B36/B36M Specification for Brass Plate,Sheet,Strip,and Rolled Bar3
B152Specification for Copper Sheet,Strip,Plate,and Rolled Bar3
B209Specification for Aluminum and Aluminum-Alloy Sheet and Plate4
B265Specification for Titanium and Titanium Alloy Strip, Sheet,and Plate5
D907Terminology of Adhesives6
D4896Guide for U of Adhesive-Bonded Single Lap-Joint Specimen Test Results6
E4Practices for Force Verification of Testing Machines7 3.Terminology
3.1Definitions—Many terms in this test method are defined in Terminology D907.
4.Significance and U
4.1This test method is primarily comparative.However,it does have application as a discriminator in determining varia-tions in adherend surface preparation parameters and adhesive environmental durability.The test method has found applica-tions in controlling surface preparations,primer,and adhesive systems for determining strength properties of tested systems.
4.2The misu of strength values obtained from this test method as design-allowable stress values for structural joints could lead to product failure,property damage,and human injury.The apparent shear strength of an adhesive obtained from a given small single-lap specimen may differ from that obtained from a joint made with different adherends or by a different bonding process.The normal variation of temperature and moisture in the rvice environment caus the adherends and the adhesive to swell or shrink.The adherends and adhesive are likely to have different thermal and moisture coefficients of expansion.
4.3Even in small specimens,short-term environmental changes may induce internal stress or chemical changes in the adhesive that permanently affect the apparent strength and other mechanical properties of the adhesive.The problem of predicting joint behavior in a changing environment is even more difficult if a different type of adherend is ud in a larger structural joint than was ud in the small specimen.
推崇的意思是什么4.4The apparent shear strength measured with a single-lap specimen is not suitable for determining design-allowable stress for designing structural joints that differ in any manner from the joints tested without thorough analysis and under-standing of the joint and adhesive behaviors.
4.5Single-lap tests may be ud for comparing and lect-ing adhesives or bonding process for susceptibility to fatigue and environmental changes,but such comparisons must be made with great caution since different adhesives may respond differently in different joints.See Guide D4896for further discussion of the concepts relative to interpretation of adhesive-bonded single-lap-joints.
5.Apparatus
5.1The testing machine shall conform to the requirements of Practices E4.The testing machine shall be so lected that the breaking load of the specimens falls between15and85 percent of the full-scale capacity.The machine shall be capable of maintaining a rate of loading of80to100kg/cm2(1200to 1400psi)/min,or,if the rate is dependent on crosshead motion, the machine should be t to approach this rate of loading, approximately0.05in./min.It shall be provided with a suitable pair of lf-aligning grips to hold the specimen.It is recom-mended that the jaws of the grips shall engage the outer25 mm(1in.)of each end of the test specimenfirmly.
5.2The grips and attachments shall be so constructed that they will move into alignment with the test specimen as soon as the load is applied,so that the long axis of the test specimen will coincide with the direction of the applied pull through the center line of the grip asmbly.
5.3The length of overlap of the specimen may be varied where necessary.The length of the specimen in the jaws, however,must not be varied.The distance from the end of the lap to the end of the jaws should be63mm(21⁄2in.)in all tests.
6.Test Specimens
6.1Test specimens shall conform to the form and dimen-sions shown in Fig.1.The shall be cut from test panels prepared as prescribed in Section
7.The recommended thick-ness of the sheets is1.6260.125mm(0.06460.005in.).The recommended length of
overlap for most metals of1.62mm
(0.064in.)in thickness is12.760.25mm(0.560.01in.).
6.2Since it is undesirable to exceed the yield point of the
metal in tension during test,the permissible length of overlap
in the specimen will vary with the thickness and type of metal,
and on the general level of strength of the adhesive being
investigated.The maximum permissible length may be com-
puted from the following relationship:
L5Fty t/t(1)
where:暮雨洒江天
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L=length of overlap,in.,
t=thickness of metal,in.,
Fty=yield point of metal(or the stress at proportional
limit),psi,and
t=150percent of the estimated average shear strength
in adhesive bond,psi.
6.3A variation in thickness of the metal,and the length of
overlap,will likely influence the test values and make direct
comparison of data questionable.For this reason,in compara-
tive or specification tests,the thickness should preferably be
1.6260.125mm(0.06460.005in.)and the length of overlap
3Annual Book of ASTM Standards,V ol02.01.
4Annual Book of ASTM Standards,V ol02.02.
5Annual Book of ASTM Standards,V ol02.04.
6Annual Book of ASTM Standards,V ol15.06.
