CN101907538A - Mechanical biaxial tension tester with variable proportion loading - Google Patents
Mechanical biaxial tension tester with variable proportion loading Download PDFInfo
- Publication number
- CN101907538A CN101907538A CN 201010240086 CN201010240086A CN101907538A CN 101907538 A CN101907538 A CN 101907538A CN 201010240086 CN201010240086 CN 201010240086 CN 201010240086 A CN201010240086 A CN 201010240086A CN 101907538 A CN101907538 A CN 101907538A
- Authority
- CN
- China
- Prior art keywords
- angled
- lift splits
- plane
- angle
- trapezoidal inclined
- 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.)
- Granted
Links
Images
Landscapes
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
Abstract
The invention discloses a mechanical biaxial tension tester with variable proportion loading, relating to a biaxial tension tester. The invention solves the problem that the traditional biaxial tension testing device can not realize variable proportion loading under a complex loading path. In the invention, a slanting slide block is an inverted trapezoidal quadrangular frustum pyramid, a workbench is provided with a cruciform chute, a cruciform test piece is arranged above the cruciform chute, four ends of the cruciform test piece are respectively and fixedly connected with a clamping head, a tension-compression sensor is fixedly connected to the outer end surface of each clamping head, the outer end of each tension-compression sensor is fixedly connected with a horizontal slide block, each horizontal slide block is installed on the workbench, the lower end of each slant beam is fixedly connected with a horizontal slide block, a rolling bearing is installed at the upper end of each slant beam, and each rolling bearing is contacted with a corresponding trapezoidal inclined plane of each slant beam and rolls on the corresponding trapezoidal inclined plane of each slant beam. The invention is suitable for a tension test of the cruciform test piece.
Description
Technical field
The present invention relates to a kind of biaxial tension tester, be specifically related to the mechanical biaxial tension tester that a kind of control with changed scale loads.
Background technology
Since Plate Theory was set up, growing field was used plate and shell structure, and particularly the most space container of aerospace field all is the bidirectional stress structure, as spherical vessel and thin-walled cartridge type spare etc.In order to solve its structure and performance issue, increasing people is devoted to biaxial tensile test since the forties in last century.Up to the present, biaxial tensile test does not well solve as yet, and reason is exactly the complicacy of two drawing device designs greatly.Scholars have studied dissimilar biaxial tensile test methods at different times, draw test as two under the unilateral stretching, the protruding two tests of drawing of expanding of film, and pressure vessel is two to draw test, and cruciform specimen is two to draw test etc.Draw the biaxial stress state of the most direct reaction test specimen directly perceived of test because cruciform specimen is two,, mainly studied the two-way stretch device of mechanical type and fluid pressure type once occurring just having attracted numerous researchers.
Existing mechanical biaxial tension test unit (referring to Fig. 7 and Fig. 8): it can not realize that the two-way arbitrary proportion of X-Y loads, and can only do specific ratio and load.Under the effect that loads, pressure head moves down, and the hound of directions X and Y direction and the angle of horizontal direction change in time, can not guarantee that the loading of X-Y direction becomes constant ratio.Up to the present the whole bag of tricks and device can't realize that all control with changed scale loads under the complicated load path.
Summary of the invention
The objective of the invention is can't realize the problem of control with changed scale loading under the complicated load path in order to solve existing bidirectional tensile tester, and then the mechanical biaxial tension tester that provides a kind of control with changed scale to load.
Technical scheme of the present invention is: the mechanical biaxial tension tester that control with changed scale loads comprises worktable, four hounds, four tension-compression sensors and four chucks; Described biaxial tension tester also comprises angled-lift splits, four rolling bearings and four cross sliding clocks, described angled-lift splits is inverted trapezoidal truncated rectangular pyramids, have cross chute on the described worktable, cruciform specimen places the top of cross chute, each fixedlys connected four terminations of cruciform specimen with a chuck, be fixedly connected with a tension-compression sensor on the outer face of each chuck, fixedly connected with a cross sliding clock in the outer end of each tension-compression sensor, each cross sliding clock is installed on the worktable, and each cross sliding clock smoothly moves in cross chute, fixedly connected with a cross sliding clock in the lower end of each hound, the upper end of each hound is equipped with a rolling bearing, each rolling bearing contacts with a corresponding trapezoidal inclined-plane of angled-lift splits, each rolling bearing rolls on a corresponding trapezoidal inclined-plane of angled-lift splits, fixedly connected with the pressure head of testing machine in the upper surface of angled-lift splits, the angle of each hound and surface level is 30 ° ~ 70 °, the trapezoidal inclined-plane of the left and right sides of angled-lift splits and the angle of upper surface are 20 °~80 °, and the trapezoidal inclined-plane of the both sides, front and back of angled-lift splits and the angle of upper surface are 20 °~80 °.
