CN104344997A - Passive type restraint loading device for triaxial test - Google Patents
Passive type restraint loading device for triaxial test Download PDFInfo
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- CN104344997A CN104344997A CN201410613856.6A CN201410613856A CN104344997A CN 104344997 A CN104344997 A CN 104344997A CN 201410613856 A CN201410613856 A CN 201410613856A CN 104344997 A CN104344997 A CN 104344997A
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- 238000012360 testing method Methods 0.000 title claims abstract description 53
- 230000006835 compression Effects 0.000 claims abstract description 11
- 238000007906 compression Methods 0.000 claims abstract description 11
- 238000006073 displacement reaction Methods 0.000 claims description 27
- 210000000988 bone and bone Anatomy 0.000 claims description 24
- 229910000831 Steel Inorganic materials 0.000 claims description 23
- 239000010959 steel Substances 0.000 claims description 23
- 239000000084 colloidal system Substances 0.000 claims description 9
- 210000002435 tendon Anatomy 0.000 claims 5
- 239000003365 glass fiber Substances 0.000 claims 1
- 230000002787 reinforcement Effects 0.000 claims 1
- 230000000452 restraining effect Effects 0.000 claims 1
- 125000006850 spacer group Chemical group 0.000 claims 1
- 239000000463 material Substances 0.000 description 27
- 210000003205 muscle Anatomy 0.000 description 27
- 238000004873 anchoring Methods 0.000 description 15
- 238000012669 compression test Methods 0.000 description 10
- 238000000034 method Methods 0.000 description 7
- 238000010586 diagram Methods 0.000 description 6
- 230000002093 peripheral effect Effects 0.000 description 5
- 238000005259 measurement Methods 0.000 description 4
- 238000007586 pull-out test Methods 0.000 description 3
- 229920002430 Fibre-reinforced plastic Polymers 0.000 description 2
- 230000008878 coupling Effects 0.000 description 2
- 238000010168 coupling process Methods 0.000 description 2
- 238000005859 coupling reaction Methods 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000011151 fibre-reinforced plastic Substances 0.000 description 2
- 239000011521 glass Substances 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000011160 research Methods 0.000 description 2
- 239000011435 rock Substances 0.000 description 2
- 238000004458 analytical method Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000002153 concerted effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000004069 differentiation Effects 0.000 description 1
- 239000013013 elastic material Substances 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 239000002689 soil Substances 0.000 description 1
- 239000011343 solid material Substances 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
- 230000001131 transforming effect Effects 0.000 description 1
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Abstract
本发明涉及一种用于三轴试验的被动式约束加载装置，该装置用于对立方体试件进行三轴试验，包括压缩试验机和加载平台，装置还包括置于压缩试验机和加载平台之间的加载框架和施力组件，施力组件通过加载框架与立方体试件连接，加载框架包括两个互相垂直连接的加载元件，加载元件由两个相对设置的加载端组成，四个加载端分别与立方体试件的四个周向面连接，加载平台分别与立方体试件的底部和加载端的底部连接，加载平台、立方体试件、加载框架和施力组件均对中置于压缩试验机加载空间内。与现有技术相比，本发明具有应用广度大等优点。
The invention relates to a passive restraint loading device for triaxial testing. The device is used for triaxial testing of cube specimens, and includes a compression testing machine and a loading platform. The device also includes a compression testing machine and a loading platform. The loading frame and the force-applying assembly are connected to the cube specimen through the loading frame. The loading frame includes two loading elements connected vertically to each other. The loading element is composed of two opposite loading ends. The four loading ends are connected to The four circumferential surfaces of the cube specimen are connected, and the loading platform is respectively connected to the bottom of the cube specimen and the bottom of the loading end, and the loading platform, cube specimen, loading frame and force application components are all centered in the loading space of the compression testing machine . Compared with the prior art, the invention has the advantages of wide application range and the like.
Description
Technical field
The present invention relates to engineering material test instrument field, especially relate to a kind of passive type for triaxial test constraint charger.
Background technology
Triaxial test is the research soil body, the test method that the architectural materials mechanics such as rock and concrete performance is important.Such material shows the mechanical characteristic be different under uniaxial stress environment under multiaxial stress environment.And in construction work, especially Mass Engineering, material is often in multi-dimensional stress state.The strength and deformation characteristic of material under multiaxial stress is of crucial importance to structural design.In addition, along with the development of computer technology, numerical evaluation becomes the important method analyzing Larger Engineering Projects, and wherein application is Finite Element Method the most widely, and the party's rule needs rational criterion of strength and constitutive relation.This just needs the experimental study by the strength and deformation performance of material under acquisition multi-axis stress state.
