Unlock instant, AI-driven research and patent intelligence for your innovation.

A rapid test device and method for unmanned aerial vehicle propeller balance

A test method and technology of test device, which are applied in static/dynamic balance test, measurement device, machine/structural component test, etc. The effect of shortened time

Active Publication Date: 2019-03-22
武汉飞流智能技术有限公司
View PDF5 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Aiming at the above defects or improvement needs of the prior art, the present invention provides a fast test device and method for unmanned aerial vehicle propeller balance; its purpose is to realize the automatic test of unmanned aerial vehicle propeller balance based on the grating sensing technology, and solve the existing problems. The problem of low accuracy and low efficiency in manual mode

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
  • A rapid test device and method for unmanned aerial vehicle propeller balance
  • A rapid test device and method for unmanned aerial vehicle propeller balance
  • A rapid test device and method for unmanned aerial vehicle propeller balance

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0044] In order to make the object, technical solution and advantages of the present invention more clear, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention. In addition, the technical features involved in the various embodiments of the present invention described below can be combined with each other as long as they do not constitute a conflict with each other.

[0045] The unmanned aerial vehicle propeller balance quick test device provided by the embodiment, its structure is as follows figure 1 As shown; including the bottom plate, and the magnetic levitation bracket placed on the bottom plate, the center of gravity status indicator board, the propeller balance controller, and the test components;

[0046] In this embodiment, the magnetic levitatio...

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 an unmanned aerial vehicle propeller balance rapid testing device and an unmanned aerial vehicle propeller balance rapid testing method. The unmanned aerial vehicle propeller balance rapid testing device comprises a bottom plate; a magnetic suspension support and a propeller balance controller, which are disposed on the bottom plate; and a testing component. The magnetic suspension support is detachably connected with the testing component. The testing component is used to carry a to-be-tested unmanned aerial vehicle propeller, and the magnetic suspension support is used to carry the testing component. The propeller balance controller is used to acquire the rotation direction and the speed of the to-be-tested unmanned aerial vehicle propeller, and is used to determine the gravity center offset direction thereof according to the acquired rotation direction and the acquired speed. The testing component comprises a magnetic suspension shaft, a propeller fixing button, a grating disc, and a grating sensor. Based on the unmanned aerial vehicle propeller balance rapid testing method of the above mentioned device and the grating sensing technology, the grating disc is used to acquire the rotation direction and the acceleration direction of the to-be-tested propeller, which are converted into pulse signals by the grating sensor, and then the gravity center offset direction of the propeller is acquired quickly, automatically, and accurately by the phase differences and the pulse widths of the pulse signals.

Description

technical field [0001] The invention belongs to the technical field of multi-rotor UAV testing, and more specifically, relates to a fast testing device and method for UAV propeller balance. Background technique [0002] At present, the method of adjusting the balance of the center of gravity of the multi-rotor UAV propeller is mostly manual adjustment with the help of the magnetic suspension balance shaft. First, fix the propeller to be adjusted on the magnetic suspension balance shaft, and then place the magnetic suspension balance shaft on the special bracket. If the center of gravity of the propeller is not on the same line as the axis of the magnetic levitation balance shaft, the propeller to be adjusted will deflect slowly under the action of gravity. The center of gravity of the propeller is adjusted by grinding the material of the propeller in the direction of the propeller; after grinding, measure the offset direction of the center of gravity in the same way again, a...

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): G01M1/12
CPCG01M1/125
Inventor 刘奇沈顺明张俊锋帅率
Owner 武汉飞流智能技术有限公司