The present invention compared with prior art has following effect: the mechanical biaxial tension tester that control with changed scale of the present invention loads resolves into orthogonal two groups of loadings on the surface level to the loading on the vertical direction by angled-lift splits.Because the oblique angle on the trapezoidal inclined-plane of two couples of same angled-lift splits is certain, trapezoidal inclined-plane contacts with the rolling bearing line, not only can reduce friction greatly, and the ratio that can guarantee the loading of two vertical direction on the horizontal direction is constant in entire test, can obtain the fore-and-aft direction loading ratio different on the surface level by the angled-lift splits that calls different angles with left and right directions, promptly obtain the different loading ratio of X-Y direction, realize that two pahtfinder hard control with changed scale of cruciform specimen of drawing load.
Description of drawings
Fig. 1 is that (X-axis is the left and right directions of tension test instrument to integrally-built stereographic map of the present invention among the figure, Y-axis is the fore-and-aft direction of tension test instrument), Fig. 2 is an one-piece construction front view of the present invention, Fig. 3 is an integrally-built rear view of the present invention, Fig. 4 is the front view of angled-lift splits 1, and Fig. 5 is the left view of angled-lift splits 1, and Fig. 6 is the upward view of Fig. 4, Fig. 7 is the front view of existing mechanical biaxial tension test unit, and Fig. 8 is the side view of existing mechanical biaxial tension test unit.
Embodiment
Embodiment one: in conjunction with Fig. 1~Fig. 6 present embodiment is described, the mechanical biaxial tension tester that the control with changed scale of present embodiment loads comprises worktable 6, four hounds 3, four tension-compression sensors 5 and four chucks 8; Described biaxial tension tester also comprises angled-lift splits 1, four rolling bearings 2 and four cross sliding clocks 4, described angled-lift splits 1 is inverted trapezoidal truncated rectangular pyramids, have cross chute 6-1 on the described worktable 6, cruciform specimen 7 places the top of cross chute 6-1, each fixedlys connected four terminations of cruciform specimen 7 with a chuck 8, be fixedly connected with a tension-compression sensor 5 on the outer face of each chuck 8, fixedly connected with a cross sliding clock 4 in the outer end of each tension-compression sensor 5, each cross sliding clock 4 is installed on the worktable 6, and each cross sliding clock 4 smoothly moves in cross chute 6-1, fixedly connected with a cross sliding clock 4 in the lower end of each hound 3, the upper end of each hound 3 is equipped with a rolling bearing 2, each rolling bearing 2 contacts with a corresponding trapezoidal inclined-plane of angled-lift splits 1, each rolling bearing 2 rolls on a corresponding trapezoidal inclined-plane of angled-lift splits 1, fixedly connected with the pressure head of testing machine 9 in the upper surface of angled-lift splits 1, each hound 3 is 30 ° ~ 70 ° with the angle α of surface level, the trapezoidal inclined-plane 1-1 of the left and right sides of angled-lift splits 1 and the angle β of upper surface are 20 °~80 °, and the trapezoidal inclined-plane 1-2 of the both sides, front and back of angled-lift splits 1 and the angle γ of upper surface are 20 °~80 °.
The cross sliding clock 4 of the present embodiment guide rail guidance system that the level and smooth working method that moves adopts in the cross chute 6-1 of worktable 6, for example the notch Cross section Design of cross chute 6-1 is a dovetail groove, the lower end design of cross sliding clock 4 has the shoulder that matches with dovetail groove, perhaps the notch Cross section Design of cross chute 6-1 is straight mouthful groove, the lower end design of cross sliding clock 4 has shoulder, adopt pressing plate that the shoulder of cross sliding clock 4 is pressed in the cross chute 6-1 then, adopt dovetail groove to be convenient to install, adopt a straight mouthful groove to be convenient to processing.
Embodiment two: in conjunction with Fig. 2 and Fig. 3 present embodiment is described, each hound 3 of present embodiment is 45 ° with the angle α of surface level.So be provided with, make the decomposing force that hound can be good arrive horizontal direction, satisfy restriction simultaneously moment.Other composition is identical with embodiment one with annexation.