For the solid material such as rock and concrete, now existing hydraulic servo three-axis tester can simulate multidirectional (two axle/tri-axles) force environment both at home and abroad.At present, the load mode of such device mainly contains constant force and controls, and constant speed power controls, permanent Bit andits control and constant speed Bit andits control four kinds of load modes.The information of power and distortion is obtained by power-displacement sensing system and synchronous acquisition instrument.Such load mode is active, and namely the loading force of a direction can not form passive type with the displacement coupling in this direction and loads.This brings difficulty to the strength of materials under analysis passive type constraint environment and deformation characteristic.And such mechanical state is more and more common along with the development of reinforcing engineering, as column members such as Building Strengthened by FRP Sheets bridge piers.Owing to lacking corresponding passive type Triaxial tester, current research all carries out follow-up study based on the experimental study of active three-axis tester, but the method and concrete stress path correlativity are runed counter to.
Summary of the invention
Object of the present invention be exactly in order to overcome above-mentioned prior art exist defect and provide a kind of apply range large the passive type for triaxial test constraint charger.
Object of the present invention can be achieved through the following technical solutions:
A kind of constraint of the passive type for triaxial test charger, this device is used for carrying out triaxial test to cube specimen, comprise compression test and weighted platform, described device also comprises the loading frame and the assembly that exerts a force that are placed between compression test and weighted platform, described force assembly is connected with cube specimen by loading frame, described loading frame comprises the loading element of two orthogonal connections, described loading element is made up of the loading end that two are oppositely arranged, described four loading ends are connected with four circumferential surfaces of cube specimen respectively, described weighted platform contacts with the bottom of loading end with the bottom of cube specimen respectively, described weighted platform, cube specimen, loading frame and the equal centering of force assembly are placed in described compression test and load in space,
Compression test applies axle pressure to cube specimen, and cube specimen produces circumferential deformation under axial compression effect, and this circumferential deformation excites force assembly to produce peripheral force, and this peripheral force is applied on four circumferential surfaces of cube specimen by loading frame.
Described force assembly comprises two mutually perpendicular forcing unit, and described two forcing unit are corresponding with two loading elements respectively to be connected.
Described forcing unit is made up of many constraining rods parallel to each other, and two loading ends of described loading element are provided with for the preformed hole by constraining rod, and described constraining rod is through this preformed hole and be connected with described two loading ends.
Described loading end comprises interconnective web joint and loads panel, and described preformed hole is located on web joint, and described loading panel contacts with cube specimen circumferential surface, and described web joint is connected with constraining rod.
Leave space between described loading end and cube specimen, between described loading end and cube specimen and cube specimen upper and lower surface be equipped with antifriction mat material, be provided with antifriction mat material between described loading end and weighted platform.
Described constraining rod is made up of muscles and bones and the anchoring body that is located at muscles and bones two ends, and described muscles and bones is connected with loading end by anchoring body.
Described anchoring body is connected with loading end by nut, is provided with steel cushion block between described nut and loading end, and described steel cushion block is made up of the semi-circular ring of two various outer diameters.
Described muscles and bones is glass fiber-reinforced polymer material, and described anchoring body comprises steel sleeve and bonding colloid, and described steel sleeve inside surface is connected with muscles and bones by bonding colloid, and outside surface is connected with nut.
Described device also comprises displacement measurement assembly, and described displacement measurement assembly comprises Acquisition Instrument and two displacement units, and described two displacement units are corresponding with two loading elements respectively to be connected, and described two displacement units are also all connected with Acquisition Instrument.
Institute's displacement unit is made up of two displacement meters, and described two displacement meters are connected with the two ends of loading element respectively.
Compared with prior art, the present invention has the following advantages:
1) passive type loads the stress path that can enrich triaxial test, expands the application range of triaxial test.
2) difference of muscle material can realize the rapport of confined pressure and distortion, and namely peripheral force and respective direction displacement meet the coupled relation of multiple line sex ratio.
3) the selection difference of different directions muscle material can realize the independence of side direction two principal directions of stress, and namely two-way linear relationship is separate.
