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本文(ASTM A579 A579M-2004a(2009) Standard Specification for Superstrength Alloy Steel Forgings《超高强度合金钢锻件的标准规范》.pdf)为本站会员(李朗)主动上传,麦多课文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文库(发送邮件至master@mydoc123.com或直接QQ联系客服),我们立即给予删除!

ASTM A579 A579M-2004a(2009) Standard Specification for Superstrength Alloy Steel Forgings《超高强度合金钢锻件的标准规范》.pdf

1、Designation: A 579/A 579M 04a (Reapproved 2009)Standard Specification forSuperstrength Alloy Steel Forgings1This standard is issued under the fixed designation A 579/A 579M; the number immediately following the designation indicates the yearof original adoption or, in the case of revision, the year

2、of last revision. A number in parentheses indicates the year of last reapproval.A superscript epsilon () indicates an editorial change since the last revision or reapproval.1. Scope1.1 This specification covers requirements for forged steelshapes for highly stressed structural members requiring yiel

3、dstrengths in excess of 140 ksi 965 MPa.1.2 This specification is not intended for applications lim-ited by creep deformation.1.3 Twenty-seven grades are covered by this specification.Selection will depend upon design, service conditions, andmechanical properties required.1.4 Supplementary requireme

4、nts are provided for use whenadditional testing or inspection is desired. These shall applyonly when specified individually by the purchaser in the order.1.5 The values stated in either SI units or inch-pound unitsare to be regarded separately as standard. The values stated ineach system may not be

5、exact equivalents; therefore, eachsystem shall be used independently of the other. Combiningvalues from the two systems may result in non-conformancewith the standard.1.6 Unless the order specifies the applicable “M” specifica-tion designation, the material shall be furnished to the inch-pound units

6、.2. Referenced Documents2.1 ASTM Standards:2A 255 Test Methods for Determining Hardenability of SteelA 275/A 275M Practice for Magnetic Particle Examinationof Steel ForgingsA 370 Test Methods and Definitions for Mechanical Testingof Steel ProductsA 388/A 388M Practice for Ultrasonic Examination ofSt

7、eel ForgingsA 788/A 788M Specification for Steel Forgings, GeneralRequirementsE3 Guide for Preparation of Metallographic SpecimensE21 Test Methods for Elevated Temperature Tension Testsof Metallic MaterialsE45 Test Methods for Determining the Inclusion Contentof SteelE112 Test Methods for Determinin

8、g Average Grain SizeE 165 Test Method for Liquid Penetrant Examination3. Ordering Information and General Requirements3.1 In addition to the ordering information required bySpecification A 788/A 788M, the purchaser shall include withthe inquiry and order a detailed drawing, sketch, or writtendescrip

9、tion of the forging.3.2 Material supplied to this specification shall conform tothe requirements of Specification A 788/A 788M, which out-lines additional ordering information, manufacturing require-ments, testing and retesting methods and procedures, marking,certification, product analysis variatio

10、ns, and additional supple-mentary requirements.3.3 If the requirements of this specification are in conflictwith the requirements of Specification A 788/A 788M, therequirements of this specification shall prevail.4. Materials and Manufacture4.1 The steel shall be made in accordance with the MeltingP

11、rocess Section of Specification A 788/A 788M. A sufficientdiscard shall be made to secure freedom from injurious pipeand undue segregation.4.2 The material shall be forged as close as practical to thespecified shape and size.4.3 The finished product shall be a hot-worked forging asdefined by Specifi

12、cation A 788/A 788M.4.4 Heat Treatment Performed by Forging SupplierForgings may be furnished in one of the following conditionsas specified in the inquiry and purchase order (some conditionsare not applicable to all grades):4.4.1 Stress relieved,4.4.2 Annealed,4.4.3 Solution treated,1This specifica

13、tion is under the jurisdiction of ASTM Committee A01 on Steel,Stainless Steel and Related Alloys and is the direct responsibility of SubcommitteeA01.06 on Steel Forgings and Billets.Current edition approved April 1, 2009. Published April 2009. Originallyapproved in 1967. Last previous edition approv

14、ed in 2004 as A 579/A 579M 04a.2For referenced ASTM standards, visit the ASTM 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.1Copyright ASTM International,

15、 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.4.4.4 Solution treated and aged,4.4.5 Normalized,4.4.6 Normalized and tempered, or4.4.7 Quenched and tempered.4.5 Heat Treatment Performed by PurchaserWhen finalheat treatment is to be performed by the purchaser aft

16、ermachining or fabrication, or both, a capability heat treatmentduplicating the purchasers final heat treatment must be per-formed by the supplier on representative samples (see 6.3)toqualify the forgings. The results of these capability tests shallconform to the requirements of Table 1 and Table 2.