Embodiment three: present embodiment is described in conjunction with Fig. 1, Fig. 4 and Fig. 5, the trapezoidal inclined-plane 1-1 of the left and right sides of the angled-lift splits 1 of present embodiment and the angle β of upper surface are 45 °, and the trapezoidal inclined-plane 1-2 of the both sides, front and back of angled-lift splits 1 and the angle γ of upper surface are 78 °.So be provided with, the ratio that obtains X-Y direction 8:1 loads.Other composition is identical with embodiment one or two with annexation.
Embodiment four: present embodiment is described in conjunction with Fig. 1, Fig. 4 and Fig. 5, the trapezoidal inclined-plane 1-1 of the left and right sides of the angled-lift splits 1 of present embodiment and the angle β of upper surface are 45 °, and the trapezoidal inclined-plane 1-2 of the both sides, front and back of angled-lift splits 1 and the angle γ of upper surface are 76 °.So be provided with, the ratio that obtains X-Y direction 4:1 loads.Other composition is identical with embodiment one or two with annexation.
Embodiment five: present embodiment is described in conjunction with Fig. 1, Fig. 4 and Fig. 5, the trapezoidal inclined-plane 1-1 of the left and right sides of the angled-lift splits 1 of present embodiment and the angle β of upper surface are 30 °, and the trapezoidal inclined-plane 1-2 of the both sides, front and back of angled-lift splits 1 and the angle γ of upper surface are 60 °.So be provided with, the ratio that obtains X-Y direction 3:1 loads.Other composition is identical with embodiment one or two with annexation.
Embodiment six: present embodiment is described in conjunction with Fig. 1, Fig. 4 and Fig. 5, the trapezoidal inclined-plane 1-1 of the left and right sides of the angled-lift splits 1 of present embodiment and the angle β of upper surface are 45 °, and the trapezoidal inclined-plane 1-2 of the both sides, front and back of angled-lift splits 1 and the angle γ of upper surface are 63 °.So be provided with, the ratio that obtains X-Y direction 2:1 loads.Other composition is identical with embodiment one or two with annexation.
Embodiment seven: present embodiment is described in conjunction with Fig. 1, Fig. 4 and Fig. 5, the trapezoidal inclined-plane 1-1 of the left and right sides of the angled-lift splits 1 of present embodiment and the angle β of upper surface are 45 °, and the trapezoidal inclined-plane 1-2 of the both sides, front and back of angled-lift splits 1 and the angle γ of upper surface are 45 °.So be provided with, obtain X-Y direction equal proportion and load.Other composition is identical with embodiment one or two with annexation.
Embodiment eight: present embodiment is described in conjunction with Fig. 1, Fig. 4 and Fig. 5, the trapezoidal inclined-plane 1-1 of the left and right sides of the angled-lift splits 1 of present embodiment and the angle β of upper surface are 63 °, and the trapezoidal inclined-plane 1-2 of the both sides, front and back of angled-lift splits 1 and the angle γ of upper surface are 45 °.So be provided with, the ratio that obtains X-Y direction 1:2 loads.Other composition is identical with embodiment one or two with annexation.
Embodiment nine: present embodiment is described in conjunction with Fig. 1, Fig. 4 and Fig. 5, the trapezoidal inclined-plane 1-1 of the left and right sides of the angled-lift splits 1 of present embodiment and the angle β of upper surface are 60 °, and the trapezoidal inclined-plane 1-2 of the both sides, front and back of angled-lift splits 1 and the angle γ of upper surface are 30 °.So be provided with, the ratio that obtains X-Y direction 1:3 loads.Other composition is identical with embodiment one or two with annexation.
Embodiment ten: present embodiment is described in conjunction with Fig. 1, Fig. 4 and Fig. 5, the trapezoidal inclined-plane 1-1 of the left and right sides of the angled-lift splits 1 of present embodiment and the angle β of upper surface are 76 °, and the trapezoidal inclined-plane 1-2 of the both sides, front and back of angled-lift splits 1 and the angle γ of upper surface are 45 °.So be provided with, the ratio that obtains X-Y direction 1:4 loads.Other composition is identical with embodiment one or two with annexation.
Embodiment 11: present embodiment is described in conjunction with Fig. 1~Fig. 3, the mechanical biaxial tension tester that the control with changed scale of present embodiment loads also increases four threaded mandrels 10 and four end plates 11, respectively be installed with an end plate 11 on the end face around the worktable 6, each threaded mandrel 10 is threaded with corresponding end plate 11, and the inner of threaded mandrel 10 contacts with cross sliding clock 4 when adjusting cross sliding clock 4.The adjustment of cross sliding clock 4 positions before and after being convenient to test so is set.Other composition is identical with embodiment one, two, three, four, five, six, seven, eight or nine with annexation.
