self-rescue. When the UAV attitude does not change significantly, the parachute device can work normally, but when the UAV has a large deflection and tilt Under such circumstances, due to the oblique shift of the ejection angle, the parachute device is not easy to open in time and effectively, thereby reducing the success rate of self-rescue of the UAV.

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
  • Multi-rotor unmanned aerial vehicle emergency parachuting device with adaptive ejection angle adjustment function and method
  • Multi-rotor unmanned aerial vehicle emergency parachuting device with adaptive ejection angle adjustment function and method
  • Multi-rotor unmanned aerial vehicle emergency parachuting device with adaptive ejection angle adjustment function and method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0042] Such as figure 1 As shown, the present embodiment provides a multi-rotor unmanned aerial vehicle emergency parachute device, which device includes an umbrella compartment 1, an umbrella compartment cover 2, a parachute 3, a parachute throwing spring 4, a lock bolt 5, an unlocking steering gear 6, a micro Controller 7, inertial motion measurement unit 8 and spring support rotation device.

[0043] There are two locking bolts 5 and two unlocking steering gears 6 respectively, and the two unlocking steering gears 6 are respectively fixed on the side walls of the umbrella compartment 1. The two locking bolts 5 are respectively located above the two unlocking steering gears 6, and respectively The two unlocking steering gears 6 are connected, and the umbrella cover 2 is fixed on the umbrella housing 1 under the joint action of the lock bolt 5 and the unlocking steering gear 6, and the umbrella housing 1 is fixed on the multi-rotor UAV.

[0044] Described parachute 3, parachut...

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 multi-rotor unmanned aerial vehicle emergency parachuting device with an adaptive ejection angle adjustment function and a method. The device comprises a parachute cabin, a parachute cabin cover, a parachute, a parachute throwing spring, a lock bolt, an unlocking steering engine, a microcontroller, an inertial motion measuring unit and a spring support rotating device. The parachute cabin cover is fixed to the parachute cabin under the combined action of the unlocking steering engine and the lock bolt, and the parachute cabin is fixed to a multi-rotor unmanned aerial vehicle; the parachute, the parachute throwing spring, the microcontroller, the inertial motion measuring unit and the spring support rotating device are arranged in a structure formed by the parachute cabin and the parachute cabin cover; the microcontroller is connected with the unlocking steering engine, the inertial motion measuring unit and the spring support rotating device, one end of the parachute throwing spring is fixed to the spring support rotating device, and the other end of the parachute throwing spring is fixed to the parachute. By adaptively adjusting the spring ejection angle, it can be guaranteed that the parachute is ejected vertically upwards even when the posture of the multi-rotor unmanned aerial vehicle has large deflection or inclination.

Description

technical field [0001] The invention relates to a UAV parachute device and method, in particular to a multi-rotor UAV emergency parachute device and method for adaptively adjusting the ejection angle, and belongs to the field of agricultural UAV research. Background technique [0002] Multi-rotor UAV is a special unmanned helicopter with three or more rotor shafts. It is a hot spot in the field of aviation research. There are a lot of demands in practical applications, such as: reconnaissance and rescue missions, scientific data collection , geological and forestry exploration, agricultural pest control, video surveillance, film and television production, etc. Using unmanned aerial vehicles to complete the above tasks can greatly reduce costs and improve personnel safety. Therefore, unmanned aerial vehicles have developed rapidly in military, civilian, and especially agricultural fields in recent years. However, at present, various unexpected risks are prone to occur due t...

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): B64D45/04B64D17/54
CPCB64D17/54B64D45/04B64U10/10B64U70/83
Inventor 徐兴王臻杰李君杨洲蔡坤陈壮辉陈华明张倩倩
Owner SOUTH CHINA AGRI 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