CN104913975B - Biaxial tension test testpieces of ribbon matrix fibre bundle and preparation method thereof - Google Patents
Biaxial tension test testpieces of ribbon matrix fibre bundle and preparation method thereof Download PDFInfo
- Publication number
- CN104913975B CN104913975B CN201510266712.2A CN201510266712A CN104913975B CN 104913975 B CN104913975 B CN 104913975B CN 201510266712 A CN201510266712 A CN 201510266712A CN 104913975 B CN104913975 B CN 104913975B
- Authority
- CN
- China
- Prior art keywords
- fibre bundle
- ribbon matrix
- biaxial tension
- drag reduction
- test
- 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.)
- Active
Links
- 239000000835 fiber Substances 0.000 title claims abstract description 80
- 238000012360 testing method Methods 0.000 title claims abstract description 61
- 239000011159 matrix material Substances 0.000 title claims abstract description 41
- 238000002360 preparation method Methods 0.000 title claims description 8
- 238000011068 loading method Methods 0.000 claims abstract description 31
- 239000004744 fabric Substances 0.000 claims abstract description 11
- 238000000151 deposition Methods 0.000 claims abstract description 6
- 238000009954 braiding Methods 0.000 claims abstract description 3
- 239000003292 glue Substances 0.000 claims description 4
- 238000012545 processing Methods 0.000 claims description 3
- 238000000605 extraction Methods 0.000 claims description 2
- 238000002474 experimental method Methods 0.000 description 12
- 239000002131 composite material Substances 0.000 description 9
- 238000000034 method Methods 0.000 description 9
- 238000007906 compression Methods 0.000 description 8
- 239000000463 material Substances 0.000 description 8
- 230000006835 compression Effects 0.000 description 7
- 229920000049 Carbon (fiber) Polymers 0.000 description 2
- 238000005452 bending Methods 0.000 description 2
- 238000004364 calculation method Methods 0.000 description 2
- 239000004917 carbon fiber Substances 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 238000010998 test method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000002657 fibrous material Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
Landscapes
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
Abstract
The invention discloses the biaxial tension test testpieces of ribbon matrix fibre bundle, including strip sample, wherein：Strip sample is made up of fiber cloth depositing base, strip sample center section is test department, two ends are clamping part, there was only warp fiber in test department, and warp fiber is along strip specimen width direction period profile, clamping part is braiding structure, and the two sides of the compressed load loading of test department are fixed with drag reduction rubber, the length of drag reduction rubber is identical with test department length, and compressive load loading head is fixed with the outside of drag reduction rubber.The present invention has the advantages that making is simple, experimental cost is low, testpieces quality is good, be not susceptible to Compressional buckling.
Description
Technical field
The present invention relates to Compound Material Engineering testing field, and in particular to the biaxial tension test testpieces of ribbon matrix fibre bundle and
Its preparation method.
Background technology
Ribbon matrix fibre bundle is the main load-carrying construction in composite.Research shows the macromechanics behavior of composite
And the mechanical property of thin sight failure procedure and ribbon matrix fibre bundle is closely related.In recent years, with the multiple dimensioned meter of composite
The rise of calculation method, using ribbon matrix fibre bundle as small composite so that the mechanical property to composite is furtherd investigate
Method turn into composite Multi-Scale Calculation field in popular problem.Ribbon matrix fibre bundle is typically in the composite
Multiaxis coupling stress state, wherein one of common stress state is tension and compression stress state, therefore it is real only to carry out biaxial tension test
The mechanical property of ribbon matrix fibre bundle could be furtherd investigate by testing.