17、 See alsoTable 3.5. Chemical Requirements Chemical Requirements5.1 Heat AnalysisThe heat analysis obtained from sam-pling in accordance with Specification A 788/A 788M shallcomply with Table 4.5.2 Product AnalysisThe product analysis provisions ofSpecification A 788/A 788M may be used by the purchas

18、er.6. Mechanical Properties6.1 The material shall conform to the mechanical propertiesspecified in Table 1, when ordered to 4.4.4 or 4.4.7. For theother heat treatments specified in 4.4, the provisions of 4.5apply.TABLE 1 Minimum Tension Test RequirementsGrade Yield Strength(0.2 % offset),ksi MPaTen

19、sile Strength,ksi MPaElongationA,%Reductionof AreaA,%Quench and Tempered13, 21, 22, 23, 12, 12a 140 965 150 1035 13 4013, 21, 22, 23, 11 160 1100 175 1210 12 3613, 21, 22, 23, 31 180 1240B190 1310 10 3213, 21, 22, 23 200 1380B210 1450 9 2822C, 23, 32, 33 225 1550B250 1720 6 25Air Hardening41 200 138

20、0B260 1790 9 3041 225 1550B280 1930 8 25Martensitic Stainless51, 52, 53 140 965 175 1210 12 4552 160 1100 220 1520 10 40No. 1 Precipitation Hardening Stainless61 140 965 165 1140 12 5061 160 1100 180 1240 10 4561 180 1240B200 1380 8 40No. 2 Precipitation Hardening Stainless64 140 965 165(1140 12 256

21、4 160 1100 185 1275 10 2564 180 1240B210 1450 10 25No. 3 Precipitation Hardening Stainless62 140 965 165 1140 6 2562, 63 160 1100 180 1240 6 2563 180 1240B200 1380 6 2563 200 1380B225 1550 5 25Maraging Steels74 160 1100 170 1170 15 6575 180 1240B190 1310 14 6071 200 1380B210 1450 12 5572 250 1720B25

22、5 1760 10 4573 275 1895B280 1930 9 40Miscellaneous81 180 1240D190 1310 13 4582 200 1380D210 1450 10 3083D225 1550D260 1790 7 2083E250 1720D280 1930 4 1584 180 1240D185 1275 14 45ASee Note in Table 3.BVacuum melting normally required to achieve list properties.CBy agreement.DBainitic.EMartensitic.A 5

23、79/A 579M 04a (2009)2TABLE 2 Minimum Room-Temperature Charpy V-Notch Energy AbsorptionAfor Respective Yield Strength Classes, ftlbf JGrade Yield Strength Class, ksi MPa1409651601100180B1240200B1380225B1550250B1720275B190011 . 4560 . . . . .12,12a 5070 . . . . . .13 20 25 10 15C. . . .21 35 45 30 40

24、20 25 15 20 . . . . . . . . .22 30 40 25 35 20 25 15 20 . . . . . . . . .23 35 45 25 35 20 25 15 20 10 15 . . . . . .31 . . 2535 . . . .32 . . . . 1217 . .33 . . . . 1520 . .41 . . . 1520C. .51 1520 . . . . . .52CC. . . . .53C. . . . . .61 25 35 . . .C. . . .62CC. . . . .63CCC. . . .64 25 35 15 20 1

25、5 20 . . . . . . . . . . . .71 . . . 3545 . . .72 . . . . . 2025 .73 . . . . . . 152074 . 6080 5070 . . . .81 . . 2535 . . . .82 . . . 2025 . . .83 . . . . 1520 1015 .84 . . 2535 . . . .ASee Note in Table 3.BVacuum melting may be required to achieve listed properties.CBy agreement.TABLE 3 Material,

26、Maximum Annealed Hardness (HB), and Section Size Capability in Inches mm forRespective Yield Strength ClassesNOTETables 1-3 show grades and maximum section sizes in which the indicated yield strength levels can usually be achieved at a 1/4 thickness depthin the direction of maximum working. Because

27、of variations in forging configuration and processing it does not follow that the ductility and impactstrengths listed in Table 1 and Table 2 can always be obtained at these depths. The properties listed are minimums, unless otherwise agreed by purchaserand manufacturer.Grade MaximumAnnealedHardness

28、(HB)Yield Strength Class, ksi MPa14096516011001801240200138022515502501720275190011 321 . . . 6.5 165 . . . . . . . . . . . . . . .12, 12a . . . 4.0 100 . . . . . . . . . . . . . . . . . .13 229 1.0 25 1.0 25 1.0 25 . . . . . . . . . . . .21 285 4.5 115 4.5 115 4.0 100 4.0 100 . . . . . . . . .22 30

29、2 4.5 115 4.5 115 4.0 100 4.0 100 3.5 90 . . . . . .23 302 8.0 200 8.0 200 8.0 200 8.0 200 8.0 200 . . . . . .31 262 . . 3.075 . . . .32 302 . . . . . . . . . . . . 5.5 140 . . . . . .33 302 . . . . 2.050 . .41 235 . . . . . . . . . 6.0 150 6.0 150 . . . . . .51 197 2.050 . . . . . .52 255 2.0 50 2.

