CN201569606U - Damage tolerance test crack detection device - Google Patents

Damage tolerance test crack detection device Download PDF

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Publication number
CN201569606U
CN201569606U CN2010200000634U CN201020000063U CN201569606U CN 201569606 U CN201569606 U CN 201569606U CN 2010200000634 U CN2010200000634 U CN 2010200000634U CN 201020000063 U CN201020000063 U CN 201020000063U CN 201569606 U CN201569606 U CN 201569606U
Authority
CN
China
Prior art keywords
digital camera
test
detection device
control computer
crack
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN2010200000634U
Other languages
Chinese (zh)
Inventor
张立红
薛伟松
张俊明
肖培军
赵春兰
李进峰
米德凤
李瑞峰
房存京
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Harbin Aircraft Industry Group Co Ltd
Original Assignee
Harbin Aircraft Industry Group Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Harbin Aircraft Industry Group Co Ltd filed Critical Harbin Aircraft Industry Group Co Ltd
Priority to CN2010200000634U priority Critical patent/CN201569606U/en
Application granted granted Critical
Publication of CN201569606U publication Critical patent/CN201569606U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model relates to a damage tolerance test crack detection device used for fatigue tests. The detection device includes a control computer, and a digital camera arranged on a test bed and accommodating a test piece in a framing zone of the digital camera, wherein the digital camera is connected with a control computer. The utility model has the advantages and the benefits that the detection device can send trigger signals according to the test loading time or send trigger signals according to the test loading value, record the crack propagation situation of the test piece, store crack photos easily, and facilitate crack propagation situation analysis, thereby reducing the work load of a tester and avoiding defects that the ocular estimate has low precision, the test is disturbed easily, and the tester is fatigable.

Description

A kind of damage tolerance test crack detection device
Technical field
The utility model relates to a kind of a kind of damage tolerance test crack detection device that is used for torture test.
Background technology
At present, fatigue criterion pilot system system in process of the test can't write down the testpieces crackle automatically both at home and abroad, need testing crew to adopt ocular estimate manual record crack propagation situation, it is bigger that there is the measuring intervals of TIME out of true in manual record, measuring accuracy is low, measurement result is influenced by record's individual difference, and the more high shortcoming of cost of labor.
Summary of the invention
The purpose of this utility model provides a kind of a kind of damage tolerance test crack detection device that can write down crack extending length automatically.Technical solution of the present utility model is, pick-up unit comprises control computer, digital camera, and digital camera places on the testing table and testpieces placed in the view area of digital camera, and digital camera and control computer are joined.Advantage that the utlity model has and beneficial effect, the utility model can load number of times according to test and send trigger pip, or send trigger pip according to the test load value, and testpieces is carried out crack propagation situation record, the crackle photo is preserved easily and is also conveniently carried out the crack propagation situation analysis.Reduced the testing crew workload, avoided the ocular estimate precision low, be subject to disturb, the fatigable shortcoming of survey crew.
Description of drawings
Fig. 1 is a structural representation of the present utility model
Embodiment
Below in conjunction with accompanying drawing the utility model is elaborated.Pick-up unit comprises control computer 1, digital camera 3, and digital camera 3 places on the testing table and testpieces 4 placed in the view area of digital camera 3, and digital camera 3 joins with control computer 1.
Annexation of the present utility model
System mainly is made up of universal test bench, hydraulic system and control system.
Digital camera 3 triggers lead 2 by digital camera and is connected on the control computer 1, and digital camera 3 is placed on the correct position of testing table, and accurate testpieces 4 is in the viewing area of digital camera, regulates focal length that digital camera 3 needs and light etc. at last.
Operating process of the present utility model
Open control computer 1 starting characteristics test, thin-walled single panel type testpieces 4 is subjected to Tensile or Compressive Loading, and crackle 5 is expanded gradually, sends trigger pip according to testing requirements by control computer 1, by lead 2 control digital cameras 3, the record crackle 5 of taking pictures.The photo of taking is kept in the digital camera 3, and the relevant information of the load of every photo correspondence and time is kept in the control computer 1 so that the testing crew editing and processing.
Automatically the record crack propagation has two kinds of triggering modes:
● the test run number of times that every interval is predetermined, control computer 1 triggers lead 2 by digital camera and triggers digital camera 3 automatic cameras 1 time, the crackle 5 of record testpieces 4;
● whenever reach predetermined test load bid value, control computer 1 triggers lead 2 by digital camera and triggers digital camera 3 automatic cameras 1 time, the crackle 5 of record testpieces 4.

Claims (1)

1. a damage tolerance is tested crack detection device, it is characterized in that, pick-up unit comprises control computer (1), digital camera (3), digital camera (3) places on the testing table and with testpieces (4) and places in the view area of digital camera (3), and digital camera (3) joins with control computer (1).
CN2010200000634U 2010-01-06 2010-01-06 Damage tolerance test crack detection device Expired - Fee Related CN201569606U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2010200000634U CN201569606U (en) 2010-01-06 2010-01-06 Damage tolerance test crack detection device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2010200000634U CN201569606U (en) 2010-01-06 2010-01-06 Damage tolerance test crack detection device

Publications (1)

Publication Number Publication Date
CN201569606U true CN201569606U (en) 2010-09-01

Family

ID=42661900

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2010200000634U Expired - Fee Related CN201569606U (en) 2010-01-06 2010-01-06 Damage tolerance test crack detection device

Country Status (1)

Country Link
CN (1) CN201569606U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104833598A (en) * 2015-05-05 2015-08-12 上海工程技术大学 Observation system for fatigue crack expansion of metal material
CN105842061B (en) * 2016-05-30 2019-03-19 中国航空工业集团公司北京航空材料研究院 It is a kind of for testing the experimental rig of aircraft target ship damage tolerance performance

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104833598A (en) * 2015-05-05 2015-08-12 上海工程技术大学 Observation system for fatigue crack expansion of metal material
CN104833598B (en) * 2015-05-05 2018-01-30 上海工程技术大学 A kind of observation system for Metal Material Fatigue Crack Extension
CN105842061B (en) * 2016-05-30 2019-03-19 中国航空工业集团公司北京航空材料研究院 It is a kind of for testing the experimental rig of aircraft target ship damage tolerance performance

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20100901

Termination date: 20150106

EXPY Termination of patent right or utility model