ASTM C583-2015 Standard Test Method for Modulus of Rupture of Refractory Materials at Elevated Temperatures《高温下耐火材料破裂模数的标准试验方法》.pdf

《ASTM C583-2015 Standard Test Method for Modulus of Rupture of Refractory Materials at Elevated Temperatures《高温下耐火材料破裂模数的标准试验方法》.pdf》由会员分享，可在线阅读，更多相关《ASTM C583-2015 Standard Test Method for Modulus of Rupture of Refractory Materials at Elevated Temperatures《高温下耐火材料破裂模数的标准试验方法》.pdf（4页珍藏版）》请在麦多课文档分享上搜索。

1、Designation: C583 15Standard Test Method forModulus of Rupture of Refractory Materials at ElevatedTemperatures1This standard is issued under the fixed designation C583; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year of la

2、st revision. A number in parentheses indicates the year of last reapproval. Asuperscript epsilon () indicates an editorial change since the last revision or reapproval.1. Scope1.1 This test method covers determination of the high-temperature modulus of rupture of refractory brick or mono-lithic refr

3、actories in an oxidizing atmosphere and under actionof a force or stress that is increased at a constant rate.1.2 The values stated in inch-pound units are to be regardedas standard. The values given in parentheses are mathematicalconversions to SI units that are provided for information onlyand are

4、 not considered standard.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 the applica-bility of regulatory limitations pri

5、or to use.2. Referenced Documents2.1 ASTM Standards:2E220 Test Method for Calibration of Thermocouples ByComparison Techniques3. Significance and Use3.1 Measuring the modulus of rupture of refractories atelevated temperatures has become a widely accepted means toevaluate materials at service tempera

6、tures. Many consumercompanies have specifications based on this type of test.3.2 This test method is limited to furnaces operating underoxidizing conditions. However, with modifications for atmo-sphere control in other test furnaces, the major criteria of thistest procedure may be employed without c

7、hange.3.3 This test method is designed for progressive applicationof a force or stress on a specimen supported as a simple beamwith center-point loading. Test apparatus designed for theprogressive application of a strain may yield different results,especially since refractory materials will reach a

8、semiplasticstate at elevated temperatures where Hookes law does notapply, that is, stress is then not proportional to strain.3.4 This test method applies to fired dense refractory brickand shapes, chemically bonded brick and shapes, shapesformed from castables, plastics, or ramming materials, and an

9、yother refractory that can be formed to the required specimendimension.4. Apparatus4.1 Use either an electrically heated or gas-fired furnace(Note 1). A typical cross section of the furnace containing thebearing edges is shown in Fig. 1. At least one pair of lowerbearing edges, made from volume-stab

10、le refractory material(Note 2), shall be installed in the furnace on 5-in. (127-mm)centers. A thrust column, containing the top bearing edge thatis made from volume-stable refractory material, shall extendoutside the furnace where means are provided for applying aload. The lower bearing edges and th

11、e bearing end of thesupport column shall have rounded bearing surfaces havingabout a14-in. (6-mm) radius (Note 3). The lower bearingsurfaces may be made adjustable, but must attain the standardspan of 5 6332 in. (127 6 2 mm). The length of the lowerbearing surfaces shall exceed the specimen width by

12、 about14in. (6 mm). The load shall be applied to the upper bearing edgeby any suitable means. Instrumentation for measuring the loadshall be accurate to 1 %. The thrust column shall be main-tained in vertical alignment and all bearing surfaces parallel inboth horizontal directions.NOTE 1The test fur

13、nace can be so constructed so that a number ofspecimens may be heated and tested at the same time. Bearing edges andloading devices may be provided for a number of individual specimens,but a more practical method is to provide means to move individualspecimens successively onto a single set of beari

14、ng edges for breaking.The use of a separate holding furnace for specimens to be transferred intothe test furnace for breaking is also satisfactory.NOTE 2A minimum of 90 % alumina content is recommended as asuitable refractory.NOTE 3All bearing surfaces should be checked periodically tomaintain a rou

15、nd surface.4.2 It is recommended that the furnace temperature becontrolled with calibrated platinum-rhodium/platinum thermo-couples connected to a program-controller recorder (see Test1This test method is under the jurisdiction of ASTM Committee C08 onRefractories and is the direct responsibility of

16、 Subcommittee C08.01 on Strength.Current edition approved March 1, 2015. Published April 2015. Originallyapproved in 1965. Last previous edition approved in 2010 as C583 10. DOI:10.1520/C0583-15.2For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact ASTM Customer Service at

17、serviceastm.org. For Annual Book of ASTMStandards volume information, refer to the standards Document Summary page onthe ASTM website.Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States1Method E220). Temperature differential within the fu

