ASTM D4812-2006 Standard Test Method for Unnotched Cantilever Beam Impact Resistance of Plastics《塑料的无凹口悬臂梁抗冲击强度的标准试验方法》.pdf

《ASTM D4812-2006 Standard Test Method for Unnotched Cantilever Beam Impact Resistance of Plastics《塑料的无凹口悬臂梁抗冲击强度的标准试验方法》.pdf》由会员分享，可在线阅读，更多相关《ASTM D4812-2006 Standard Test Method for Unnotched Cantilever Beam Impact Resistance of Plastics《塑料的无凹口悬臂梁抗冲击强度的标准试验方法》.pdf（12页珍藏版）》请在麦多课文档分享上搜索。

1、Designation: D 4812 06Standard Test Method forUnnotched Cantilever Beam Impact Resistance of Plastics1This standard is issued under the fixed designation D 4812; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year of last revi

2、sion. A number in parentheses indicates the year of last reapproval. Asuperscript epsilon (e) indicates an editorial change since the last revision or reapproval.1. Scope*1.1 This test method covers the determination of the resis-tance of plastics to breakage by flexural shock, as indicated bythe en

3、ergy extracted from standardized pendulum-type ham-mers, mounted in standardized machines, in breaking standardspecimens with one pendulum swing. The result of this testmethod is reported as energy absorbed per unit of specimenwidth.NOTE 1The pendulum-type test instruments have been standardizedin t

4、hat they must comply with certain requirements, including a fixedheight of hammer fall that results in a substantially fixed velocity of thehammer at the moment of impact. Pendulums of different initial energies(produced by varying their effective weights) are recommended for usewith specimens of di

5、fferent impact strengths. Moreover, manufacturers ofthe equipment are permitted to use different lengths and constructions ofpendulums (with resulting possible differences in pendulum rigidities (seeSection 5), and other differences in machine design).1.2 The values stated in SI units are to be rega

6、rded asstandard. The values given in brackets are for information only.1.3 This standard does not purport to address all of thesafety concerns, if any, associated with its use. It is theresponsibility of the user of this standard to establish appro-priate safety and health practices and determine th

7、e applica-bility of regulatory limitations prior to use.NOTE 2This standard and ISO 180, Method 1U, are similar in contentbut are not technically equivalent.2. Referenced Documents2.1 ASTM Standards:2D 256 Test Methods for Determining the Izod PendulumImpact Resistance of PlasticsD 618 Practice for

8、Conditioning Plastics for TestingD 883 Terminology Relating to PlasticsD 5947 Test Methods for Physical Dimensions of SolidPlastics SpecimensE 691 Practice for Conducting an Interlaboratory Study toDetermine the Precision of a Test Method3. Terminology3.1 DefinitionsDefinitions used in this test met

9、hod are inaccordance with Terminology D 883.4. Summary of Test Method4.1 This test method differs from others of similar characterin that unnotched test specimens are used (see Test MethodsD 256 for procedures using notched test specimens). The lackof a notch makes this test method especially useful

10、 forreinforced materials where a notch may mask the effects oforientation. It may also be used with other filled or unrein-forced materials where a stress-concentrating notch is notdesired. It is not valid for materials that twist when subjectedto this test.5. Significance and Use5.1 The pendulum-im

11、pact test indicates the energy to breakstandard test specimens of specified size under stipulatedconditions of specimen mounting and pendulum velocity atimpact.5.2 The energy lost by the pendulum during the breakage ofthe specimen is the sum of the energies required to produce thefollowing results:5

12、.2.1 To initiate fracture of the specimen,5.2.2 To propagate the fracture across the specimen,5.2.3 To throw the free end (or pieces) of the brokenspecimen (toss correction),5.2.4 To bend the specimen,5.2.5 To produce vibration in the pendulum arm,5.2.6 To produce vibration or horizontal movement of

13、 themachine frame or base,5.2.7 To overcome friction in the pendulum bearing and inthe indicating mechanism, and to overcome windage (pendu-lum air drag),5.2.8 To indent or deform plastically the specimen at theline of impact, and5.2.9 To overcome the friction caused by the rubbing of thestriking no

14、se (or other part of the pendulum) over the face ofthe bent specimen.5.3 For relatively brittle materials for which fracture propa-gation energy is small in comparison with the fracture initiationenergy, the indicated impact energy absorbed is, for all1This test method is under the jurisdiction ofAS

15、TM Committee D20 on Plasticsand is the direct responsibility of Subcommittee D20.10 on Mechanical Properties.Current edition approved March 15, 2006. Published March 2006. Originallyapproved in 1988. Last previous edition approved in 2005 as D 4812 - 05.2For referenced ASTM standards, visit the ASTM

