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Flexible aerofoil vibration detecting and control device based on high-speed camera and method thereof

A technology of vibration detection and high-speed camera, which is applied in the direction of mechanical vibration control, measuring device, vibration test, etc., can solve the problem that vibration information cannot be fed back to the driver, etc., and achieve the effect of suppressing multi-mode vibration, excellent performance, and improving reliability

Inactive Publication Date: 2017-09-15
SOUTH CHINA UNIV OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The purpose of the present invention is to provide a flexible wing vibration detection and control device based on a high-speed camera for the shortcomings and deficiencies of the existing flexible wing vibration detection and control technology. The device uses a high-speed camera as a vibration detection and analysis At the same time, the acceleration sensor is used as an auxiliary method, which overcomes the problem that it takes a certain time to analyze and process the obtained photos by the high-speed camera to obtain the vibration information of the wing, and the problem that the vibration information cannot be fed back to the driver immediately can be obtained simply and quickly Comprehensive vibration information in the measured area, and the vibration information is fed back to the computer in real time. After processing by the control algorithm set in the computer, the control value is obtained and output to the electromagnetic actuator to generate control force, so that the vibration of the flexible wing get suppressed

Method used

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  • Flexible aerofoil vibration detecting and control device based on high-speed camera and method thereof
  • Flexible aerofoil vibration detecting and control device based on high-speed camera and method thereof
  • Flexible aerofoil vibration detecting and control device based on high-speed camera and method thereof

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Embodiment 1

[0033] Such as figure 1 , image 3 and Figure 4 As shown, the present embodiment provides a flexible wing vibration detection and control device based on a high-speed camera, including a flexible wing body part, a vibration detection part, a vibration control part, a signal processing module and a computer (15), the flexible wing The wing body part includes the wing (1), base (5) and exciter (6), and the wing (1) is composed of 11 ribs (4) and 6 beams (3) to form a support (wing The internal structure diagram is as follows figure 2 shown), and is composed of a layer of skin (2) on the outside, the wing (1) is 1500mm long, the length of the wing root is about 500mm, and the length of the wing tail is about 400mm, which is installed through the base (5) On the test stand (12), the surface of the wing (1) is parallel to the test stand (12), and the left and right wing (1) upper surfaces are respectively provided with marker points for vibration detection (mark points on the ...

Embodiment 2

[0039] This embodiment provides a method for detecting and controlling the vibration of a flexible wing based on a high-speed camera, the method comprising the following steps:

[0040] Step 1. The signal generator (18) sends out a vibration signal, which is amplified by the power amplifier (19) and then sent to the two exciters (6). Wing (1) produces multi-modal vibrations. During the vibration process of left and right wings (1), two pairs of binocular vision systems composed of high-speed camera Ⅰ (8) and high-speed camera Ⅱ (9) respectively monitor the left and right wings ( 1) Synchronous shooting is carried out, and the photos are transmitted to the computer (15), and after image processing, the vibration information of the left and right wings (1) is obtained, and at the same time, the vibration information measured by the acceleration sensor (10) is amplified by the charge amplifier (13) After being converted by the A / D converter (16), it is input into the computer (15...

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Abstract

The invention discloses a flexible aerofoil vibration detecting and control device based on a high-speed camera. The device comprises a flexible aerofoil body part, a vibration detecting part, a vibration control part, a signal processing module and a computer. The flexible aerofoil body part comprises an aerofoil, a base and a vibration exciter. The vibration detecting part comprises two pairs of binocular vision systems which are composed of high-speed cameras and a plurality of acceleration sensors. The vibration control part comprises a plurality of electromagnetic actuators. The mounting positions of the plurality of electromagnetic actuators are same with that of the plurality of acceleration sensors. The vibration detecting part measures vibration information of the flexible aerofoil body part. Through processing by the signal processing module, the processed vibration information is transmitted to the computer. The computer performs corresponding processing and then makes the vibration control part perform action, thereby finishing measurement and control on vibration of the flexible aerofoil body part. The device has advantages of high sensitivity and high response speed. Furthermore the device can realize accurate measurement and control for vibration of the flexible aerofoil.

Description

technical field [0001] The invention relates to the field of vibration detection and control of flexible structures, in particular to a device and method for vibration detection and control of a flexible wing based on a high-speed camera. Background technique [0002] With the rapid development of the aviation industry, airplanes play an increasingly important role in cargo transportation and passenger transportation, including the use of aerospace vehicles and the development of functional drones. One of the greatest inventions of the century has increasingly become an indispensable tool in today's world. In the design and practical application of the aircraft, the vibration of the wing is one of the very important and key considerations. If there is no effective means to suppress the vibration of the aircraft wing, the vibration will cause the mechanical fatigue of the wing during the flight of the aircraft. , under the action of stress and strain, if one or several place...

Claims

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Application Information

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IPC IPC(8): G05D19/02G01M7/02G01H9/00
CPCG05D19/02G01H9/00G01M7/025
Inventor 邱志成梁卓文
Owner SOUTH CHINA UNIV OF TECH
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