CN104132845A - Test method for measuring stress intensity factor at cutting-angle part of anisotropic material - Google Patents

Test method for measuring stress intensity factor at cutting-angle part of anisotropic material Download PDF

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CN104132845A
CN104132845A CN201410308765.1A CN201410308765A CN104132845A CN 104132845 A CN104132845 A CN 104132845A CN 201410308765 A CN201410308765 A CN 201410308765A CN 104132845 A CN104132845 A CN 104132845A
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test
stress intensity
intensity factor
bight
otch
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CN201410308765.1A
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平学成
吴卫星
李烽
朱增辉
王清
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East China Jiaotong University
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East China Jiaotong University
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Abstract

The invention discloses a test method for measuring stress intensity factor at a cutting-angle part of an anisotropic material. A test piece is a disc consisting of two sectorial wedge-body test pieces, and the two wedge bodies are made of different materials. The cutting angel part is at the center of the disc. By taking the disc as the test piece, the test piece is subjected to single-shaft compression test, a compressive load at an arbitrary diameter direction is applied to the circumferential outer edge of the test piece for measuring the stress intensity factor at the cutting-angle part, and a load applied when the cutting-angle part is damaged is taken as the critical load. According to the test method, the disc test piece is subjected to single-shaft compression test for measuring the stress intensity factor at the cutting-angle part of the anisotropic composite material, the method is reliable in principle, uniform in loading force, high in measuring precision and accurate and recorded data and analyzed results, and is especially applicable to measure the stress intensity factor at the cutting-angle part of a composite material integrating an anisotropic composite material and an isotropic material.