The course of work: angled-lift splits 1 is connected with the pressure head 9 of testing machine, the trapezoidal inclined-plane that the pressure head 9 of testing machine presses down angled-lift splits 1 in the process contacts with rolling bearing 2, and drive hound 3 and cross sliding clock 4 along orthogonal directions X on the surface level and the translation gliding of Y direction, cross sliding clock 4 connects tension-compression sensor 5, the other end of tension-compression sensor 5 chuck 8 of ining succession, cruciform specimen 7 in chuck 8 clampings, realizes the stretching to cruciform specimen 7.The deflection of the directions X of cruciform specimen 7 and Y direction and pulling force are measured by tension-compression sensor 5, signal is by the data acquisition software acquisition process, record data and the in real time pulling force-displacement curve of sample on directions X and the Y direction on the reveal competence direction on computers obtain stress-strain curve by post-processed.
Claims (10)
1. the mechanical biaxial tension tester that loads of a control with changed scale, it comprises worktable (6), four hounds (3), four tension-compression sensors (5) and four chucks (8); It is characterized in that: described biaxial tension tester also comprises angled-lift splits (1), four rolling bearings (2) and four cross sliding clocks (4), described angled-lift splits (1) is inverted trapezoidal truncated rectangular pyramids, have cross chute (6-1) on the described worktable (6), cruciform specimen (7) places the top of cross chute (6-1), each fixedlys connected four terminations of cruciform specimen (7) with a chuck (8), be fixedly connected with a tension-compression sensor (5) on the outer face of each chuck (8), fixedly connected with a cross sliding clock (4) in the outer end of each tension-compression sensor (5), each cross sliding clock (4) is installed on the worktable (6), and each cross sliding clock (4) is level and smooth moving in cross chute (6-1), fixedly connected with a cross sliding clock (4) in the lower end of each hound (3), the upper end of each hound (3) is equipped with a rolling bearing (2), each rolling bearing (2) contacts with a corresponding trapezoidal inclined-plane of angled-lift splits (1), each rolling bearing (2) rolls on a corresponding trapezoidal inclined-plane of angled-lift splits (1), fixedly connected with the pressure head (9) of testing machine in the upper surface of angled-lift splits (1), each hound (3) is 30 ° ~ 70 ° with the angle (α) of surface level, the trapezoidal inclined-plane (1-1) of the left and right sides of angled-lift splits (1) is 20 °~80 ° with the angle (β) of upper surface, and the trapezoidal inclined-plane (1-2) of the both sides, front and back of angled-lift splits (1) is 20 °~80 ° with the angle (γ) of upper surface.
2. the mechanical biaxial tension tester that control with changed scale according to claim 1 loads is characterized in that: each hound (3) is 45 ° with the angle (α) of surface level.
3. the mechanical biaxial tension tester that control with changed scale according to claim 1 and 2 loads, it is characterized in that: the trapezoidal inclined-plane (1-1) of the left and right sides of angled-lift splits (1) is 45 ° with the angle (β) of upper surface, and the trapezoidal inclined-plane (1-2) of the both sides, front and back of angled-lift splits (1) is 78 ° with the angle (γ) of upper surface.
4. the mechanical biaxial tension tester that control with changed scale according to claim 1 and 2 loads, it is characterized in that: the trapezoidal inclined-plane (1-1) of the left and right sides of angled-lift splits (1) is 45 ° with the angle (β) of upper surface, and the trapezoidal inclined-plane (1-2) of the both sides, front and back of angled-lift splits (1) is 76 ° with the angle (γ) of upper surface.
5. the mechanical biaxial tension tester that control with changed scale according to claim 1 and 2 loads, it is characterized in that: the trapezoidal inclined-plane (1-1) of the left and right sides of angled-lift splits (1) is 30 ° with the angle (β) of upper surface, and the trapezoidal inclined-plane (1-2) of the both sides, front and back of angled-lift splits (1) is 60 ° with the angle (γ) of upper surface.
6. the mechanical biaxial tension tester that control with changed scale according to claim 1 and 2 loads, it is characterized in that: the trapezoidal inclined-plane (1-1) of the left and right sides of angled-lift splits (1) is 45 ° with the angle (β) of upper surface, and the trapezoidal inclined-plane (1-2) of the both sides, front and back of angled-lift splits (1) is 63 ° with the angle (γ) of upper surface.