7Annual Book of ASTM Standards,V ol03.01.FIG.1Form and Dimensions of Test Specimen
should preferably be12.760.25mm(0.560.01in.),or not in excess of the value computed in6.2.For development tests values could be different,but should then be constant.
6.4The following grades of metal are recommended for the test specimens:
Metal ASTM Designation
Brass B36,C26800(Alloy8)
Copper B152,C11000
Aluminum B209,Alloy2024,T3temper
Steel A109,Grade2
档案自查报告Corrosion-resisting steel A167,Type302
Titanium B265
6.5At least30specimens shall be tested,reprenting at least four different joints.However,if statistical analysis of data and variance is employed,it should be possible to reduce this number.
7.Preparation of Test Joints
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7.1It is recommended that test specimens be made up in multiples of at leastfive specimens,and then cut into indi-vidual test specimens(Note1),Fig.2and Fig.3.Cut sheets of the metals prescribed in6.1and6.4to suitable size.All edges of the metal panels and specimens which will be within(or which will bound)the lap joints shall be machined true (without burrs or bevels and at right angles to faces)and smooth(rms160max)before the panels are surface-treated and bonded.Clean and dry the sheets carefully,according to the procedure prescribed by the manufacturer of the adhesive, and asmble in pairs.Prepare and apply the adhesive accord-ing to the recommendations of the manufacturer of the adhe-sive.Apply the adhesive to a sufficient length in the area
习惯名言>贷款电话across FIG.2Standard Test
Panel
the end of one or both metal sheets so that the adhesive will
cover a space approximately 6mm (1⁄4in.)longer than the
overlap as lected in Section 6.Asmble the sheets so that
they will be held rigidly so that the length of the overlap will
be controlled,as indicated in Section 6,within 0.25mm
(60.01in.),and the adhesive allowed to cure as prescribed by
the manufacturer of the adhesive.
N OTE 1—Bonding specimens in multiple panels is believed to give
more reprentative specimens.However,individual specimens may be
prepared if agreeable to the supplier or the purchar of the adhesive.
评价理论8.Preparation of Test Specimens
8.1Cut the test specimens,as shown in Fig.1,from the
panels,Figs.2and 3.Perform the cutting operation so as to
avoid overheating or mechanical damage to the joints (Note 2).
For final preparation trim panel area according to Fig. 2.
Measure the width of the specimen and the length of the
overlap to the nearest 0.25mm (0.01in.)to determine the shear
area.
N OTE 2—A five-tooth,typetter’s circular saw has been found suitable
for such purpos.
9.Procedure
9.1Test the specimens,prepared as prescribed in Section 8,
as soon after preparation as possible.The manufacturer of the adhesive may,however,prescribe a definite period of condi-tioning under specific conditions before testing.9.2Place the specimens in the grips of the testing machine so that the outer 25mm (1in.)of each end are in contact with the jaws (e 5.3)and so that the long axis of the test specimen coincides with the direction of applied pull through the center line of the grip asmbly.Apply the loading immediately to the specimen at the rate of 80to 100kg/cm 2(1200to 1400psi)of the shear area per min.Continue the load to failure.This rate of loading will be approximated by a free crosshead speed of 1.3mm (0.05in.)/min.10.Calculations 10.1Record the load at failure and the nature and amount of this failure (cohesion in adhesive or metal,or adhesion)for each specimen.Express all failing loads in kilograms per square centimeter (pounds per square inch)of shear area,calculated to the nearest 0.06cm 2(0.01in.2).11.Report 11.1Report the following:11.1.1Complete identification of the adhesive tested,in-cluding type,source,date manufactured,manufacturers’code numbers,form,etc.,11.1.2Comp
lete identification of the metal ud,its thick-ness,and the method of cleaning and preparing its surfaces prior to bonding,11.1.3Application and
bonding conditions ud in prepar-ing specimens,11.1.4Average thickness of adhesive layer after formation of the joint within 0.001in.(0.025mm).The method of obtaining the thickness of the adhesive layer shall be described including procedure,location of measurements,and range of measurements.11.1.5Length of overlap ud,11.1.6Conditioning procedure ud for specimens prior to testing,11.1.7Number of specimens tested,11.1.8Number of joints reprented and type of joint if other than single overlap,11.1.9Maximum,minimum,and average values for the failing load,and 11.1.10The nature of the failure,including the average estimated percentages of failure in the cohesion of the adhe-sive,contact failure,and adhesion to the metal.12.Precision and Bias 12.1The precision and bias statement for this test method has not been determined yet.Archival and round-robin infor-mation is being reviewed,and the results are expected by September 2004.13.Keywords 13.1adhesives;metal-to-metal;shear strength;single-lap joint;tension loading
FIG.3Optional Panel for Acceptance Tests Only
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