SAE J 125-1988 Elevated Temperature Properties of Cast Irons《锻铁的升温性能》.pdf

1、SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirelyvoluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefro

2、m, is the sole responsibility of the user.”SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions.QUESTIONS REGARDING THIS DOCUMENT: (724) 772-8512 FAX: (724) 776-0243TO PLACE A DOCUMENT

3、 ORDER; (724) 776-4970 FAX: (724) 776-0790SAE WEB ADDRESS http:/www.sae.orgCopyright 1988 Society of Automotive Engineers, Inc.All rights reserved. Printed in U.S.A.SURFACEVEHICLE400 Commonwealth Drive, Warrendale, PA 15096-0001INFORMATIONREPORTAn American National StandardJ125REAF.MAY88Issued 1969-

4、09Reaffirmed 1988-05Superseding J125 SEP69ELEVATED TEMPERATURE PROPERTIES OF CAST IRONSForewordThis Document has not changed other than to put it into the new SAE Technical Standards Boardformat.This document is currently under revision.1. ScopeThe purpose of this SAE Information Report is to provid

5、e automotive engineers and designers with aconcise statement of the basic characteristics of cast iron under elevated temperature conditions. As such,the report concentrates on general statements regarding these properties with limited illustrative data,anticipating that those who may be interested

6、in more detail will want to use the bibliography provided at theconclusion of the report.2. References2.1 Related PublicationsThe following publications are provided for information purposes only and are not arequired part of this document.2.1.1 OTHER PUBLICATIONS1. “Mechanical Properties of Metals

7、and Alloys.“ U.S. Dept. of Commerce Circular C-447, NationalBureau of Standards, 1943.2. Kattus and McPherson, “Properties of Cast Iron at Elevated Temperatures.“ ASTM Special TechnicalPublication No. 248.3. Malleable Iron Casting Handbook. Malleable Founders Society, 1960.4. Gray Iron Castings Hand

8、book. Gray Iron Founders Society, Inc., 1958.5. Cast Metals Handbook. American Foundrymens Society, 1957.6. Colin J. Smithell, “Metals Reference Book.“ Washington Butterworths, 1962.7. Metals Handbook, 8th Edition. American Society for Metals, 1961.8. “Engineering Properties of Ductile Ni-Resist Aus

9、tenitic Irons.“ International Nickel Co., 1955.9. Schelleng and Eash, “Effect of Composition on the Elevated-Temperature Properties of Ductile Iron.“Proceedings of ASTM, Vol. 57, 1957.10. Greene and Sefing, “Cast Irons in High Temperature Service.“ Corrosion, Vol. 11, No. 7, July 1955.11. Turnbull a

10、nd Wallace, “Molybdenum Effect on Gray Iron Elevated Temperature Properties.“Transactions AFS, Vol. 67, 1959.12. F. B. Foley, “Mechanical Properties at Temperature of Ductile Cast Iron.“ Preprint No. 55-A-204,ASME, 1955.13. Engineering Properties of Ni-Resist Ductile Irons.“ International Nickel Co.

11、, 1958.COPYRIGHT Society of Automotive Engineers, Inc.Licensed by Information Handling ServicesSAE J125 Reaffirmed MAY88-2-14. Elevated Temperature Properties of Ductile Cast Irons.“ ASM Transactions, Vol. 47, 1955.15. Scholz, Doane, and Timmons, “Effects of Molybdenum on Stability and High Temperat

12、ure Propertiesof Pearlitic Malleable Iron.“ AFS Transactions, Vol. 63, 1955.16. D. A. Pearson, “Stress-Rupture and Elongation of Malleable Iron at Elevated Temperatures.“ AFSTransactions, Vol. 74, 1966.17. W. L. Collins, “Fatigue and Static Load Tests of an Austenitic Cast Iron at Elevated Temperatu

13、res.“ASTM Proceedings, Vol. 48, 1948.3. IntroductionCast irons, like steels and other metals, lose strength as operating temperatures increase.Composition is of importance not only because of its effect on the basic properties of materials at elevatedtemperatures, but also because in cast irons it i

14、nfluences growth resulting from oxidation and microstructuralchanges. Irons may be used in most atmospheres at temperatures up to 750 F without growth being a seriousfactor. Beyond 900 F graphitization can cause growth and above 1200 F internal oxidation can cause growthunless sufficient alloy is pr

15、esent to prevent it.Deterioration of properties at high temperatures is in general time-dependent as well as temperature-dependent. Even at temperatures where strength has been greatly reduced, many useful hours of life can beobtained from a structure if proper allowances are made in the initial des

16、ign. Where applications involvesustained stress at high temperature, the most valuable information for the designer is the creep rate at thetemperature and stress involved. However, creep rate data generally involve long time tests and as aconsequence complete information has not been generated for

17、all materials under all conditions. Instead, ithas been the practice for many years to compare materials in shorter duration tests. Such tests are calledstress-to-rupture tests or more simply stress-rupture tests. These are conducted in the temperature ranges ofinterest but usually at much greater l