4) test unit is simple, without the need to manufacturing three-axis tester, can test on general pressure testing machine.
Accompanying drawing explanation
Fig. 1 is planimetric map of the present invention;
Fig. 2 is the A-A cut-open view of Fig. 1;
Fig. 3 is constraining rod structural representation;
Fig. 4 is the main apparent size schematic diagram of left and right directions loading end in embodiment;
Fig. 5 is the side-looking scale diagrams of left and right directions loading end in embodiment;
Fig. 6 be in embodiment left and right directions loading end overlook scale diagrams;
Fig. 7 is the main apparent size schematic diagram of fore-and-aft direction loading end in embodiment;
Fig. 8 is the side-looking scale diagrams of fore-and-aft direction loading end in embodiment;
Fig. 9 be in embodiment fore-and-aft direction loading end overlook scale diagrams;
Wherein: 1, compression test, 2, weighted platform, 3, cube specimen, 4, displacement meter, 5, constraining rod, 6, loading end, 51, muscles and bones, 52, steel sleeve, 53, nut, 54, steel cushion block, 55, bond colloid, and 61, wing plate, 62, web joint, 63, load panel.
Embodiment
Below in conjunction with the drawings and specific embodiments, the present invention is described in detail.The present embodiment is implemented premised on technical solution of the present invention, give detailed embodiment and concrete operating process, but protection scope of the present invention is not limited to following embodiment.
A kind of constraint of the passive type for triaxial test charger, this device is used for carrying out triaxial test to cube specimen 3, as depicted in figs. 1 and 2, comprise compression test 1, weighted platform 2 and the loading frame be placed between compression test 1 and weighted platform 2 and the assembly that exerts a force, force assembly is connected with cube specimen 3 by loading frame, loading frame comprises the loading element of two orthogonal connections, loading element is made up of two loading ends be oppositely arranged 6, four loading ends 6 are connected with four circumferential surfaces of cube specimen 3 respectively, weighted platform 2 is connected with the bottom of cube specimen 3 and the bottom of loading end respectively, weighted platform 2, cube specimen 3, loading frame and the equal centering of force assembly are placed in compression test 1 and load in space, in the present embodiment cube specimen 3 for the length of side be the concrete test block of 100 millimeters,
Compression test 1 pair of cube specimen 3 applies axle pressure, cube specimen 3 produces circumferential deformation under axial compression effect, this circumferential deformation excites force assembly to produce peripheral force, and this peripheral force is applied on four circumferential surfaces of cube specimen 3 by loading frame.
Force assembly comprises two mutually perpendicular forcing unit, and two forcing unit are corresponding with two loading elements respectively to be connected.
Each forcing unit is made up of 4 constraining rods 5 parallel to each other, two loading ends 6 of loading element is equipped with for 4 preformed holes by constraining rod 5, and 4 constraining rods 5 are through 4 preformed holes and be connected with two loading ends 6.
Loading end 6 comprises interconnective web joint 62 and loads panel 63, preformed hole is located on web joint 62, load panel 63 to contact with cube specimen 3 circumferential surface, web joint 62 is connected with constraining rod 5, in the present embodiment, loading end 6 is steel, loading end 6 also comprises two blocks of wing plates 61, and web joint 62 is connected by two pieces of wings 61 with loading panel 63.
Space is left between loading end 6 and cube specimen 3, six faces of cube specimen 3 are equipped with antifriction mat material, antifriction mat material is provided with between described loading end 6 and weighted platform 2 lower shoe, wherein, antifriction mat material is for avoiding because the end restraint of interfacial friction formation is on the impact of test material intensity.
As shown in Figure 3, constraining rod 5 is made up of muscles and bones 51 and the anchoring body that is located at muscles and bones 51 two ends, and muscles and bones 51 is connected with loading end 6 by anchoring body.
As shown in Figure 3, anchoring body is connected with loading end 6 by nut, steel cushion block 54 is provided with between nut and loading end 6, steel cushion block 54 is made up of the semi-circular ring of two various outer diameters, be convenient to knock removal, the internal diameter of two semi-circular ring is identical, in the present embodiment, the semi-circular ring overall diameter of top is 110 millimeters, and the overall diameter of the semi-circular ring of below is 80 millimeters, and interior diameter is 35 millimeters, as shown in Figure 2, only the constraining rod 5 of top is provided with steel cushion block 54 with the junction of web joint 62, and in order to save material further, constraining rod 5 two ends only one end are provided with steel cushion block 54.