Description

A kind of test method of measuring anisotropic material otch bight stress intensity factor
Technical field
The present invention relates to a kind of test method, relate in particular to a kind of test method of measuring anisotropic composite material otch bight stress intensity factor.
Background technology
Along with the commercial Application of the advanced materials such as types of functionality material, compound substance, bond material increases gradually, the interface mechanical behavior being comprised of different materials is more and more subject to people's attention.The joint portion of various types of materials and structure, as metal, being combined the combination interface etc. of interface, function element and bearing carrier with Ceramic bond interface, dissimilar metal has very important impact to the mechanical behavior of material or structural entity.Compound substance is when bearing external load, existence due to the Stress singularity in combination interface otch bight, tend to from otch bight cumulative damage, and then form the destruction that defects i.e.cracks causes compound substance, because material is concentrated in conjunction with easily having defect near interface or producing stress, thus bond material easily junction or near first destroy.
The test specimen type that has at present multiple measurement compound substance stress intensity factor, the most frequently used have asymmetric three point bending specimen, monolateral otch four-point bending test specimen, asymmetric four-point bending test specimen, disk test specimen, a limit crackle bar shaped test specimen etc.Method of testing also has a variety of, is exactly typically three point bending test.The method that represents material fracture toughness has generalized intensity factors, crack extension energy rate and J integration etc.The method of these tests has a lot of stress intensity factors that are applicable to measuring the isotropic material with stress symmetric field, but because the stress field right and wrong in anisotropic composite material otch bight are symmetric, during material damage, angle is uncertain, and it is very necessary therefore inventing a kind of test method of measuring the stress intensity factor in anisotropic composite material otch bight.
Due to the difficulty of clamping sample, and fixture clamping place easily produces stress and concentrates, and makes test specimen produce in advance destroying infection test findings.In order to solve such problem, relatively extensively adopting at present the sample of measuring material stress intensity factor is disk test specimen, and its principle is testing machine diameter in the diametric(al) of disk sample load of exerting pressure, and sample is destroyed along loading diameter.Adopt disk test specimen, and on sample, increase a pair of platform for loading parallel to each other, this is conducive to sample from center crack initiation, can avoid again concentrated force in the adverse effect of part, contact position.Therefore can utilize disk sample, from the feature of center crack initiation, measure anisotropic composite material otch bight stress intensity factor.But because disk test specimen is isotropic material, and as a whole test specimen, therefore also need disk test specimen to improve in order to measure anisotropic composite material otch bight stress intensity factor.
Summary of the invention
The object of this invention is to provide a kind of test method of measuring anisotropic material otch bight stress intensity factor.The method is the method based on disc test and makes improvements.
Of the present invention a kind of for measuring the test specimen of anisotropic composite material otch bight stress intensity factor, comprise the disk jointly being formed by material 1 and the tight wedge shape combination of material 2, wherein material 2 accounts for 1/4th of disk, and the key groove of material 2 is 90o, and the key groove of material 1 is 270 °.
This test specimen is placed in Material Testing Machine and carries out uniaxial compression test, and platen applies compressive load along the diametric(al) of disk sample in circumferential outer edge, take anisotropic composite material otch bight to occur that breakage is as critical load.
When applying compressive load, must keep upper pressing disc parallel with disc centre centering, until breakage appears in otch bight, pressure when record is damaged and damage location data analysis are obtained a result.
The invention has the beneficial effects as follows, adopt test method of the present invention can obtain easily the value of anisotropic composite material otch bight stress intensity factor, a kind of test method that anisotropic composite material otch bight has the stress intensity factor value of asymmetric stresses field of measuring is provided.This test method principle is reliable, and loading force is even, and test accuracy is high, and record data and to analyze data accurate have great importance for performance development and the optimal design of material.
Accompanying drawing explanation
Fig. 1 is geometric configuration and the load load mode of testing test specimen in the present invention.Test specimen is by material 1 and material 2 wedge shapes disk cemented together.The key groove of material 1 is 270 °, and the key groove of material 2 is 90o, and material 1 represents anisotropic composite material, and material 2 represents metallic briquette.Load pwith xthe angle of axle is α.
Fig. 2 is test fixture and loading principle schematic diagram.Comprise platen 3 and pressing disc 4, and the test test specimen being formed by material 1 and material 2.
Fig. 3 is the destruction closed curve based on measuring anisotropic composite material otch bight stress intensity factor.What record under each load load angle kvalue record with k 1/ k 1Cfor horizontal ordinate, k 2/ k 2Con coordinate system for ordinate, adjacent two loading angles kvalue connects the destruction closed curve that can obtain anisotropic composite material otch bight stress intensity factor with straight line.
Embodiment
Below by embodiment, illustrate test method and the process of measuring anisotropic composite material otch bight stress intensity factor.
1. test specimen condition:
(1) material 1, for carbon fiber strengthens composite plastic (CFRP) laminate, belongs to anisotropic material, and material 2 is cast iron briquetting, belongs to isotropic material.The two fits tightly formation thickness by wedge shape is 7 ± 1mm, the disc test sample that diameter is 17 ± 1.5mm.Each is loaded to angle and make 3~4 test specimens, and record corresponding disk diameter and thickness.
(2) test fixture: go up as shown in Figure 2 platen 3 parallel with disc centre centering with pressing disc 4, test specimen is in the center of upper pressing disc.
2. process of the test:
Diameter and the thickness of first record test test specimen are standby, in Material Testing Machine, test specimen are installed to fixture afterwards, adjust the upper pressing disc line of centres through disc centre axis and perpendicular during installation, and the direction of exerting pressure is along disk diameter direction.Then each test specimen is carried out respectively to uniaxial compression test, with the speed of the load angle stipulated and 0.05mm/min, load, until that material cut bight occurs is damaged, pressure and damage location when record is damaged.
3. test result analysis:
(1) the otch bight stress intensity factor of this material can be obtained by following formula:
In formula: subscript " FEM " and " exp " represent respectively the value of finite element analysis and the value that experiment records; pthe failing load (N) that represents test specimen; twith rthe thickness (mm) and the radius (mm) that represent respectively test specimen; λ k for characteristic exponent.Wherein, p fEM =100N, t fEM =1mm, r fEM =1mm.
Test findings is all with the arithmetic mean value representation of test figure.
(2) test specimen failure criteria: the data substitution above formula of the value of the generalized intensity factors that finite element analysis is obtained and experiment gained can obtain the value of the stress intensity factor under each load angle.
Because otch bight is having singularity along glide direction with vertical glide direction, therefore kthere are two values.Due to k 1with k 2unit different, so propose the expression formula of a Generalized Stress Intensity Factor based on failure criteria, be:
Wherein, k 1Cwith k 2Ccan be obtained by (1) formula, ψfor name fracture mixed mode phasing degree, can be obtained by following formula:
Utilize ψwith κ c( ψ) these two parameters just can define a destruction closed curve based on evaluating Generalized Stress Intensity Factor criterion, as shown in Figure 3.With k 1/ k 1Cfor horizontal ordinate, k 2/ k 2Cfor ordinate, utmost point footpath is κ c( ψ), polar angle is ψcurve map.In curve, represent place of safety, extra curvature represents unsafe region.

