ASTM E2004-2004 Standard Test Method for Facing Cleavage of Sandwich Panels《三合板表面裂缝的标准试验方法》.pdf
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1、Designation: E 2004 04Standard Test Method forFacing Cleavage of Sandwich Panels1This standard is issued under the fixed designation E 2004; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year of last revision. A number in par
2、entheses indicates the year of last reapproval. Asuperscript epsilon (e) indicates an editorial change since the last revision or reapproval.This standard has been approved for use by agencies of the Department of Defense.1. Scope1.1 This test method covers the determination of the cleav-age force t
3、o peel stiff facings from sandwich panels.1.2 The values stated in inch-pound units are to be regardedas the standard. The SI units given in parenthesis may beapproximate, and are for information only.1.3 This standard does not purport to address all of thesafety concerns, if any, associated with it
4、s use. It is theresponsibility of the user of this standard to establish appro-priate safety and health practices and determine the applica-bility of regulatory limitations prior to use.2. Referenced Documents2.1 ASTM Standards:2D 1781 Test Method for Climbing Drum Peel for AdhesivesE4 Practices for
5、 Force Verification of Testing Machines3. Terminology3.1 Definitions:3.1.1 adhesive failurefailure that is completely within theadhesive layer with no evidence of interfacial disbondingbetween the core and the adhesive, between the adhesive andthe facing, and no evidence of tearing or rupture within
6、 thecore.3.1.2 bond failurefailure that is interfacial and is either(a) between the adhesive and the core, or (b) between theadhesive and the facing; no core or adhesive failure will be inevidence in this type of failure.3.1.2.1 DiscussionIf bond failure occurs it should bespecified as to whether it
7、 is type (a)or(b).3.1.3 core failurefailure that is completely within the corematerial and is comprised of a tearing or rupture of the corematerial with no evidence of interfacial disbonding betweenthe core and the adhesive, within the adhesive itself, orbetween the adhesive and the facing.3.1.4 mix
8、ed-mode failurefailure that shows evidence ofmore than one of the three failure modes described above.3.1.4.1 DiscussionVisually estimate and report the per-cent of the total failure surface area that is covered by each typeof failure.4. Significance and Use4.1 This test method determines the cleava
9、ge force requiredto peel stiff facings from the core of sandwich panels, and isused to determine how well the facing is bonded to the core.Test Method D 1781 only works well with flexible facings. Asa guideline, the cleavage test method would work better onsandwich panels that have facings with a be
10、nding stiffness (EI)of greater than approximately 27.3 lbs-in2/inch width (3.09kNmm2/mm width). This converts to approximately 0.032 in.(0.81 mm) aluminum, 0.023 in. (0.57 mm) steel, and 0.046 in.(1.18 mm) fiberglass facings.5. Apparatus5.1 Test Machine, capable of maintaining a controlled load-ing
11、rate and indicating the load with an accuracy of 61%ofthe indicated value. The accuracy of the test machine shall beverified in accordance with Practices E4.5.2 Deflectometer, capable of measuring the displacementwith a precision of at least 610 %.5.3 Micrometer gage or caliper, capable of measuring
12、accurately to 0.01 in. (0.25 mm).6. Test Specimen6.1 The test specimen shall be from the sandwich panelbeing evaluated.6.2 Prepare the specimen according to the dimensionsspecified in Fig. 1.6.3 The loading blocks shall be bonded to the specimen withan adhesive or attached with pop-rivets. See Fig.
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