Anchoring body is connected with loading end by nut, is provided with steel cushion block between nut and loading end, and steel cushion block is made up of the semi-circular ring of two various outer diameters.
Muscles and bones 51 is glass fiber-reinforced polymer material, anchoring body comprises steel sleeve 52 and bonding colloid 55, and steel sleeve 52 inside surface is connected with muscles and bones 51 by bonding colloid 55, and outside surface is connected with nut 53, in the present embodiment, steel sleeve 52 adopts internal and external threads, and internal thread is for the snap-in force strengthened and bond between colloid 55, and external thread is used for being connected with nut 53, bonding colloid 55 material is epoxy resin, the overall diameter of nut 53 is 50 millimeters, and the overall diameter of steel sleeve 52 is 33 millimeters, and interior diameter is 30 millimeters.
As shown in Figure 1, device also comprises displacement measurement assembly, and displacement measurement assembly comprises Acquisition Instrument and two displacement units, and two displacement units are corresponding with two loading elements respectively to be connected, and two displacement units are also all connected with Acquisition Instrument.
Wherein, the dimension information of two loading elements can be different, in the present embodiment, concrete dimension information is as shown in Fig. 4 to Fig. 9, in Fig. 1, the web joint 62 of left and right directions loading end 6 is of a size of 250 millimeters × 200 millimeters, in Fig. 1, the web joint 62 of above-below direction (i.e. actual fore-and-aft direction) loading end 6 is of a size of 200 millimeters × 200 millimeters, wherein load the measure-alike of panel 63, be 95 millimeters × 95 millimeters.
The use procedure of the passive type constraint charger of this triaxial test is specific as follows:
1) make cube specimen 3, mark the axial compression face that circumferential stress surface corresponding to differentiation about four is corresponding with about two.District is laid in test block test cube being positioned over charger, namely on weighted platform 2;
2) install circumferential loading frame and force assembly, force direction is respectively perpendicular to cubical circumferential stress surface;
The installation of loading frame and force assembly only can install a pair, and it is two right also can to install, and the process of installing a pair is as follows:
By a loading element, namely two loading ends 6 are placed in weighted platform respectively relatively, by four preformed holes of constraining rod 5 through web joint 62, fixing position makes the free segment center of constraining rod 5 and loading center at same straight line, line is in loading surface normal orientation, be screwed into bolt by anchoring body again, now cube specimen 3 is only provided with antifriction mat material in four surfaces, the surface being respectively upper and lower surface and contacting with loading end 6.
Two right processes of installing are as follows:
First by a loading element, namely two loading ends 6 are placed in weighted platform relatively, by constraining rod 5 four preformed holes through web joint 62, fix position and make the free segment center of constraining rod 5 and loading center at same straight line, line is in loading surface normal orientation, then is screwed into bolt by anchoring body; Again by another one loading element, namely two other loading end 6 is satisfied with first and is placed on loading bench to perpendicular direction, by four preformed holes of constraining rod 5 through steel plate, fixing position makes the free segment of constraining rod 5 be in loading center, be screwed into bolt by anchoring body again, now cube specimen 3 six surfaces are equipped with antifriction mat material;
Between the nut being positioned on the upside of loading end 6 two constraining rod 5 sides and loading end 6, add the steel cushion block 54 being convenient to device unloading, tighten the end nut of all constraining rods 5;
3) installation displacement meter 4 and foil gauge are in charger, test cube test specimen 3 axial deformation respectively, the distortion of circumferential deformation and charger self;
4) Acquisition Instrument is connected, by the Information Monitoring synchronization of power and distortion;
5) start compression test 1, the active carrying out axial force by controlling axial displacement rate of deformation loads, and records power and each data to distortion simultaneously;
6) when circumferential deformation reaches the limit values or cube specimen 3 destruction can not continuing loading occurs, off-test.
The material that above-mentioned force assembly adopts is linear elastic material, and this system need carry out pull-out test before the test, obtains the scale factor K=Δ F/ Δ L of power increment and incremental deformation.This factor changes by the elastic modulus of muscles and bones and physical dimension.