Claims (5)

1. one kind for measuring the test method of anisotropic composite material otch bight stress intensity factor, it is characterized in that disk test specimen after improving as test test specimen, its otch bight is in disc centre, by test specimen is carried out to uniaxial compression test, circumferential outer edge is applied along the compressive load of arbitrary diameter direction, measure its otch bight stress intensity factor, take anisotropic composite material otch bight occur breakage as test basic point.
2. test test specimen according to claim 1 is characterized in that the disk being combined by two fan-shaped wedge body test specimens, two sphenoids can be the materials of unlike material, its otch bight is at the center of disk, the key groove of tested anisotropic composite material is 270o, the key groove of another metallic briquette is 90o, the two closely combines formation thickness by wedge shape is 7 ± 1mm, diameter is the disc test sample of 17 ± 1.5mm, each is loaded to angle and make 3~4 test specimens, and record corresponding disk diameter and thickness.
3. the test method of measurement stress intensity factor according to claim 1, when it is characterized in that installing test specimen and testing, adjust the upper pressing disc line of centres through disc centre axis and perpendicular, the direction of exerting pressure is along disk diameter direction, then each test specimen is carried out respectively to uniaxial compression test, with the load angle of regulation and the speed of 0.05mm/min, load, until breakage appears in material cut bight, pressure when record is damaged and damage location data analysis are obtained a result.
4. data analysis according to claim 3, is characterized in that the otch bight stress intensity factor of this material can be obtained by following formula:
In formula: subscript " FEM " and " exp " represent respectively the value of finite element analysis and the value that experiment records; pthe failing load (N) that represents test specimen; twith rthe thickness (mm) and the radius (mm) that represent respectively test specimen; λ k for characteristic exponent, wherein, p fEM =100N, t fEM =1mm, r fEM =1mm.
5. otch according to claim 4 bight stress intensity factor, is characterized in that can being used for obtaining the expression formula of a Generalized Stress Intensity Factor based on failure criteria:
Wherein, k 1Cwith k 2Ccan be obtained by (1) formula, ψfor name fracture mixed mode phasing degree, can be obtained by following formula:
Utilize ψwith κ c( ψ) these two parameters just can define a destruction closed curve based on evaluating Generalized Stress Intensity Factor criterion, as shown in Figure 3, with k 1/ k 1Cfor horizontal ordinate, k 2/ k 2Cfor ordinate, utmost point footpath is κ c( ψ), polar angle is ψcurve map, in curve, represent place of safety, extra curvature represents unsafe region.
CN201410308765.1A 2014-07-01 2014-07-01 Test method for measuring stress intensity factor at cutting-angle part of anisotropic material Pending CN104132845A (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106802202A (en) * 2017-03-15 2017-06-06 哈尔滨工业大学 A kind of method for measuring anisotropic material plane stress
CN109916686A (en) * 2019-04-04 2019-06-21 上海交通大学 A kind of test sample of the anisotropy breaking strength of sheet metal
CN111024520A (en) * 2019-12-20 2020-04-17 中国矿业大学(北京) Calculation method, experimental method and experimental device for V-shaped grooving tip stress intensity factor under pure shear loading

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106802202A (en) * 2017-03-15 2017-06-06 哈尔滨工业大学 A kind of method for measuring anisotropic material plane stress
CN109916686A (en) * 2019-04-04 2019-06-21 上海交通大学 A kind of test sample of the anisotropy breaking strength of sheet metal
CN111024520A (en) * 2019-12-20 2020-04-17 中国矿业大学(北京) Calculation method, experimental method and experimental device for V-shaped grooving tip stress intensity factor under pure shear loading

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Application publication date: 20141105