18、oads than any realistic design. In general, materials showing superiorstress-rupture life have the lowest creep rates. This type of information has been used primarily for materialdevelopment work. It can be used by the designer, however, to select better material on a comparison basis.Several types

19、 of iron are included in this section to show trends; they are representative of broad classes ofirons used commercially, and for which thermal data are available in the literature.4. Effect of Elevated Temperature on Mechanical Properties4.1 Tensile StrengthThe tensile strength of ferrous materials

20、 generally shows small changes from roomtemperature up to 600800 F, at higher temperature the strengths usually fall rather rapidly. The presence ofalloying elements which affect the stability of the higher strength microstructures tends to delay this effect orraise the temperature at which rapid lo

21、ss of strength occurs. In some ferrous alloys, changes in microstructureoccur at temperatures between room temperature and 800 F which may cause small changes in strength and,in fact, may cause reversals in the strength versus temperature curve. In Figure 1, examples of tensile strengthversus temper

22、ature for some typical cast irons are illustrated in comparison with the behavior of low carbonsteel. Generally, the changes in structure which occur over this temperature range are associated withtempering after hardening. These changes are irreversible.COPYRIGHT Society of Automotive Engineers, In

23、c.Licensed by Information Handling ServicesSAE J125 Reaffirmed MAY88-3-FIGURE 1ELEVATED TEMPERATURE TENSILE STRENGTH4.2 Stress Rupture PropertiesWhere metals are required to sustain loads over long periods of time at elevatedtemperatures, the stress-rupture test is used as an indication of the relat

24、ive load-carrying ability at the testtemperature.TABLE 1CHEMICAL COMPOSITION FOR CAST IRONS SHOWN IN FIGURES 17Material Alloying, %T.C. C Si Mn P S Cr Ni Mo MgAlloy gray cast iron (ASTM A 48, No. 60) (2)(1)1. Parenthetical numbers indicate source of data in 2.2.3.06 1.79 0.70 0.04 0.09 0.61 0.04 0.8

25、4 Alloy gray cast iron (SAE G4500) (2) 3.31 1.56 0.68 0.19 0.114 0.08 0.08 0.73 Gray cast iron SAE G4000 (2) 3.27 1.74 0.72 0.26 0.156 0.08 0.15 0.07 Ferritic malleable (3) (Creep and stress rupture data)2.16 1.01 0.29 0.11 0.074 0.017 2.29 1.17 0.38 0.148 0.095 0.000Pearlitic malleable (3) 2.27 1.0

26、1 0.89 0.135 0.098 0.019 2.29 1.15 0.75 0.110 0.086 0.000Ferritic malleable (3) (Elevated temperature tensile strength data)2.30 0.98 0.30 0.162 0.078 2.33 1.05 0.34 0.168 0.084Gray cast iron SAE G4500 (4) 2.84 1.52 1.05 0.07 0.124 0.31 0.20 Ferritic ductile iron (4) 3.7 2.6 0.40 1.0 Low carbon stee

27、l (7) 0.08 0.25 0.30 0.045 0.060 0.20 0.80Austenitic ductile + Cr and Mo (9) 2.38 1.99 0.62 3.05 30.18 0.95 0.13Austenitic ductile + Cr (9) 2.98 2.20 1.15 2.36 20.48 0.085Ferritic ductile iron (4) 3.64 2.66 0.46 0.032 0.014 0.66 0.076Austenitic cast iron (17) 2.63 2.14 1.23 0.16 0.059 2.09 14.9 COPY

28、RIGHT Society of Automotive Engineers, Inc.Licensed by Information Handling ServicesSAE J125 Reaffirmed MAY88-4-The material is stressed in tension under a constant load at a constant temperature and the time that it takesthe sample to rupture under these conditions is recorded. Separate samples of

29、the material are stressedunder a number of different loads at the same temperature and the rupture times are plotted against load togive a stress-rupture curve for the material. Typical stress-rupture curves for a number of SAE cast irons andalloyed irons at 800 F are plotted in Figure 2. Stress-rup

30、ture curves for these and other cast irons at 1000 Fare plotted in Figure 3, which includes a stress-rupture curve for low carbon wrought steel for comparison.FIGURE 2STRESS RUPTURE PROPERTIES OF CAST IRONS AT 800 FFIGURE 3STRESS RUPTURE PROPERTIES OF CAST IRONS AT 1000 FCOPYRIGHT Society of Automot

31、ive Engineers, Inc.Licensed by Information Handling ServicesSAE J125 Reaffirmed MAY88-5-4.3 Creep Properties of IronsAnother important temperature effect on cast irons is the effect of creep orelongation per hour at a given stress and temperature. These tests are difficult to run on cast irons becau

32、se ofthe growth and oxidation phenomena. Figure 4 shows typical creep curves for some SAE and alloyed castirons at 800 and 1000 F. A creep curve for a plain carbon steel at 1000 F is included for comparison. Thevalues shown on the creep rate curves in Figure 4 include any growth that occurred during

33、 the tests. Thisallows these figures to be used as design parameters.FIGURE 4CREEP PROPERTIES OF CAST IRONS4.4 Growth of Cast IronGrowth in irons is generally defined as the permanent increase in volume which occursafter prolonged exposure to constant elevated temperatures or after repeated heating