7. the mechanical biaxial tension tester that control with changed scale according to claim 1 and 2 loads, it is characterized in that: the trapezoidal inclined-plane (1-1) of the left and right sides of angled-lift splits (1) is 45 ° with the angle (β) of upper surface, and the trapezoidal inclined-plane (1-2) of the both sides, front and back of angled-lift splits (1) is 45 ° with the angle (γ) of upper surface.
8. the mechanical biaxial tension tester that control with changed scale according to claim 1 and 2 loads, it is characterized in that: the trapezoidal inclined-plane (1-1) of the left and right sides of angled-lift splits (1) is 63 ° with the angle (β) of upper surface, and the trapezoidal inclined-plane (1-2) of the both sides, front and back of angled-lift splits (1) is 45 ° with the angle (γ) of upper surface.
9. the mechanical biaxial tension tester that control with changed scale according to claim 1 and 2 loads, it is characterized in that: the trapezoidal inclined-plane (1-1) of the left and right sides of angled-lift splits (1) is 60 ° with the angle (β) of upper surface, and the trapezoidal inclined-plane (1-2) of the both sides, front and back of angled-lift splits (1) is 30 ° with the angle (γ) of upper surface.
10. the mechanical biaxial tension tester that control with changed scale according to claim 1 and 2 loads, it is characterized in that: the mechanical biaxial tension tester that described control with changed scale loads also comprises four threaded mandrels (10) and four end plates (11), respectively be installed with an end plate (11) on the end face around the worktable (6), each threaded mandrel (10) is threaded with corresponding end plate (11), and the inner of threaded mandrel (10) contacts with cross sliding clock (4) when adjusting cross sliding clock (4).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2010102400867A CN101907538B (en) | 2010-07-29 | 2010-07-29 | Mechanical biaxial tension tester with variable proportion loading |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2010102400867A CN101907538B (en) | 2010-07-29 | 2010-07-29 | Mechanical biaxial tension tester with variable proportion loading |
Publications (2)
Publication Number | Publication Date |
---|---|
CN101907538A true CN101907538A (en) | 2010-12-08 |
CN101907538B CN101907538B (en) | 2012-04-18 |
Family
ID=43263061
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2010102400867A Expired - Fee Related CN101907538B (en) | 2010-07-29 | 2010-07-29 | Mechanical biaxial tension tester with variable proportion loading |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN101907538B (en) |
Cited By (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102507320A (en) * | 2011-10-25 | 2012-06-20 | 华南理工大学 | Single-power two-way stretching method and device |
CN102706731A (en) * | 2012-06-14 | 2012-10-03 | 河南理工大学 | Biaxial tension test device for testing performance of sheet metal |
RU2464545C1 (en) * | 2011-05-03 | 2012-10-20 | Открытое акционерное общество "Рязанское конструкторское бюро "Глобус" | Device for creation of force fields at strength tests of load handling facilities |
CN103512809A (en) * | 2013-09-24 | 2014-01-15 | 清华大学苏州汽车研究院(相城) | Equiaxial tensile test device for elastic material |
CN103645045A (en) * | 2013-12-24 | 2014-03-19 | 威海市试验机制造有限公司 | Aircraft inclined stay bar testing machine |
CN104359767A (en) * | 2014-10-18 | 2015-02-18 | 吉林大学 | High-temperature biaxial tension device |
CN105092373A (en) * | 2014-05-13 | 2015-11-25 | 株式会社岛津制作所 | Material testing machine |
CN105403456A (en) * | 2016-01-08 | 2016-03-16 | 西安科技大学 | Metal material monoaxial performance test clamp |
CN105424471A (en) * | 2015-12-24 | 2016-03-23 | 合肥工业大学 | Sheet metal bidirectional stretching apparatus based on die technology |
CN105571942A (en) * | 2015-12-15 | 2016-05-11 | 中国科学院力学研究所 | Bidirectional test device and test method for single-shaft material test machine |
CN105758722A (en) * | 2016-02-26 | 2016-07-13 | 重庆大学 | Simple and stretching ratio adjustable type double-shaft synchronous stretching device and method |