30、0 50 . . . . . . . . . . . . . . .53 285 4.0 100 . . . . . . . . . . . . . . . . . .61 375 8.0 200 8.0 200 1.0 25 . . . . . . . . . . . .62 207 6.0 150 6.0 150 . . . . . . . . . . . . . . .63 241 . . . 6.0 150 6.0 150 6.0 150 . . . . . . . . .64 321 6.0 150 6.0 150 6.0 150 . . . . . . . . . . . .71

31、321 . . . . . . . . . 12.0 300 . . . . . . . . .72 321 . . . . . . . . . . . . . . . 12.0 300 . . .73 321 . . . . . . . . . . . . . . . . . . 12.0 30074 321 . . . 12.0 300 . . . . . . . . . . . . . . .75 321 . . . . . . 12.0 300 . . . . . . . . . . . .81 341 . . . . . . 6.0 150 . . . . . . . . . . .

32、 .82 341 . . . . . . . . . 5.0 125 . . . . . . . . .83 341 . . . . . . . . . . . . 3.0 75 3.0 75 . . .84 341 . . . . . . 6.0 150 . . . . . . . . . . . .A 579/A 579M 04a (2009)36.2 Tension tests are required for all material ordered to thisspecification. However, room-temperature Charpy V-notch im-pa

33、ct tests are required only for those grades which haveminimum impact strength requirements listed in Table 2.6.3 Tests shall be conducted in accordance with the latestissue of Test Methods and Definitions A 370. The largestobtainable tension test specimen as specified in Test Methodsand Definitions

34、A 370 shall be used. Impact specimens shall bethe standard size, Charpy V-notch, as shown in the figure forthe Charpy (Simple-Beam) Impact Test of Test Methods andDefinitions A 370. The use of subsize impact specimensrequires prior purchaser approval.6.4 The longitudinal axis of the specimens shall

35、be parallelto the direction of major working of the forging. For upset-discTABLE 4 Chemical RequirementsElements Composition, %min max min max min max min max min max min max min maxGrade 11 12 12a 13 21 22 23Carbon 0.23 0.28 . . . 0.12 . . . 0.20 0.27 0.33 0.31 0.38 0.38 0.43 0.45 0.50Manganese . .

36、 . 0.20 0.60 0.90 0.60 0.90 0.40 0.60 0.60 0.90 0.60 0.90 0.60 0.90Phosphorus . . . 0.01 . . . 0.010 . . . 0.015 . . . 0.025 . . . 0.025 . . . 0.025 . . . 0.015Sulfur . . . 0.01 . . . 0.010 . . . 0.015 . . . 0.025 . . . 0.025 . . . 0.025 . . . 0.015Silicon . . . 0.10 0.20 0.35 0.20 0.35 0.20 0.35 0.

37、20 0.35 0.20 0.35 0.15 0.30Nickel 2.75 3.25 4.75 5.25 4.75 5.25 . . . . . . 1.65 2.00 1.65 2.00 0.40 0.70Chromium 1.40 1.65 0.40 0.70 0.40 0.70 0.80 1.10 0.65 0.90 0.70 0.90 0.90 1.20Molybdenum 0.8 1.0 0.30 0.65 0.30 0.65 0.15 0.25 0.30 0.60 0.30 0.60 0.90 1.10Vanadium . . . . . . 0.05 0.10 0.05 0.1

38、0 0.05 0.10 0.17 0.23 0.05 0.10 0.08 0.15Columbium 0.03 0.07 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Grade 31 32 33 41 51 52 53ACarbon 0.23 0.28 0.40 0.45 0.41 0.46 0.38 0.43 . . . 0.15 0.20 0.25 . . . 0.20Manganese 1.20 1.50 0.65 0.90 0.75 1.00 0.20 0.40 . . . 1.00 0.

39、50 1.00 . . . 1.00Phosphorus . . . 0.025 . . . 0.025 . . . 0.025 . . . 0.015 . . . 0.025 . . . 0.025 . . . 0.025Sulfur . . . 0.025 . . . 0.025 . . . 0.025 . . . 0.015 . . . 0.025 . . . 0.025 . . . 0.025Silicon 1.30 1.70 1.45 1.80 1.40 1.75 0.80 1.00 . . . 1.00 . . . 0.50 . . . 1.00Nickel 1.65 2.00 1

40、.65 2.00 . . . . . . . . . . . . . . . 0.75 0.50 1.00 1.25 2.50Chromium 0.20 0.40 0.65 0.90 1.90 2.25 4.75 5.25 11.5 13.5 11.0 12.5 15.0 17.0Molybdenum 0.35 0.45 0.30 0.45 0.45 0.60 1.20 1.40 . . . 0.50 0.90 1.25 . . . . . .Copper . . . . . . . . . . . . . . . . . . . . . . . . . . . 0.50 . . . . .