18、rnaceshall not be more than 620F (11C), but the controllingthermocouple shall be placed within12 in. (13 mm) of thegeometric center of a side face of the test specimen whenpositioned on the bearing edges.4.3 Furnace Atmosphere (gas-fired furnaces only)Abovea furnace temperature of 1470F (800C), the

19、furnace atmo-sphere shall contain a minimum of 0.5 % oxygen with 0 %combustibles. Take the atmosphere sample from the furnacechamber proper, preferably as near the test specimen aspossible.5. Sampling5.1 The sample shall consist of five specimens, each takenfrom five brick or shapes or from test spe

20、cimens made frommonolithic aggregate refractories.6. Test Specimen6.1 The standard test specimen shall be 1 6132 by 1 6132by approximately 6 in. (25 6 0.8 by 25 6 0.8 by approxi-mately 152 mm). Note in the report if other specimen sizes areused. Specimens cut from brick shall have at least one origi

21、nalbrick surface. If cut from shapes, the specimens shall be takenparallel to the longest dimension. For irregular shapes, all fourlong surfaces of the specimen may be cut faces. Note this in thereport.6.2 The relative ratio of the largest grain size to the smallestspecimen dimension may significant

22、ly affect the numericalresults. For example, smaller cut specimens containing largegrains may present different results than the bricks from whichthey were cut. Under no circumstances should 6- by 1- by 1-in.(152- by 25- by 25-mm) specimens be prepared and tested formaterials containing grains with

23、a maximum grain dimensionexceeding 0.25 in. (6.4 mm).6.3 Opposite faces of the specimen shall be parallel, andadjacent faces shall be perpendicular.6.4 Measure the width and depth of the test specimen atmid-span to the nearest 0.01 in. (0.3 mm).7. Procedure7.1 Set the specimens in either the test or

24、 holding furnacewithout an applied load, and heat to the test temperature usingthe following schedule:7.1.1 Burned Refractory ProductsThe rate of heatingfrom room temperature shall not exceed 600F (330C)/h to1800F (980C), and shall not exceed 200F (110C)/h from1800F to the test temperature (Note 4).

25、 Maintain the testtemperature for a minimum of3h(Note 5).NOTE 4Heating at 600F (330C)/h can initiate thermal shock in somebrick. A maximum heating rate of 150F (83C)/h is recommended formaterials sensitive to thermal shock.NOTE 5Maintaining specimens at test temperature for 3 h before loadapplicatio

26、n is adequate for most compositions and temperatures ofinterest. However, there may be certain compositions and temperaturesrequiring additional holding time at temperature in order to obtainconsistent results. Experience and use of the test procedure will aid indetermining when exploratory testing

27、is required to arrive at the holdingtime necessary. If departure is made from the specified minimum time, theholding time used will be included in the report of the results.7.1.2 Unburned or Chemically Bonded RefractoryProductsThe rate of heating from room temperature shall be600F (330C)/h to 1800F

28、(980C), and 200F (110C)/hfrom 1800F to the test temperature. Maintain the test tem-perature for a minimum of 12 h.7.2 Following the holding period, move the specimen to thesupporting bearing edges. When possible, an original face ofthe specimen shall be used for the tension face, that is, the facein

29、 contact with the two lower bearing edges. Apply the loadparallel to the direction (if known) of pressing of the specimen.FIG. 1 Cross Section of Typical Apparatus (Heating Means Not Shown)C583 1527.3 Control test temperature by the thermocouple that islocated within12 in. (13 mm) of the geometric c

30、enter of a sideface of the specimen when it is in position for testing. Holdspecimen in testing position 10 min before testing (Note 6).Temperature shall not vary more than minus 0 plus 20F(11C) from the specified test temperature.NOTE 6This hold period may be shortened for continuously chargedfurna

31、ces.7.4 Test temperatures are not specified but must be agreedupon between laboratories and must be included in the report.Test temperatures should be selected in even 100F (55C)intervals, but if agreed, other multiples could be used.7.5 Bring the top bearing edge to bear at mid-span on thespecimen,

32、 ensure proper alignment of bearing surfaces, andapply pressure through the loading mechanism until failure ofthe specimen occurs. The rate of application of the load on thespecimen shall be 175 6 17.5 lbf (778 6 77.8 N)/min. Theresulting rate of increase in bending stress for the standard 1 by1 by

33、6-in. (25 by 25 by 152-mm) specimen is 1312.5 6 131 psi(9.05 6 0.9 MPa)/min.3If non-standard specimens are used,the proper loading rate should be determined from the forego-ing stressing rate and full details disclosed in the report.7.6 Move the other specimens successfully onto the bearingedges and