The connection of above-mentioned force assembly and loading frame is anchor connection, and its anchor force need meet with slippage linear, and linear factor is much smaller than scale factor K.
The distortion equity of muscle material and anchoring system thereof in the circumferential deformation of cube specimen 3 and respective direction, specifically such as formula shown in (1-1):
ε
iL
c＝ε
rL
r+2s (1-1)
Wherein: L
cfor the test block length of side (mm), ε
ifor a certain principal strain of test block side direction.ε
rfor muscles and bones elastic strain, L
rfor the drift (this apparatus design length is 200mm) of muscles and bones, s is muscles and bones slippage (mm) in anchoring body.
Cohesive force and muscles and bones pulling force mutually balance set up muscles and bones slippage and muscles and bones elastic strain mutual relationship such as formula shown in (1-2):
Ks＝E
rε
rA
r(1-2)
Wherein: K is muscles and bones drawing rigidity (unit N/mm), E
rfor the elastic modulus (units MPa) of muscle material.Two parameter records by being with the muscle material pull-out test of anchoring piece, A
rfor muscle material sectional area (unit mm
2).
Simultaneous formula (1-1) and (1-2) can set up the transforming relationship of muscles and bones strain and concrete strain, shown in (1-3):
This passive loading system finally acts on making a concerted effort such as formula shown in (1-4) on a certain principal direction of stress of concrete test block:
Wherein: n
rfor certain confined pressure direction muscle material radical, i.e. the radical of constraining rod 5 in a loading element.
Its loading speed ρ
ican be calculated by formula (1-5):
Wherein: f '
cfor concrete test cube uniaxial compressive strength.
Namely the linear coupling of distortion and load is met.And the pull-out test of the assembly that actual loaded speed combines with constraining rod 5 by two pairs of loading ends 6 records.
Claims (10)
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Cited By (6)
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| CN104792609A (en) * | 2015-04-29 | 2015-07-22 | 中国矿业大学 | Lateral restraint system for compression test of platy rock sample and test method thereof |
| CN105486604A (en) * | 2015-12-11 | 2016-04-13 | 中国飞机强度研究所 | Calibration conversion device for loading frame of combined loading complete equipment |
| CN107764636A (en) * | 2017-10-23 | 2018-03-06 | 中国矿业大学 | A kind of deformation measuring device and method of cuboid rock sample conventional triaxial compression test |
| CN107941615A (en) * | 2017-12-21 | 2018-04-20 | 四川德翔科创仪器有限公司 | A kind of three-axis tester and pilot system |
| CN110514523A (en) * | 2019-08-29 | 2019-11-29 | 广东工业大学 | A stress loading combination device |
| CN110646343A (en) * | 2019-09-03 | 2020-01-03 | 山东大学 | A device and method for testing the pullout force of an anchor rod specimen with adjustable confining pressure |
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Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104792609A (en) * | 2015-04-29 | 2015-07-22 | 中国矿业大学 | Lateral restraint system for compression test of platy rock sample and test method thereof |
| CN105486604A (en) * | 2015-12-11 | 2016-04-13 | 中国飞机强度研究所 | Calibration conversion device for loading frame of combined loading complete equipment |
| CN105486604B (en) * | 2015-12-11 | 2018-04-13 | 中国飞机强度研究所 | A kind of calibration conversion equipment for Combined Loading complete set of equipments load frame |
| CN107764636A (en) * | 2017-10-23 | 2018-03-06 | 中国矿业大学 | A kind of deformation measuring device and method of cuboid rock sample conventional triaxial compression test |
| CN107764636B (en) * | 2017-10-23 | 2019-04-19 | 中国矿业大学 | Deformation measuring device and method for conventional triaxial compression test of cuboid rock sample |
| CN107941615A (en) * | 2017-12-21 | 2018-04-20 | 四川德翔科创仪器有限公司 | A kind of three-axis tester and pilot system |
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| CN110514523A (en) * | 2019-08-29 | 2019-11-29 | 广东工业大学 | A stress loading combination device |
| CN110514523B (en) * | 2019-08-29 | 2024-09-24 | 广东工业大学 | Stress loading combined device |
| CN110646343A (en) * | 2019-09-03 | 2020-01-03 | 山东大学 | A device and method for testing the pullout force of an anchor rod specimen with adjustable confining pressure |
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|---|---|
| CN104344997B (en) | 2017-01-11 |
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