16、 website, www.astm.org, orcontact ASTM Customer Service at serviceastm.org. For Annual Book of ASTMStandards volume information, refer to the standards Document Summary page onthe ASTM website.1*A Summary of Changes section appears at the end of this standard.Copyright ASTM International, 100 Barr H

17、arbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.practical purposes, the sum of items given in 5.2.1 and 5.2.3.The toss correction (5.2.3) may represent a very large fractionof the total energy absorbed when testing relatively dense andbrittle materials.5.4 For materials for

18、 which the fracture propagation energy(5.2.2) may be large compared to the fracture initiation energy(5.2.1), factors (5.2.2, 5.2.5, and 5.2.9) can become quitesignificant, even when the specimen is accurately machinedand positioned and the machine is in good condition withadequate capacity (Note 3)

19、. Bending (5.2.4) and indentationlosses (5.2.8) may be appreciable when testing soft materials.NOTE 3Although the frame and base of the machine should besufficiently rigid and massive to handle the energies of tough specimenswithout motion or excessive vibration, the pendulum arm cannot be madevery

20、massive because the greater part of its mass must be concentratednear its center of percussion at the striking nose. Locating the striking noseprecisely at the center of percussion reduces vibration of the pendulumarm when used with brittle specimens. However, some losses due topendulum-arm vibratio

21、n, the amount varying with the design of thependulum, will occur with tough specimens even when the striking noseis properly positioned.5.5 In a well-designed machine of sufficient rigidity andmass the losses due to the items given in 5.2.6 and 5.2.7 shouldbe very small. Vibrational losses (5.2.6) c

22、an be quite largewhen specimens of tough materials are tested in machines ofinsufficient mass which are not securely fastened to a heavybase.5.6 This test method requires that the type of failure for eachspecimen be recorded as one of the three coded categoriesdefined as follows:5.6.1 C (Complete Br

23、eak)A break in which the specimenis separated into two or more pieces.5.6.2 P (Partial Break)An incomplete break that hasfractured at least 90 % of the depth of the specimen.5.6.3 NB (Non-Break)An incomplete break where thefracture extends less than 90 % of the depth of the specimen.5.6.3.1 For toug

24、h materials the pendulum may not have theenergy necessary to completely break the extreme outermostfibers and toss the broken piece or pieces. Results obtainedfrom “non-break” specimens shall be considered a departurefrom standard and shall be reported as “NB” only and anumerical value shall not be

25、reported. Impact values cannot bedirectly compared for any two materials that experiencedifferent types of failure as defined by this code.5.6.4 Averages reported must likewise be derived fromspecimens contained within a single failure category. Thisletter code will be included with the reported imp

26、act identify-ing the types of failure associated with the reported value. Ifmore than one type of failure is observed for a sample material,then the report will indicate the average impact value for eachtype of failure, followed by the percent of the specimens failingin that manner and identified by

27、 the letter code.5.7 The value of this impact test method lies mainly in theareas of quality control and materials specification. The factthat a material shows twice the energy absorption of anotherunder these conditions of test does not indicate that this samerelationship will exist under another s

28、et of test conditions. Theranking of materials may even be changed under differenttesting conditions.5.8 Before proceeding with this test method, referenceshould be made to the specification of the material being tested.Any test specimen preparation, conditioning, dimensions, ortesting parameters, o

29、r combination thereof, covered in thematerial specification shall take precedence over those men-tioned in this test method except in cases where to do so wouldconflict with the purpose for conducting testing. If there are nomaterial specifications, then the default conditions apply.6. Apparatus6.1

30、Impact Machine, consisting of a massive base on whichis mounted a vise for holding the specimen and to which isconnected, through a rigid frame and antifriction bearings, oneof a number of pendulum-type hammers (or one basic hammerto which extra weights may be attached) having an initialenergy suita

31、ble for use with the particular specimen to betested, plus a pendulum holding and releasing mechanism anda mechanism for indicating the breaking energy of the speci-men. A jig for positioning the specimen in the vise and graphsor tables to aid in the calculation of the correction for frictionand win

32、dage should be included. See Fig. 1 for one type ofmachine that may be used. The type of machine that is depictedcan also be used for the testing of notched specimens usingTest Methods D 256. Detailed requirements are given in6.2-6.5. See Appendix X1 for general methods for checkingand calibrating t

33、he machine. Additional instructions for adjust-ing a particular machine should be supplied by the manufac-turer.6.2 Pendulum, consisting of a single or multimembered armwith a bearing on one end and a head, containing the strikingnose, on the other. Although a large proportion of the mass ofthe pend