At present, the stretching for tow material is primarily present in the prior art（Chinese patent CN101949797B, one
Kind of testing micro-tensile mechanical properties of metal fiber method and device, Chinese patent CN102426135B, a kind of carbon fiber multifilament and
Carbon fiber cable extension test fixture auxiliary tool）, compression（Chinese patent CN100561176C, fibrous material transverse compression
The measuring method and device of performance, Chinese patent CN101650282B, the measuring method and dress of a kind of monofilament fiber compression performance
Put）Etc. test method, the report for tow material biaxial tension test test method is had no.Because ribbon matrix tow material exists
It is less bar-shaped for diameter in form, therefore be difficult that biaxial tension test experiment directly is carried out to ribbon matrix fibre bundle.
For non-fiber strand material, biaxial tension test experimental method typically uses cross biaxial tension test sample（It is Chinese special
Sharp CN103267672B,《A kind of twin shaft plate tension and compression CYCLIC LOADING tests anti-bending system and method》）, square tabular twin shaft draws
Press sample（Chinese patent CN104316393A,《Loading device and method for material biaxial tension-compression strength》）Or square block
Shape biaxial tension test sample（Chinese patent CN201955268U,《A kind of loading test device of concrete biaxial tension and compression》）.Cross
Shape biaxial tension test sample generally requires additional anti-Compressional buckling device（Chinese patent CN103267672B,《A kind of twin shaft plate is drawn
CYCLIC LOADING is pressed to test anti-bending system and method》）Prevent sample from unstability occurring under compressive loading.Square tabular biaxial tension test
Specimen size is big, and the material consumed in experiment is more, adds the cost of batch experiment.Square bulk biaxial tension test sample is used
The mode of splicing transmits axial tensile loads, can not effectively add for the higher fibre reinforced composites this method of tensile strength
Carry.Therefore, it is difficult to carry out ribbon matrix fibre bundle biaxial tension test experiment by prior art.
The content of the invention
The technical problems to be solved by the invention are to be directed to the above-mentioned state of the art, and supply one kind to make simple, experimental cost
It is low, testpieces quality is good, the biaxial tension test testpieces that is not susceptible to Compressional buckling and preparation method thereof.
The present invention solve the technical scheme that is used of above-mentioned technical problem for：
The biaxial tension test testpieces of ribbon matrix fibre bundle, including strip sample, wherein：Strip sample is sunk by fiber cloth
Product matrix is constituted, and strip sample center section is test department, and two ends are there was only warp fiber in clamping part, test department, and
Warp fiber is along strip specimen width direction period profile, and clamping part is braiding structure, the compressed load loading of test department
Two sides are fixed with drag reduction rubber, and the length of drag reduction rubber is identical with test department length, and compression is fixed with the outside of drag reduction rubber
Load loading head.
For optimization above-mentioned technical proposal, the concrete measure taken also includes：
Drag reduction rubber is adhesively fixed by glue with test department.
Compressive load loading head is fixed by glue with drag reduction rubber bound.
The thickness of drag reduction rubber is identical with test department thickness.
Compressive load loading head is T-shaped load loading head.
A kind of preparation method of the biaxial tension test testpieces of ribbon matrix fibre bundle, comprises the following steps：
Step 1: preparing the individual layer precast body of ribbon matrix fibre bundle：By the weft fiber of control of two-dimensional braided fiber cloth interlude
Extract out, leave behind warp fiber；It can not upset the periodicity of warp fiber when extracting weft fiber；
Step 2: getting up and being fixed on mould the fiber cloth through-thickness obtained in step one stacking, sink repeatedly
Product matrix obtains ribbon matrix fibre bundle flat board；
Step 3: the ribbon matrix fibre bundle flat board after processing depositing base obtains strip sample；
Step 4: drag reduction rubber is fixed in the middle of the strip sample at the compressive load loading of test department both sides；
Step 5: fixing the biaxial tension test experiment that compressive load loading head obtains ribbon matrix fibre bundle in drag reduction rubber outer side
Part.
Compared with prior art, biaxial tension test testpieces of ribbon matrix fibre bundle of the invention and preparation method thereof, beneficial
Effect is：
(1) present invention can realize the biaxial tension test experiment of ribbon matrix fibre bundle.Elongated straps matrix fiber beam twin shaft is drawn
Pressure sample more saves experiment material than cross biaxial tension test sample and square tabular biaxial tension test sample, reduces and criticizes
Measure the cost of experiment.