41、. . . . . . .Titanium . . . . . . . . . . . 0.05 . .Vanadium . . . . . . . . . . . . 0.03 0.08 0.40 0.60 . . . . . . 0.20 0.30 . . . . . .Cobalt . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0.25 . . . . . .Aluminum . . . . . . . . . 0.05 . 0.05 . .Tungsten . . . . . . . . . . .

42、. . . . . . . . . . . . . . . . . . . 0.90 1.25 . . . . . .Tin . . . . . . . . . 0.05 . 0.04 . .Grade 61A,B62A,B63A,B64A,B71A,B72A,B73A,BCarbon . . . 0.07 . . . 0.09 . . . 0.09 0.10 0.15 . . . 0.03 . . . 0.03 . . . 0.03Manganese . . . 1.00 . . . 1.00 . . . 1.00 0.50 1.25 . . . 0.10 . . . 0.10 . . .

43、0.10Phosphorus . . . 0.025 . . . 0.025 . . . 0.025 . . . 0.025 . . . 0.01 . . . 0.01 . . . 0.01Sulfur . . . 0.025 . . . 0.025 . . . 0.025 . . . 0.025 . . . 0.01 . . . 0.01 . . . 0.01Silicon . . . 1.00 . . . 1.00 . . . 0.50 . . . 0.50 . . . 0.10 . . . 0.10 . . . 0.10Nickel 3.0 5.0 6.5 7.75 6.5 7.75 4

44、.0 5.0 17.0 19.0 17.0 19.0 18.0 19.0Chromium 15.5 17.5 16.0 18.0 14.0 15.25 15.0 16.0 . . . . . . . . . . . . . . . . . .Molybdenum . . . . . . . . . . . . 2.0 2.75 2.50 3.25 3.0 3.5 4.6 5.2 4.6 5.2Copper 3.0 5.0 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Titanium . . . .

45、 . . . . . . . . . . . . . . . . . . . . 0.15 0.25 0.30 0.50 0.50 0.80Columbium 0.15 0.45 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Cobalt . . . . . . . . . . . . . . . . . . . . . . . . 8.0 9.0 7.0 8.5 8.5 9.5Aluminum . . . . . . 0.75 1.50 0.75 1.25 . . . . . . 0.05 0.1

46、5 0.05 0.15 0.05 0.15Nitrogen . . . . . . . . . . . . . . . . . . 0.07 0.13 . . . . . . . . . . . . . . . . . .Grade 74A,B75A,B81A,B82A,B83A,B84A,BCarbon . . . 0.03 . . . 0.03 0.24 0.30 0.28 0.34 0.42 0.47 0.16 0.23Manganese . . . 0.10 . . . 0.10 0.10 0.35 0.10 0.35 0.10 0.35 0.20 0.40Phosphorus . .

47、 . 0.01 . . . 0.01 . . . 0.01 . . . 0.01 . . . 0.01 . . . 0.010Sulfur . . . 0.01 . . . 0.01 . . . 0.01 . . . 0.01 . . . 0.01 . . . 0.005Silicon . . . 0.12 . . . 0.12 . . . 0.10 . . . 0.10 . . . 0.10 . . . 0.20Nickel 11.5 12.5 11.5 12.5 7.0 9.0 7.0 8.5 7.0 8.5 8.5 9.5Chromium 4.75 5.25 4.75 5.25 0.35

48、 0.60 0.90 1.10 0.20 0.35 0.65 0.85Molybdenum 2.75 3.25 2.75 3.25 0.35 0.60 0.90 1.10 0.20 0.35 0.95 1.10Titanium 0.05 0.15 0.10 0.25 . . . . . . . .Vanadium . . . . . . . . . . . . 0.06 0.12 0.06 0.12 0.06 0.12 0.06 0.15Cobalt . . . . . . . . . . . . 3.5 4.5 4.0 5.0 3.5 4.5 4.25 4.75Aluminum 0.25 0.40 0.35 0.50 . . . . . . . . . . . . . . . . . . . . . 0.020AProduct analysis of sulfur and phosphorus shall conform to the requirements of Table 4.B0.06 calcium, 0.003 boron, and 0.02 zirconium may be added.A 579/A 579M 04a (2009)4forgings, the lon

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