34、 break them in accordance with the precedingprocedure.8. Calculation8.1 Calculate the modulus of rupture (MOR) for eachrectangular specimen as follows:MOR 5 3PL/2bd2(1)where:MOR = modulus of rupture, psi or MPa,P = concentrated load at rupture, lbf or N,L = span between supports, in. or mm,b = bread

35、th or width of specimen, in. or mm, andd = depth of specimen, in. or mm.9. Report9.1 Report the test temperature, the five individual testresults, and the average modulus of rupture and standarddeviation in lbf/in.2(or MPa) for the five specimens.9.2 Also, list in the report any deviations from stan

36、dard testrequirements such as specimen size, span, heating rate, soaktime, or loading rate.10. Precision and Bias10.1 Ruggedness tests conducted in 1977 showed that themost sensitive variables were specimen dimensions, testtemperature, and soak time. Of smaller influence were heatingrate above 1800F

37、 (980C) and loading rate. Test results areincorporated in the method.10.2 Interlaboratory Test DataThe results of interlabora-tory studies conducted in 1963 and in 1970 were used in 1979to revise the precision statements in accordance with latestrecommendations from ASTM Committee E11.10.2.1 In the

38、1963 study, four types of direct-bonded (fired)magnesite-chrome brick and two types of chemically-bondedmagnesite-chrome brick were tested at 1800F (980C) and2300F (1260C). Five laboratories tested five specimens ofeach brick at each test temperature. In the 1970 study, twotypes of direct-bonded chr

39、ome brick, one 95 % MgO firedpericlase brick (BOF type), and one 90 % alumina brick weretested at 2700F (1480C) by four laboratories using twentyspecimens of each type of brick.10.2.2 The precision was found to vary with the type ofbrick tested and also with the test temperature. Generally thestanda

40、rd deviation was proportional to the strength level, andrelative precision is given in terms of the average coefficientsof variation for each brick type and test temperature. However,in the case of fired brick, the relative precision tends toimprove with the level of strength.10.3 PrecisionFor two a

41、verages of five specimens testedwithin one laboratory, their difference is considered significantfor a probability of 95 % and t = 1.96 if it equals or exceeds therepeatability interval for the applicable brick type in Table 1.Likewise, the difference between two averages obtained by twolaboratories

42、 is considered significant if it equals or exceeds theapplicable reproducibility interval in Table 1.3This rate is 0.151 MPa/s, which is in agreement with the stress rate in PRERecommendation R 18, “Determination of the Hot Modulus of Rupture of Shapedand Unshaped Dense and Insulating Refractory Pro

43、ducts,” 1978. Copies of PREstandards are available from the PRE Secretary, Lowenstrasse 31, P.O. Box 3361,CH-8023 Zurich, Switzerland.TABLE 1 Relative PrecisionBrick TypeTest Temperature Average MOR Coefficient of VariationRepeatabilityInterval, % ofAverageAReproducibilityInterval, % ofAverageAF C p

44、si MPaWithinLabs, %BetweenLabs, %Chem-bond 1800 980 360 2.48 14.2 13.5 17.6 41.2Chem-bond 2300 1260 332 2.29 7.7 13.6 9.4 39.1Direct-bond 1800 980 1530 10.55 15.7 17.4 19.4 52.9Direct-bond 2300 1260 1208 8.33 17.9 15.3 22.2 47.9Direct-bond 2700 1480 708 4.88 32.3 29.8 40.0 91.7Periclase 2700 1480 13

45、02 8.98 21.0 16.2 26.4 52.0Alumina 2700 1480 1836 12.66 17.6 10.4 21.8 36.1ABased on five specimens.C583 15310.4 BiasNo justifiable statement of bias is possiblebecause the true value of hot modulus of rupture cannot beestablished.11. Keywords11.1 compressive load; deformation resistance; flexuralst

46、rength; high temperature; modulus of rupture; monolithicrefractories; refractory brickASTM International takes no position respecting the validity of any patent rights asserted in connection with any item mentionedin this standard. Users of this standard are expressly advised that determination of t

47、he validity of any such patent rights, and the riskof infringement of such rights, are entirely their own responsibility.This standard is subject to revision at any time by the responsible technical committee and must be reviewed every five years andif not revised, either reapproved or withdrawn. Yo

48、ur comments are invited either for revision of this standard or for additional standardsand should be addressed to ASTM International Headquarters. Your comments will receive careful consideration at a meeting of theresponsible technical committee, which you may attend. If you feel that your comment

49、s have not received a fair hearing you shouldmake your views known to the ASTM Committee on Standards, at the address shown below.This standard is copyrighted by ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959,United States. Individual reprints (single or multiple copies) of this standard may be obtained by contacting ASTM at the aboveaddress or at 610-832-9585 (phone), 610-832-9555 (fax), or serviceastm.org (e-mail); or through the ASTM website(www.astm.org). Permission rights to pho