(2) size of the elongated straps matrix fiber beam biaxial tension test sample that the present invention is used in compressive load action direction
It is small, therefore unstability will not occur for sample without the anti-Compressional buckling device of additional sample under compressive load effect, simplify
Compressive load loading device, improves the reliability of experiment.
(3) the drag reduction rubber that the present invention is used can reduce the axial resistance between sample and compressive load loading head, because
The measurement result of this axial load is more accurate.
Brief description of the drawings
Fig. 1 is the fiber cloth schematic diagram for not extracting weft fiber；
Fig. 2 is the fiber cloth schematic diagram after extraction weft fiber；
Fig. 3 is strip sample；
Fig. 4 is ribbon matrix fibre bundle biaxial tension test sample（Arrow represents loading direction in figure）；
Fig. 5 is the flow chart that periodicity principle of the present invention prepares sample.
In figure：1- warp fibers, 2- weft fibers, 3- strips sample, at 3-1- compressive load loadings, 3-2- axially draws
Stretch load loading end, 4- compressive loads loading head, 5- drag reduction rubber.
Embodiment
Embodiments of the invention are described in further detail below in conjunction with the accompanying drawings.
The preparation method of the biaxial tension test testpieces of ribbon matrix fibre bundle of the present invention, comprises the following steps：
Step 1: preparing the individual layer precast body of ribbon matrix fibre bundle using periodicity principle.In order to ensure tape base in sample
The form of body fibre bundle is consistent with the form in true composite, by control of two-dimensional braided fiber cloth（Fig. 1）The broadwise of interlude is fine
Dimension 2 is extracted out, leaves behind warp fiber 1, should not upset the periodicity of warp fiber during extracting weft fiber；
Step 2: by the fiber cloth obtained in step one（Fig. 2）Through-thickness stacking is got up and is fixed on mould, instead
Multiple depositing base obtains ribbon matrix fibre bundle flat board；
Step 3: the ribbon matrix fibre bundle flat board after processing depositing base obtains strip sample 3；
Step 4: 3-1 symmetrically pastes drag reduction rubber at the compressive load loading of the middle test department both sides of strip sample 3
5；
Step 5: pasting the twin shaft drawing that T-shaped compressive load loading head 4 obtains ribbon matrix fibre bundle in the outside of drag reduction rubber 5
Press testpieces（Fig. 4）；
During experiment, applying pressure at compressive load loading at 3-1, pulling force applied in axial tensile loads loading end 3-2,
Realize and the biaxial tension test of test department is tested.
It is noted that in the experiment of ribbon matrix fibre bundle, the fibre bundle of testpieces tensile load action direction is determined
Justice is warp fiber, and fibre bundle normal thereto is weft fiber.
Described above is only the preferred embodiment of the present invention, it is noted that for the ordinary skill people of the art
For member, some improvement can also be made under the premise without departing from the principles of the invention, and these improvement also should be regarded as the present invention's
Protection domain.
Claims (6)
1. the biaxial tension test testpieces of ribbon matrix fibre bundle, including strip sample (3), it is characterized in that：Described strip examination
Sample (3) is made up of the control of two-dimensional braided fiber cloth depositing base after extraction interlude weft fiber, in described strip sample (3)
Between be partly test department, two ends are clamping part, only warp fiber (1) in test department, and warp fiber (1) is tried along strip
Sample (3) width period profile, clamping part is braiding structure, and the two sides of the compressed load loading of described test department are fixed
There is drag reduction rubber (5), the length of described drag reduction rubber (5) is identical with test department length, the outside of described drag reduction rubber (5)
It is fixed with compressive load loading head (4).
