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Aiming positioning device and method for strong impact test system

A technology of impact test and positioning device, applied in impact test, measuring device, testing of machine/structural components, etc., to achieve the effect of ensuring coincidence, easy installation, and improving efficiency

Pending Publication Date: 2021-07-23
CHINA AIRPLANT STRENGTH RES INST
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of this application is to provide an aiming and positioning device and method for a strong impact test system to solve at least one problem in the prior art

Method used

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  • Aiming positioning device and method for strong impact test system
  • Aiming positioning device and method for strong impact test system

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Embodiment Construction

[0027] In order to make the purpose, technical solution and advantages of the application more clear, the technical solution in the embodiment of the application will be described in more detail below in conjunction with the drawings in the embodiment of the application. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the application. The embodiments described below by referring to the figures are exemplary, and are intended to explain the present application, and should not be construed as limiting the present application. Based on the embodiments in this application, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of this application. Embodiments of the present application will be described in detail below in conjunction with th...

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PUM

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Abstract

The invention belongs to the field of aviation test application, and particularly relates to an aiming positioning device and method for a strong impact test system. The device comprises a positioning flange 1, a positioning ring 2, a core shaft 3 and an infrared generator 7, wherein a gun barrel is provided with a containing cavity, the positioning flange 1 is coaxially mounted in the containing cavity of the gun barrel, the positioning ring 2 is fixedly mounted on the positioning flange 1 through a fastening screw 4, the core shaft 3 is nested in the positioning ring 2 and is fixedly connected with the positioning ring 2 through a positioning pin 5, and the infrared generator 7 is coaxially mounted at the end part of the core shaft 3. According to the invention, the device is installed in a gun barrel, the coaxiality with the axis of the gun barrel is guaranteed through flanges at the two ends, non-contact aiming and positioning are conducted through light beams of an infrared generator installed in the center, installation and positioning of an impacted object are achieved, the purpose of guaranteeing coincidence of a test piece and a tested point is achieved, installation is convenient, the installation time is saved, and efficiency is improved.

Description

technical field [0001] The application belongs to the application field of aviation test, and in particular relates to an aiming and positioning device and method for a strong impact test system. Background technique [0002] The strong impact test system is a test system used for strong impact and extreme target tests on the test piece, which can verify the safety, reliability and effectiveness of the test piece. In the impact test, the corresponding positioning structure is generally used to position the test piece to avoid the deviation of the test piece during the impact test. However, in the ultimate target test, there is still a lack of an aiming and positioning method that can achieve the coincidence of the axis of the test piece with the point to be tested. The test piece cannot be accurately aimed at the object being hit, so that the accurate test of the performance of the test piece cannot be realized. [0003] Therefore, it is desirable to have a technical soluti...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M7/08
CPCG01M7/08
Inventor 王文宇李碧波王靖郭军姚小明王兰张积广赵文华
Owner CHINA AIRPLANT STRENGTH RES INST