34、and cooling.The mechanism of growth is rather complex in irons owing to the fact that it results from several different andindependent phenomena; which phenomena occur in any given case is dependent upon the temperatureinvolved, the environment, the chemical composition and structure of the iron, an

35、d the severity of cycling, if any.The main phenomena which cause growth in irons at temperature are as follows:1. Oxidation: This may progress into the body of an iron along graphite flakes or cracks, resulting in agreater dimensional change than in materials where oxidation is limited to the surfac

36、es.2. Graphitization: If the iron has carbides in its structure and is heated to a temperature which willdecompose the carbide structures (this temperature will vary considerably with chemistry), theresulting ferrite and graphite will occupy considerably greater volume than the original carbide.3. C

37、razing or Thermal Cracking: When an iron is repeatedly heated and cooled through a transformationrange, the stresses, imposed by the expansion and contraction resulting from the transformation, willcause crazing.Ductile and malleable irons are less affected by oxidation than gray iron. Some investig

38、ators have indicatedthat this difference is a result of graphite carbon shapes. Alloyed irons are usually less susceptible to growth,and this can either be due to an increased stability of the structure at the temperature involved, improvedoxidation resistance, or a change of the critical temperatur

39、e so the part does not experience a transformation inthe temperature range. Examples of the growth experienced by some common SAE irons are shown in Figure5.COPYRIGHT Society of Automotive Engineers, Inc.Licensed by Information Handling ServicesSAE J125 Reaffirmed MAY88-6-FIGURE 5CAST IRON GROWTH AT

40、 1000 F4.5 Endurance LimitRelatively little data are available on the endurance limit of cast irons at elevatedtemperatures. The curves in Figure 6 show the relationship between the tensile strength and the endurancelimit of a low carbon equivalent low alloy gray cast iron up to a temperature of 110

41、0 F. It can be seen that theendurance ratio is nearly constant from room temperature to 1100 F for this iron. It is probable that for mostgray cast irons heated in air, the endurance ratio would remain nearly constant up to a temperature at whichchanges occur in the structure or severe oxidation tak

42、es place. A second set of curves for an austenitic grayiron are included in Figure 6. This shows how the endurance limit is affected by structure.FIGURE 6EFFECT OF TEMPERATURE ON STRENGTH AND ENDURANCE LIMITCOPYRIGHT Society of Automotive Engineers, Inc.Licensed by Information Handling ServicesSAE J

43、125 Reaffirmed MAY88-7-5. Effect of Temperature on Physical Properties5.1 Modulus of ElasticityThe modulus of elasticity at room temperature varies considerably for the varioustypes of iron. It is difficult to give representative figures; but, in general, it can be said that the cast irons do notsho

44、w a marked drop in modulus up to 800 F.5.2 Specific Heatof ferritic malleable iron:The specific heat of pearlitic malleable iron is substantially the same as that of ferritic malleable.In gray cast iron the specific heat varies with the temperature and the structure; therefore, a temperature rangewh

45、ich causes a change in microstructure may result in a reversal in the specific heat versus temperature curvewhich will result in a curve such as Figure 7. A commonly used figure for average cast irons is 0.13 cal/g-C.FIGURE 7SPECIFIC HEAT VERSUS TEMPERATURE FOR A GRAY CAST IRON (4)5.3 Thermal Conduc

46、tivityThe thermal conductivity of gray cast iron varies considerably with both temperatureand composition. Most plain and alloy gray irons will have a thermal conductivity of 0.10 to 0.135 cal-cm/s-cm2-C at 100 C and this will drop to about 0.09-0.115 cal-cm/s-cm2C at 400 C. Some specific cases areg

47、iven in the following table:Temperature Range Mean Specific HeatF C Btu/lb-F Cal/g-C70- 210 20-100 0.122 0.12270- 570 20-300 0.128 0.12870- 750 20-400 0.139 0.13970-1300 20-700 0.159 0.159COPYRIGHT Society of Automotive Engineers, Inc.Licensed by Information Handling ServicesSAE J125 Reaffirmed MAY8

48、8-8-Malleable iron has a thermal conductivity of about 0.151 cal-cm/s-cm2-C at 100 C (437.9 Btu-in/h-ft2-F at212 F) and 0.139 cal-cm/s-cm2-C at 400 C (403.1 Btu-in/h-ft2-F at 750 F).Ductile cast iron has the following conductivity.5.4 Average Coefficient of ExpansionThe coefficient of expansion of c

49、ast irons varies with temperature, andto a lesser degree with alloy content and structure or heat treatment. The following table gives valuescommonly used:6. Bibliography1. “Mechanical Properties of Metals and Alloys.“ U.S. Dept. of Commerce Circular C-447, NationalBureau of Standards, 1943.2. Kattus and McPherson, “Properties of Cast Iron at Elevated Temperatures.“ ASTM Special TechnicalPublication No. 248.3. Malleable Iron Casting Handbook. Malleable Founders Soci