2. the biaxial tension test testpieces of ribbon matrix fibre bundle according to claim 1, it is characterized in that：Described drag reduction rubber
(5) it is adhesively fixed by glue with test department.
3. the biaxial tension test testpieces of ribbon matrix fibre bundle according to claim 1, it is characterized in that：Described compressive load
Loading head (4) is adhesively fixed by glue with drag reduction rubber (5).
4. the biaxial tension test testpieces of ribbon matrix fibre bundle according to claim 1, it is characterized in that：Described drag reduction rubber
(5) thickness is identical with test department thickness.
5. the biaxial tension test testpieces of ribbon matrix fibre bundle according to claim 1, it is characterized in that：Described compressive load
Loading head (4) is T-shaped load loading head.
6. a kind of preparation method of the biaxial tension test testpieces of ribbon matrix fibre bundle, it is characterized in that：Comprise the following steps：
Step 1: preparing the individual layer precast body of ribbon matrix fibre bundle：The weft fiber (2) of control of two-dimensional braided fiber cloth interlude is taken out
Go out, leave behind warp fiber (1)；The periodicity of warp fiber (1) can not be upset when extracting weft fiber (2)；
Step 2: getting up and being fixed on mould the fiber cloth through-thickness obtained in step one stacking, base is deposited repeatedly
Body obtains ribbon matrix fibre bundle flat board；
Step 3: the ribbon matrix fibre bundle flat board after processing depositing base obtains strip sample (3)；
Step 4: fixing drag reduction rubber (5) at the compressive load loading of the middle test department both sides of strip sample (3)；
Step 5: fixed compressive load loading head (4) obtains the biaxial tension test examination of ribbon matrix fibre bundle on the outside of drag reduction rubber (5)
Test part.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510266712.2A CN104913975B (en) | 2015-05-22 | 2015-05-22 | Biaxial tension test testpieces of ribbon matrix fibre bundle and preparation method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510266712.2A CN104913975B (en) | 2015-05-22 | 2015-05-22 | Biaxial tension test testpieces of ribbon matrix fibre bundle and preparation method thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104913975A CN104913975A (en) | 2015-09-16 |
| CN104913975B true CN104913975B (en) | 2017-08-01 |
Family
ID=54083231
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510266712.2A Active CN104913975B (en) | 2015-05-22 | 2015-05-22 | Biaxial tension test testpieces of ribbon matrix fibre bundle and preparation method thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104913975B (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110108567B (en) * | 2019-06-25 | 2020-06-16 | 南京航空航天大学 | Ceramic matrix composite interlaminar tensile test piece, and preparation method and test method thereof |
| CN111272650A (en) * | 2020-03-02 | 2020-06-12 | 广西师范大学 | Joint for testing failure criterion of composite material bonding structure |
| CN111855398B (en) * | 2020-06-09 | 2021-06-29 | 北京航空航天大学 | Biaxial stress state test piece is realized in unipolar loading of face of cylinder working section |
| CN113092207B (en) * | 2021-04-02 | 2022-09-27 | 凯尔测控试验系统（天津）有限公司 | Method for manufacturing conductive adhesive film sample for in-plane biaxial tensile property test |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3765996A (en) * | 1972-04-03 | 1973-10-16 | Whittaker Corp | Unidirectional tensile test specimen incorporating integrated load pads |
| CN2090321U (en) * | 1991-03-08 | 1991-12-11 | 林和国 | Metal and glass fibre reinforced plastics composite plate |
| DE19626921A1 (en) * | 1996-07-04 | 1998-01-08 | Dornier Gmbh | CFRP release laminate |
| JP3918011B2 (en) * | 2003-12-30 | 2007-05-23 | サムヤン コーポレイション | Method for producing geogrid made of fiber reinforced polymer strip |
| JP2010014612A (en) * | 2008-07-04 | 2010-01-21 | Mitsubishi Materials Corp | Two axes tensile testing device |