CN105842055A (en) * | 2016-03-15 | 2016-08-10 | 北京航空航天大学 | Strength testing fixture using uniaxial testing machine for variable-proportion biaxial loading |
CN106289968A (en) * | 2015-06-23 | 2017-01-04 | 核工业北京地质研究院 | A kind of assay device for different sliding distance loading heads |
CN106525593A (en) * | 2016-12-29 | 2017-03-22 | 清华大学苏州汽车研究院(相城) | Equal biaxial tensile test device |
CN106644720A (en) * | 2016-12-27 | 2017-05-10 | 重庆大学 | Biaxial stretching device for realizing adjustable stress and strain ratio based on unidirectional testing machine |
CN106896028A (en) * | 2017-02-28 | 2017-06-27 | 天津工业大学 | Three dimensional fabric shearing, biaxial stretching experimental rig and method |
CN106908319A (en) * | 2017-03-27 | 2017-06-30 | 山东大学 | A kind of two-way cross tensile test device |
CN106932274A (en) * | 2017-03-07 | 2017-07-07 | 南京航空航天大学 | For the device and method of material biaxial tension test load test |
CN107255587A (en) * | 2017-07-28 | 2017-10-17 | 中南大学 | A kind of creep ageing two-direction pull press experimental rig |
CN107941598A (en) * | 2017-12-07 | 2018-04-20 | 中国商用飞机有限责任公司 | Biaxial tension loading device |
CN107966367A (en) * | 2017-12-29 | 2018-04-27 | 山东省建筑科学研究院 | A kind of biaxial tension verifying attachment and method for cross shaped head welded reinforcement part |
CN108956290A (en) * | 2018-06-11 | 2018-12-07 | 哈尔滨工程大学 | The isometric extension test platform of rubber plane |
CN109163975A (en) * | 2018-11-09 | 2019-01-08 | 中南大学 | A kind of biaxial stretch-formed experimental provision of rock and its application method |
CN109297811A (en) * | 2018-09-28 | 2019-02-01 | 西北工业大学 | Double-shaft two-way compression-loaded devices and methods therefor |
CN111044363A (en) * | 2019-12-09 | 2020-04-21 | 上海交通大学 | Biaxial tension experimental device with variable load ratio |
CN111060397A (en) * | 2019-11-29 | 2020-04-24 | 南京航空航天大学 | Novel four-axis bidirectional loading device and test method thereof |
CN112461652A (en) * | 2020-11-06 | 2021-03-09 | 中国人民解放军火箭军工程大学 | Material performance testing device and method for converting uniaxial drive into biaxial variable-ratio stretching |
CN113155619A (en) * | 2021-04-30 | 2021-07-23 | 吉林大学 | Quasi-static in-situ biaxial stretching mechanical property testing device under scanning electron microscope |
CN113281167A (en) * | 2021-05-19 | 2021-08-20 | 中南大学 | Experimental device and method for realizing bidirectional uniform-speed stretching or compression loading |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SU864046A1 (en) * | 1979-08-22 | 1981-09-15 | Тольяттинский политехнический институт | Apparatus for testing sheet specimens for biaxial tension |
JPS58173450A (en) * | 1982-04-06 | 1983-10-12 | Taiyo Kogyo Kk | Biaxial tension tester |
CN87205653U (en) * | 1987-03-28 | 1987-12-02 | 华南工学院 | Mechanical double directions tensile tester |
US7204160B1 (en) * | 2004-05-24 | 2007-04-17 | The United States Of America As Represented By The Secretary Of The Navy | Biaxial and shear testing apparatus with force controls |
CN101561376A (en) * | 2008-04-17 | 2009-10-21 | 西北工业大学 | Bidirectional tensile tester |
-
2010
- 2010-07-29 CN CN2010102400867A patent/CN101907538B/en not_active Expired - Fee Related
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SU864046A1 (en) * | 1979-08-22 | 1981-09-15 | Тольяттинский политехнический институт | Apparatus for testing sheet specimens for biaxial tension |
JPS58173450A (en) * | 1982-04-06 | 1983-10-12 | Taiyo Kogyo Kk | Biaxial tension tester |
CN87205653U (en) * | 1987-03-28 | 1987-12-02 | 华南工学院 | Mechanical double directions tensile tester |
US7204160B1 (en) * | 2004-05-24 | 2007-04-17 | The United States Of America As Represented By The Secretary Of The Navy | Biaxial and shear testing apparatus with force controls |
CN101561376A (en) * | 2008-04-17 | 2009-10-21 | 西北工业大学 | Bidirectional tensile tester |
Non-Patent Citations (2)
Title |
---|
《岳阳大学学报》 19901031 李冈陵等 双向拉伸试验研究 第3卷, 第2期 2 * |
《岳阳师范学院学报》 20000331 陈积光等 TA2薄板的双向拉伸试验研究 第13卷, 第1期 2 * |
Cited By (43)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2464545C1 (en) * | 2011-05-03 | 2012-10-20 | Открытое акционерное общество "Рязанское конструкторское бюро "Глобус" | Device for creation of force fields at strength tests of load handling facilities |
CN102507320A (en) * | 2011-10-25 | 2012-06-20 | 华南理工大学 | Single-power two-way stretching method and device |
CN102507320B (en) * | 2011-10-25 | 2014-04-02 | 华南理工大学 | Single-power two-way stretching method and device |
CN102706731A (en) * | 2012-06-14 | 2012-10-03 | 河南理工大学 | Biaxial tension test device for testing performance of sheet metal |
CN103512809A (en) * | 2013-09-24 | 2014-01-15 | 清华大学苏州汽车研究院(相城) | Equiaxial tensile test device for elastic material |
CN103512809B (en) * | 2013-09-24 | 2017-01-04 | 清华大学苏州汽车研究院(相城) | A kind of Equiaxial tensile test device for elastic material |
CN103645045A (en) * | 2013-12-24 | 2014-03-19 | 威海市试验机制造有限公司 | Aircraft inclined stay bar testing machine |
CN105092373A (en) * | 2014-05-13 | 2015-11-25 | 株式会社岛津制作所 | Material testing machine |
JP2015215289A (en) * | 2014-05-13 | 2015-12-03 | 株式会社島津製作所 | Material testing machine |
CN104359767A (en) * | 2014-10-18 | 2015-02-18 | 吉林大学 | High-temperature biaxial tension device |
CN106289968A (en) * | 2015-06-23 | 2017-01-04 | 核工业北京地质研究院 | A kind of assay device for different sliding distance loading heads |
CN105571942A (en) * | 2015-12-15 | 2016-05-11 | 中国科学院力学研究所 | Bidirectional test device and test method for single-shaft material test machine |
CN105424471A (en) * | 2015-12-24 | 2016-03-23 | 合肥工业大学 | Sheet metal bidirectional stretching apparatus based on die technology |
CN105424471B (en) * | 2015-12-24 | 2018-05-01 | 合肥工业大学 | Sheet metal two-way stretch device based on Tool and Die Technology |
CN105403456A (en) * | 2016-01-08 | 2016-03-16 | 西安科技大学 | Metal material monoaxial performance test clamp |
CN105403456B (en) * | 2016-01-08 | 2018-11-02 | 西安科技大学 | A kind of metal material single shaft performance test fixture |
CN105758722B (en) * | 2016-02-26 | 2019-05-17 | 重庆大学 | A kind of easy, the adjustable Dual-shaft synchronous stretching device of stretch ratio and method |
CN105758722A (en) * | 2016-02-26 | 2016-07-13 | 重庆大学 | Simple and stretching ratio adjustable type double-shaft synchronous stretching device and method |
CN105842055A (en) * | 2016-03-15 | 2016-08-10 | 北京航空航天大学 | Strength testing fixture using uniaxial testing machine for variable-proportion biaxial loading |
CN105842055B (en) * | 2016-03-15 | 2018-05-18 | 北京航空航天大学 | A kind of strength test fixture that control with changed scale Biaxial stress is carried out using single axis test machines |
CN106644720A (en) * | 2016-12-27 | 2017-05-10 | 重庆大学 | Biaxial stretching device for realizing adjustable stress and strain ratio based on unidirectional testing machine |
CN106525593A (en) * | 2016-12-29 | 2017-03-22 | 清华大学苏州汽车研究院(相城) | Equal biaxial tensile test device |
CN106896028A (en) * | 2017-02-28 | 2017-06-27 | 天津工业大学 | Three dimensional fabric shearing, biaxial stretching experimental rig and method |
CN106932274A (en) * | 2017-03-07 | 2017-07-07 | 南京航空航天大学 | For the device and method of material biaxial tension test load test |
CN106908319A (en) * | 2017-03-27 | 2017-06-30 | 山东大学 | A kind of two-way cross tensile test device |
CN106908319B (en) * | 2017-03-27 | 2019-11-19 | 山东大学 | A kind of two-way cross tensile test device |
CN107255587A (en) * | 2017-07-28 | 2017-10-17 | 中南大学 | A kind of creep ageing two-direction pull press experimental rig |
CN107941598A (en) * | 2017-12-07 | 2018-04-20 | 中国商用飞机有限责任公司 | Biaxial tension loading device |
CN107941598B (en) * | 2017-12-07 | 2021-05-07 | 中国商用飞机有限责任公司 | Bidirectional stretching loading device |
CN107966367A (en) * | 2017-12-29 | 2018-04-27 | 山东省建筑科学研究院 | A kind of biaxial tension verifying attachment and method for cross shaped head welded reinforcement part |
CN107966367B (en) * | 2017-12-29 | 2024-03-29 | 山东省建筑科学研究院有限公司 | Biaxial stretching inspection device and method for cross-shaped welded steel bar |
CN108956290A (en) * | 2018-06-11 | 2018-12-07 | 哈尔滨工程大学 | The isometric extension test platform of rubber plane |
CN109297811A (en) * | 2018-09-28 | 2019-02-01 | 西北工业大学 | Double-shaft two-way compression-loaded devices and methods therefor |
CN109163975B (en) * | 2018-11-09 | 2020-11-06 | 中南大学 | Rock biaxial tension experimental device and application method thereof |
CN109163975A (en) * | 2018-11-09 | 2019-01-08 | 中南大学 | A kind of biaxial stretch-formed experimental provision of rock and its application method |
CN111060397A (en) * | 2019-11-29 | 2020-04-24 | 南京航空航天大学 | Novel four-axis bidirectional loading device and test method thereof |
CN111060397B (en) * | 2019-11-29 | 2022-06-10 | 南京航空航天大学 | Four-axis bidirectional loading device and test method thereof |
CN111044363A (en) * | 2019-12-09 | 2020-04-21 | 上海交通大学 | Biaxial tension experimental device with variable load ratio |
CN112461652A (en) * | 2020-11-06 | 2021-03-09 | 中国人民解放军火箭军工程大学 | Material performance testing device and method for converting uniaxial drive into biaxial variable-ratio stretching |
CN112461652B (en) * | 2020-11-06 | 2024-03-19 | 中国人民解放军火箭军工程大学 | Testing device and method for converting uniaxial drive into biaxial variable-proportion stretching |
CN113155619A (en) * | 2021-04-30 | 2021-07-23 | 吉林大学 | Quasi-static in-situ biaxial stretching mechanical property testing device under scanning electron microscope |
CN113155619B (en) * | 2021-04-30 | 2022-06-07 | 吉林大学 | Quasi-static in-situ biaxial stretching mechanical property testing device under scanning electron microscope |
CN113281167A (en) * | 2021-05-19 | 2021-08-20 | 中南大学 | Experimental device and method for realizing bidirectional uniform-speed stretching or compression loading |
Also Published As
Publication number | Publication date |
---|---|
CN101907538B (en) | 2012-04-18 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN101907538B (en) | Mechanical biaxial tension tester with variable proportion loading | |
CN102095647B (en) | Device for testing mechanical properties of thin sheet under simple shear loading | |
CN103969107B (en) | High pressure servo moves true triaxial test machine | |
CN201233218Y (en) | Battery thickness measuring instrument | |
CN102507320B (en) | Single-power two-way stretching method and device | |
CN102353578B (en) | Testing device for two-way loading test of material | |
CN204314136U (en) | The normal direction loading equipemtn of fretting fatigue testing system | |
CN106644720A (en) | Biaxial stretching device for realizing adjustable stress and strain ratio based on unidirectional testing machine | |
CN105424471B (en) | Sheet metal two-way stretch device based on Tool and Die Technology | |
CN206192776U (en) | Tensile testing machine | |
CN103558083B (en) | A kind of Fracture of Metal Material performance wedging method of testing and device | |
CN104568619A (en) | Normal loading device of fretting fatigue test system | |
CN105928785A (en) | Metal plate pulling-pressing experiment device in pure mechanical structure form | |
CN106353181A (en) | Asymmetric clamping device and experimental method for sheet compressing | |
CN204535922U (en) | A kind of mass property measures auxiliary clamp | |
CN106918417A (en) | Steel plate membrane stress tests force application apparatus | |
CN203811459U (en) | Static load test device for concrete beam | |
CN207280855U (en) | A kind of measurer for pulling force | |
CN202583020U (en) | Durometer | |
CN100476396C (en) | Pressing lever steady experimental device for electronic universal testing machine | |
CN104034474B (en) | 3-SPU six-dimensional force cell sensor in parallel | |
CN203965246U (en) | A kind of proving installation that obtains faying face normal contact stiffness | |
CN202630878U (en) | Taper detection device of large taper hole | |
CN204613051U (en) | Two-dimensional friction testing device | |
CN107767752B (en) | Deformation broken block device in fault simulation module device |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120418 Termination date: 20210729 |