34、ulum should be concentrated in the head, the arm mustbe sufficiently rigid to maintain the proper clearances andgeometric relationships between the machine parts and theFIG. 1 Cantilever Beam Impact Test EquipmentD4812062specimen and to minimize vibrational losses which are alwaysincluded in the mea

35、sured impact value.6.2.1 Striking Nose (of the Pendulum), of hardened steel andcylindrical surface having a radius of curvature of 0.80 6 0.20mm 0.031 6 0.008 in. with its axis horizontal and perpen-dicular to the plane of swing of the pendulum.6.2.1.1 The line of contact of the striking nose shall

36、belocated at the center of percussion of the pendulum within62.54 mm 60.100 in. (Note 4). Those portions of thependulum adjacent to the cylindrical striking edge shall berecessed or inclined at a suitable angle so that there will be nochance for other than this cylindrical surface coming intocontact

37、 with the specimen during the break.6.2.2 Pendulum Holding and Releasing Mechanism,inaposition such that the vertical height of fall of the striking noseshall be 610 6 2 mm 24.0 6 0.1 in.; this will produce avelocity of the striking nose at the moment of impact ofapproximately 3.46 m 11.35 ft/s. The

38、 mechanism shall be soconstructed and operated that it will release the pendulumwithout imparting acceleration or vibration to it.6.2.3 The effective length of the pendulum shall be between0.325 and 0.406 m 12.8 and 16.0 in. so that the aboverequired elevation of the striking nose may be obtained by

39、raising the pendulum to an angle between 60 and 30 above thehorizontal.NOTE 4The distance from the axis of support to the center ofpercussion may be determined experimentally from the period of smallamplitude oscillations of the pendulum, as follows:L 5 g/4p2!p2(1)where:L = distance from the axis of

40、 support to the center of percussion, mft,g = local gravitational acceleration (known to an accuracy of one partin one thousand), m/s2ft/s2,p = 3.1416 (4p2= 39.4786), andp = period, s, of a single complete swing (to and fro) determined fromat least 50 consecutive and uninterrupted swings (known to o

41、nepart in two thousands). The angle of swing shall be less than 5each side of center.6.2.4 The machine shall be provided with a basic pendulumcapable of delivering an energy of 2.710 6 0.135 J 2.00 60.10 ft-lbf. This pendulum shall be used with all specimensthat extract less than 85 % of this energy

42、. Heavier pendulumsshall be provided for specimens that require more energy tobreak. These may be separate interchangeable pendulums orone basic pendulum to which extra pairs of equal calibratedweights may be attached rigidly to opposite sides of thependulum at its center of percussion. It is impera

43、tive that theextra weights shall not change the position of the center ofpercussion of the free-hanging rest point of the pendulum.6.2.4.1 Arange of pendulums having energies from 2.710 to21.680 J 2 to 16 ft-lbf has been found to be sufficient for usewith most plastic specimens and may be used with

44、mostmachines. A series of pendulums such that each has twice theenergy of the next lighter one will be found convenient. Eachpendulum shall have an energy within 60.5 % of its nominalcapacity.6.2.5 When the pendulum is free-hanging, the strikingsurface shall come within 0.5 % of scale of touching th

45、e frontface of a standard specimen. During an actual swing thiselement shall make initial contact with the specimen on a line22.00 6 0.05 mm 0.866 6 0.002 in. above the top surface ofthe vise.6.2.6 Means shall be provided for determining the energyexpended by the pendulum in breaking the specimen. T

46、his isaccomplished using either a pointer and dial mechanism or anelectronic system consisting of a digital indicator and sensor(typically an encoder or resolver). In either case, the indicatedbreaking energy is determined by detecting the height of rise ofthe pendulum beyond the point of impact in

47、terms of energyremoved from that specific pendulum. Since the indicatedenergy must be corrected for pendulum-bearing friction,pointer friction, pointer inertia, and pendulum windage, in-structions for making these corrections are included in 9.3 andAnnex A1 and Annex A2. If the electronic display do

48、es notautomatically correct for windage and friction, it shall beincumbent for the operator to determine the energy lossmanually. (See Note 5)NOTE 5Many digital indicating systems automatically correct forwindage and friction. The equipment manufacturer may be consulted fordetails concerning how thi

49、s is performed, or if it is necessary to determinethe means for manually calculating the energy loss due to windage andfriction.6.3 Vise, for clamping the specimen rigidly in position sothat the long axis of the specimen is vertical and at right anglesto the top plane of the vise. The top edges of the jaws of thevise shall have a radius of 0.25 6 0.12 mm 0.010 6 0.005 in.(see Fig. 2).NOTE 6It is especially important that the correct radius be maintainedon the moveable vise jaw. Any sharp edge, nick, or burr on this jaw willcreate a “notch” or stress co