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Control device for hail impact test and operation method thereof

A technology of control device and impact test, applied in measurement devices, instruments, scientific instruments, etc., can solve the problems of multiple launch launch accuracy and launch time, and achieve the effect of reducing errors, improving reliability, and reducing launch time.

Active Publication Date: 2010-09-15
SOUTHEAST UNIV
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  • Abstract
  • Description
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  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to provide a control device for hail test and its working method, which can solve the problems of multiple launches, launch accuracy and launch time in the prior art, realize the multiple launch requirements of hail test in a short time, and Ensure the consistency of multiple test launches, the accuracy and speed of data

Method used

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  • Control device for hail impact test and operation method thereof
  • Control device for hail impact test and operation method thereof
  • Control device for hail impact test and operation method thereof

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Embodiment Construction

[0016] Below in conjunction with accompanying drawing, technical characterictic of the present invention is described further:

[0017] Such as figure 1 As shown, the control device for the hail impact test of the present invention includes a host computer and a lower computer, and the host computer is controlled by an LED speed display, a first microprocessor, a first controller, a photoelectric isolator, a first communication module, valve, switch and booster controller; the lower computer is made up of a first photoelectric sensor, a second photoelectric sensor, a second microprocessor, a second controller and a second communication module; the output terminal of the first controller is connected with the The input end of the first microprocessor is connected, the output end of the first microprocessor is respectively connected with the input end of LED speed indicator, photoelectric isolator, the first communication module is electrically connected with the first microproc...

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Abstract

The invention discloses a control device for hail impact test and an operation method thereof. The control device comprises an upper computer and a lower computer; wherein the upper computer comprises an LED velocity indicator, a first microprocessor, a first controller, an optoelectronic isolator, a first communication module, a control valve, a switch and a boost controller; the lower computer comprises a first photoelectric sensor, a second photoelectric sensor, a second microprocessor, a second controller and a second communication module; the operation method comprises the following steps: by utilizing the boost signal and the sending signal of the first controller, respectively starting an air booster pump and sending hail balls through the first microprocessor and the optoelectronic isolator, the hail balls respectively passing through the first photoelectric sensor and the second photoelectric sensor to obtaining an interrupt signal, calculating the hail ball velocity signal through the second microprocessor, and sending the hail ball velocity signal to the LED velocity indicator via the communication module and the first microprocessor. The invention realizes the requirement on multiple sending in hail tests in a short period of time, and ensures the sending conformity and data accuracy.

Description

technical field [0001] The invention relates to a hail emission control device and a working method for the hail impact reliability test, and is also suitable for other small particle impact tests. Background technique [0002] At present, there are no relevant reports on the hail impact test in China. There are relevant test standards in the United States abroad, but there are no detailed elaborations and requirements for the launch process and launch system of hail. For the domestic bird strike test carried out on the same principle as the hail impact test, the test process and control are all manually controlled, and the membrane-rupturing method is generally used. The disadvantage of the membrane-breaking manual launch control is that the launch time cannot be accurately controlled, and each launch time has a large change. At the same time, the launch time cannot reach the microsecond level standard, and the preparation time for a single launch is long. (1 minute) Conti...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01N3/303
Inventor 薛澄岐易红尤志芳
Owner SOUTHEAST UNIV
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