| CN201955268U (en) * | 2010-11-24 | 2011-08-31 | 大连民族学院 | Concrete biaxial tension and pressure loading test device |
| CN103592218B (en) * | 2013-11-12 | 2016-05-04 | 哈尔滨工程大学 | The integrated drag reduction testing arrangement of elastomer rubber sealing ring drag reduction testing arrangement and elastomer rubber sealing ring/non-smooth surface |
| CN104122202B (en) * | 2014-07-29 | 2017-05-03 | 厦门大学 | Method for testing interfacial bonding strength of ceramic fiber-reinforced resin matrix composite material |
| CN104230368B (en) * | 2014-09-26 | 2016-01-20 | 辽宁奥亿达新材料有限公司 | Asphalt base carbon fiber non-woven mat warming plate and manufacture method thereof |
| CN204202955U (en) * | 2014-09-30 | 2015-03-11 | 中国矿业大学 | Be applicable to the biaxial stretch-formed test specimen of coated fabric film material |
-
2015
- 2015-05-22 CN CN201510266712.2A patent/CN104913975B/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN104913975A (en) | 2015-09-16 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104913975B (en) | Biaxial tension test testpieces of ribbon matrix fibre bundle and preparation method thereof | |
| Gao et al. | Damage accumulation in woven-fabric CFRP laminates under tensile loading: Part 1. Observations of damage accumulation | |
| Zhang et al. | Progressive damage analysis of three-dimensional braided composites under flexural load by micro-CT and acoustic emission | |
| Pankow et al. | Split Hopkinson pressure bar testing of 3D woven composites | |
| Moothoo et al. | A study of the tensile behaviour of flax tows and their potential for composite processing | |
| Bru et al. | Use of the Iosipescu test for the identification of shear damage evolution laws of an orthotropic composite | |
| Shokrieh et al. | Investigating the transverse behavior of Glass–Epoxy composites under intermediate strain rates | |
| Ramakrishna et al. | Tensile behaviour of knitted carbon-fibre-fabric/epoxy laminates—part I: Experimental | |
| Rigaud et al. | Characterization of bending and tensile behavior of ultra-high performance concrete containing glass fibers | |
| CN106404543A (en) | Prestressed carbon fiber plate anchor test device | |
| Hao et al. | Study on the torsion behavior of 3-D braided composite shafts | |
| CN106483016A (en) | A kind of concrete sample uniaxial tension Complete stress-strain curve experimental rig | |
| Arteiro et al. | Effect of tow thickness on the structural response of aerospace-grade spread-tow fabrics | |
| CN103471938B (en) | T-shaped Hopkinson torsion bar device | |
| Qi et al. | Research on carbon fiber/epoxy interfacial bonding characterization of transverse fiber bundle composites fabricated by different preparation processes: Effect of fiber volume fraction | |
| CN103883076A (en) | Intelligent hybrid composite FRP (Fiber Reinforce Plastic) prestressed reinforcement based on piezoelectric ceramic and preparation method of intelligent hybrid composite FRP prestressed reinforcement | |
| Catangiu et al. | Experimental results for bending fatigue behaviour of glass-epoxy composite materials | |
| Deng et al. | Assessment of interfacial bonding between polymer threads and epoxy resin by transverse fibre bundle (TFB) tests | |
| Yin et al. | Comparative study on piezoresistive properties of CFRP tendons prepared by two different methods | |
| CN203479614U (en) | Split Hopkinson torsion bar test piece clamp device | |
| Baets et al. | Determination of the optimal flax fibre preparation for use in UD-epoxy composites | |
| Hucker et al. | Investigation into the behaviour of hollow glass fibre bundles under compressive loading | |
| CN111551434A (en) | Method for testing axial compression performance of carbon fiber composite material and constitutive model | |
| CN207472674U (en) | A kind of axis pulling experiment device of web or pieces of cloth | |
| Figeys et al. | A new composite for external reinforcement: Steel cord reinforced polymer |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |