ASTM A743 A743M-2013a Standard Specification for Castings Iron-Chromium Iron-Chromium-Nickel Corrosion Resistant for General Application《一般应用耐腐蚀铬铁及镍铬铁合金铸件的标准规格》.pdf

上传人:eastlab115 文档编号:459368 上传时间:2018-11-25 格式:PDF 页数:8 大小:75.90KB
下载 相关 举报
ASTM A743 A743M-2013a Standard Specification for Castings Iron-Chromium Iron-Chromium-Nickel Corrosion Resistant for General Application《一般应用耐腐蚀铬铁及镍铬铁合金铸件的标准规格》.pdf_第1页
第1页 / 共8页
ASTM A743 A743M-2013a Standard Specification for Castings Iron-Chromium Iron-Chromium-Nickel Corrosion Resistant for General Application《一般应用耐腐蚀铬铁及镍铬铁合金铸件的标准规格》.pdf_第2页
第2页 / 共8页
ASTM A743 A743M-2013a Standard Specification for Castings Iron-Chromium Iron-Chromium-Nickel Corrosion Resistant for General Application《一般应用耐腐蚀铬铁及镍铬铁合金铸件的标准规格》.pdf_第3页
第3页 / 共8页
ASTM A743 A743M-2013a Standard Specification for Castings Iron-Chromium Iron-Chromium-Nickel Corrosion Resistant for General Application《一般应用耐腐蚀铬铁及镍铬铁合金铸件的标准规格》.pdf_第4页
第4页 / 共8页
ASTM A743 A743M-2013a Standard Specification for Castings Iron-Chromium Iron-Chromium-Nickel Corrosion Resistant for General Application《一般应用耐腐蚀铬铁及镍铬铁合金铸件的标准规格》.pdf_第5页
第5页 / 共8页
亲,该文档总共8页,到这儿已超出免费预览范围,如果喜欢就下载吧!
资源描述

1、Designation: A743/A743M 13A743/A743M 13aStandard Specification forCastings, Iron-Chromium, Iron-Chromium-Nickel, CorrosionResistant, for General Application1This standard is issued under the fixed designation A743/A743M; the number immediately following the designation indicates the yearof original

2、adoption or, in the case of revision, the year 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.This standard has been approved for use by agencies of the Department of Defense

3、.1. Scope*1.1 This specification covers iron-chromium and iron-chromium-nickel alloy castings for general corrosion-resistant applica-tion. The grades covered by this specification represent types of alloy castings suitable for broad ranges of application which areintended for a wide variety of corr

4、osion environments.NOTE 1For alloy castings for severe corrosion-resistant service, reference should be made to Specification A744/A744M. For general heat-resistantalloy castings, reference should be made to Specification A297/A297M. For nickel alloy castings for corrosion-resistant service, referen

5、ce should be madeto Specification A494/A494M.1.2 The values stated in either inch-pound units or SI units are to be regarded separately as standard. Within the text, the SI unitsare shown in brackets. The values stated in each system are not exact equivalents; therefore, each system must be usedinde

6、pendently of the other. Combining values from the two systems may result in nonconformance with the specification.Inch-pound units are applicable for material ordered to Specification A743 and SI units for material ordered to SpecificationA743M.2. Referenced Documents2.1 ASTM Standards:2A262 Practic

7、es for Detecting Susceptibility to Intergranular Attack in Austenitic Stainless SteelsA297/A297M Specification for Steel Castings, Iron-Chromium and Iron-Chromium-Nickel, Heat Resistant, for GeneralApplicationA370 Test Methods and Definitions for Mechanical Testing of Steel ProductsA494/A494M Specif

8、ication for Castings, Nickel and Nickel AlloyA744/A744M Specification for Castings, Iron-Chromium-Nickel, Corrosion Resistant, for Severe ServiceA781/A781M Specification for Castings, Steel and Alloy, Common Requirements, for General Industrial UseA890/A890M Specification for Castings, Iron-Chromium

9、-Nickel-Molybdenum Corrosion-Resistant, Duplex (Austenitic/Ferritic) for General ApplicationA957 Specification for Investment Castings, Steel and Alloy, Common Requirements, for General Industrial Use3. General Conditions for Delivery3.1 Except for investment castings, castings furnished to this spe

10、cification shall conform to the requirements of SpecificationA781/A781M, including any supplementary requirements that are indicated on the purchase order. Failure to comply with thegeneral requirements of Specification A781/A781M constitutes nonconformance with this specification. In case of confli

11、ct betweenthe requirements of this specification and Specification A781/A781M, this specification shall prevail.3.2 Steel investment castings furnished to this specification shall conform to the requirements of Specification A957, includingany supplementary requirements that are indicated in the pur

12、chase order. Failure to comply with the general requirements ofSpecification A957 constitutes nonconformance with this specification. In case of conflict between the requirements of thisspecification and Specification A957, Specification A957 shall prevail.1 This specification is under the jurisdict

13、ion ofASTM Committee A01 on Steel, Stainless Steel and RelatedAlloys and is the direct responsibility of Subcommittee A01.18on Castings.Current edition approved May 1, 2013May 15, 2013. Published May 2013June 2013. Originally approved in 1977. Last previous edition approved in 20122013 asA743/A743M

14、12.A743/A743M 13. DOI: 10.1520/A0743_A0743M-13.10.1520/A0743_A0743M-13A.2 For referencedASTM standards, visit theASTM website, www.astm.org, or contactASTM Customer Service at serviceastm.org. For Annual Book of ASTM Standardsvolume information, refer to the standards Document Summary page on the AS

15、TM website.This document is not an ASTM standard and is intended only to provide the user of an ASTM standard an indication of what changes have been made to the previous version. Becauseit may not be technically possible to adequately depict all changes accurately, ASTM recommends that users consul

16、t prior editions as appropriate. In all cases only the current versionof the standard as published by ASTM is to be considered the official document.*A Summary of Changes section appears at the end of this standardCopyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, P

17、A 19428-2959. United States14. Ordering Information4.1 Orders for material to this specification should include the following, as required, to describe the material adequately:4.1.1 Description of the casting by pattern number or drawing,4.1.2 Grade,4.1.3 Heat treatment,4.1.4 Options in the specific

18、ation,4.1.5 Whether castings are to be produced using the investment casting process, and4.1.6 Supplementary requirements desired, including the standards of acceptance.5. Process5.1 The steel shall be made by the electric furnace process with or without separate refining such as argon-oxygendecarbu

19、rization (AOD).6. Heat Treatment6.1 Castings shall be heat treated in accordance with the requirements in Table 1.NOTE 2Proper heat treatment of these alloys is usually necessary to enhance corrosion resistance and in some cases to meet mechanical properties.Minimum heat treat temperatures are speci

20、fied; however, it is sometimes necessary to heat treat at higher temperatures, hold for some minimum time attemperature and then rapidly cool the castings in order to enhance the corrosion resistance and meet mechanical properties.TABLE 1 Heat Treatment RequirementsGrade Heat TreatmentCA6N Heat to 1

21、900F 1040C, air cool, reheat to 1500F 815C, air cool, and age at 800F 425C, holding at eachtemperature sufficient time to heat casting uniformly to temperature.CA6NM Heat to 1850F 1010C minimum, air cool to 200F 95C or lower prior to any optional intermediate temper andprior to the final temper. The

22、 final temper shall be between 1050F 565C and 1150F 620C.CA15, CA15M, CA40, CA40F (1) Heat to 1750F 955C minimum, air cool and temper at 1100F 595C minimum, or(2) Anneal at 1450F 790C minimum.CA28MWV (1) Heat to 18751925F 10251050C, quench in air or oil, and temper at 1150F 620C minimum, or(2) Annea

23、l at 1400F 760C minimum.CB30, CC50 (1) Heat to 1450F 790C minimum, and air cool, or(2) Heat to 1450F 790C minimum, and furnace cool.CB6 Heat between 1800F 980C and 1920F 1050C, forced air, cool to 120F 50C maximum, and temperbetween 1100F and 1160F 595C and 625C.CE30, CH10, CH20, CK20 Heat to 2000F

24、1093C minimum, hold for sufficient time to heat casting to temperature, quench in water or rapidcool by other means.CF3, CF3M, CF3MN (1) Heat to 1900F 1040C minimum, hold for sufficient time to heat casting to temperature, quench in water orrapid cool by other means.(2) As cast if corrosion resistan

25、ce is acceptable.CF8, CF8C, CF8M, CF16F, CF16Fa,CF20, CG3M, CG8M, CG12Heat to 1900F 1040C minimum, hold for sufficient time to heat casting to temperature, quench in water or rapidcool by other means.CF10SMnN Heat to 1950F 1065C minimum, hold for sufficient time to heat casting to temperature, quenc

26、h in water or rapidcool by other means.CG6MMN, CN7M Heat to 2050F 1120C minimum, hold for sufficient time to heat casting to temperature, quench in water or rapidcool by other means.CK3MCuN Heat to 2100F 1150C minimum, hold for sufficient time to heat casting to temperature, quench in water or rapid

27、cool by other means.CK3MCuN, CK35MN, CN3M, CN3MN Heat to 2200F 1200C minimum, hold for 4 hours minimum, quench in water or rapid cool by other means.CK35MN Heat to 2100-2190F 1150-1200C, hold for sufficient time to heat casting to temperature, quench in water or rapidcool by other means.CN3M Heat to

28、 2150F 1175C minimum, hold for sufficient time to heat casting to temperature, quench in water or rapidcool by other means.CN3MN Heat to 2100F 1150C minimum, hold for sufficient time to heat casting to temperature, quench in water or rapidcool by other means.CG6MMN, CN7M Heat to 2050F 1120C minimum,

29、 hold for sufficient time to heat casting to temperature, quench in water or rapidcool by other means.CN7MS Heat to 2100F 1150C minimum, 2150F 1180C maximum, hold for sufficient time (2 h minimum) to heatcasting to temperature and quench in water.HG10MNN As-castA743/A743M 13a27. Chemical Requirement

30、s7.1 The chemical requirements are shown in Table 2.TABLE 2 Chemical RequirementsGrade(UNS) TypeComposition, %Carbon,maxMan-ganese,maxSilicon,maxPhospho-rus, maxSulfur,max Chromium NickelMolybde-numColum-biumSele-nium CopperTung-sten,maxVana-dium,maxNitrogenCA6N 11 Chromium, 0.06 0.50 1.00 0.02 0.02

31、 10.512.5 6.0 . . . . . . .7 Nickel 8.0CA6NM(J91540)12 Chromium,4 Nickel0.06 1.00 1.00 0.04 0.03 11.514.0 3.54.50.401.0 . . . . . .CA15(J91150)12 Chromium 0.15 1.00 1.50 0.04 0.04 11.514.0 1.00max0.50 max . . . . . .CA15M(J91151)12 Chromium 0.15 1.00 0.65 0.040 0.040 11.514.0 1.0max0.151.0 . . . . .

32、 .CA28MWV(J91422)12 Chromium, withMolybdenum,Tungsten andVanadium0.200.280.501.001.0 0.030 0.030 11.012.5 0.501.000.901.25 . . . 0.901.250.200.30.CA40(J91153)12 Chromium 0.200.401.00 1.50 0.04 0.04 11.514.0 1.0max0.5 max . . . . . .CA40F(J91154)12 Chromium,Free Machining0.200.401.00 1.50 0.04 0.200.

33、4011.514.0 1.0max0.5 max . . . . . .CB6(J91804)16 Chromium,4 Nickel0.06 1.00 1.00 0.04 0.03 15.517.5 3.55.5 0.5 max . . . . . . . . . . . . . . . . . .CB30(J91803)20 Chromium 0.30 1.00 1.50 0.04 0.04 18.021.0 2.00max. . . B . . .CC50(J92615)28 Chromium 0.50 1.00 1.50 0.04 0.04 26.030.0 4.00max. . .

34、. . . .CE30(J93423)29 Chromium,9 Nickel0.30 1.50 2.00 0.04 0.04 26.030.0 8.011.0. . . . . . .CF3(J92500)19 Chromium,9 Nickel0.03 1.50 2.00 0.04 0.04 17.021.0 8.012.0. . . . . . .CF3M(J92800)19 Chromium,10 Nickel, withMolybdenum0.03 1.50 1.50 0.04 0.04 17.021.0 9.013.02.03.0 . . . . . .CF3MN(J92804)1

35、9 Chromium,10 Nickel, withMolybdenum, andNitrogen0.03 1.50 1.50 0.040 0.040 17.022.0 9.013.02.03.0 . . . . . 0.100.20CF8(J92600)19 Chromium,9 Nickel0.08 1.50 2.00 0.04 0.04 18.021.0 8.011.0. . . . . . .CF8C(J92710)19 Chromium,10 Nickel, withColumbium0.08 1.50 2.00 0.04 0.04 18.021.0 9.012.0. A . . .

36、 . .CF8M(J92900)19 Chromium,10 Nickel, withMolybdenum0.08 1.50 2.00 0.04 0.04 18.021.0 9.012.02.03.0 . . . . . .CF10SMnN(J92972)17 Chromium, 8.5Nickel withNitrogen0.10 7.009.003.504.500.060 0.030 16.018.0 8.09.0. . . . . . 0.080.18CF16F(J92701)19 Chromium,9 Nickel, FreeMachining0.16 1.50 2.00 0.17 0

37、.04 18.021.0 9.012.01.50 max . 0.200.35. . . .CF16Fa 19 Chromium,9 Nickel, FreeMachining0.16 1.50 2.00 0.04 0.200.4018.021.0 9.012.00.400.80 . . . . . .CF20(J92602)19 Chromium,9 Nickel0.20 1.50 2.00 0.04 0.04 18.021.0 8.011.0. . . . . . .CG3M(J92999)19 Chromium,11 Nickel, withMolybdenum0.03 1.50 1.5

38、0 0.04 0.04 18.021.0 9.013.03.04.0 . . . . . . . . . . . . . . . . . .CG6MMN(J93790)0.06 4.006.001.00 0.04 0.03 20.523.5 11.513.51.503.00 0.100.30. . . 0.100.300.200.40CG8M(J93000)19 Chromium,11 Nickel, withMolybdenum0.08 1.50 1.50 0.04 0.04 18.021.0 9.013.03.04.0 . . . . . .CG12(J93001)22 Chromium,

39、12 Nickel0.12 1.50 2.00 0.04 0.04 20.023.0 10.013.0. . . . . . .CH10(J93401)25 Chromium,12 Nickel0.10 1.50 2.00 0.04 0.04 22.026.0 12.015.0. . . . . . . . .CH20(J93402)25 Chromium,12 Nickel0.20 1.50 2.00 0.04 0.04 22.026.0 12.015.0. . . . . . .A743/A743M 13a3TABLE 2 ContinuedGrade(UNS) TypeCompositi

40、on, %Carbon,maxMan-ganese,maxSilicon,maxPhospho-rus, maxSulfur,max Chromium NickelMolybde-numColum-biumSele-nium CopperTung-sten,maxVana-dium,maxNitrogenCK35MN 23 Chromium, 21Nickel, withMolybdenum andNitrogen0.035 2.00 1.00 0.035 0.020 22.0-24.0 20.0-22.06.0-6.8 . . . . . . 0.40 . . . . . . 0.21-0.

41、32CK3MCuN(J93254)20 Chromium18 Nickel, withCopper andMolybdenum0.025 1.20 1.00 0.045 0.010 19.520.5 17.519.56.07.0 . . . . . . 0.501.00. . . . . . 0.1800.240CK20(J94202)25 Chromium,20 Nickel0.20 2.00 2.00 0.04 0.04 23.027.0 19.022.0. . . . . . .CN3M(J94652)0.03 2.0 1.0 0.03 0.03 20.022.0 23.027.04.5

42、5.5 . . . . . .CN3MN(J94651)21 Chromium,24 Nickel withMolybdenumand Nitrogen0.03 2.00 1.00 0.040 0.010 20.022.0 23.525.56.07.0 . . 0.75max. . 0.180.26CN7M(N08007)20 Chromium,29 Nickel, withCopper andMolybdenum0.07 1.50 1.50 0.04 0.04 19.022.0 27.530.52.03.0 . . 3.04.0. . .CN7MS(J94650)19 Chromium,24

43、 Nickel, withCopper andMolybdenum0.07 1.00 2.503.500.04 0.03 18.020.0 22.025.02.53.0 . . 1.52.0.HG10MNNJ9260419 Chromium,12 Nickel,4 Manganese0.070.113.05.00.70 0.040 0.030 18.5 20.511.513.50.250.45C . 0.50 . . 0.200.30A Grade CF8C shall have a columbium content of not less than eight times the carb

44、on content and not more than 1.0%. If a columbium-plus-tantalum alloy in theapproximate Cb:Ta ratio of 3:1 is used for stabilizing this grade, the total columbium-plus-tantalum content shall not be less than nine times the carbon content and shallnot exceed 1.1%.B For Grade CB30 a copper content of

45、0.90 to 1.20% is optional.C Grade HG10MNN shall have a columbium content of not less than eight times the carbon, but not over 1.00 %.8. Repair by Welding8.1 Repair welding of Grade CA28MWV is not permitted unless by agreement between the manufacturer and the purchaser.8.2 When methods involving hig

46、h temperature are used in the removal of discontinuities, castings shall be preheated inaccordance with Table 3. Weld repairs shall be subject to the same quality standards as are used to inspect the castings.8.3 Post weld heat treatment, if required, shall be in accordance with Table 1.8.3.1 The ma

47、rtensitic grades CA6NM, CA15, CA15M, CB6, and CA40 shall be retempered after weld repairing, except thatlocal tempering will be permitted if, in the opinion of the manufacturer, furnace heat treating will be damaging to the finishedsurface of a machined casting. Heat treatment, other than tempering,

48、 of grades CA6NM, CA15, CA15M, CB6, and CA40 afterweld repairing shall be performed only when agreed upon between the manufacturer and the purchaser. Weld repair on GradeCA40F is not recommended because of the risk of local hardening and possible cracking in the heat affected zone.8.3.2 Post weld he

49、at treatment is not required on the other grades of this specification.When post weld heat treatment is believednecessary for adequate corrosion resistance in the service environment, castings should be ordered in accordance with SpecificationA744/A744M.8.3.3 For Grade HG10MNN, the filler metal to be used shall be established by mutual agreement

展开阅读全文
相关资源
猜你喜欢
  • AECMA PREN 2275-1979 Steel FE-PA95 1750 MPa Less Than or Equal to Rm Less Than or Equal to 2000 MPa Forgings De Less Than or Equal to 150 mm Aerospace Series Edition 1《航空航天系列.钢 FE-.pdf AECMA PREN 2275-1979 Steel FE-PA95 1750 MPa Less Than or Equal to Rm Less Than or Equal to 2000 MPa Forgings De Less Than or Equal to 150 mm Aerospace Series Edition 1《航空航天系列.钢 FE-.pdf
  • AECMA PREN 2276-1979 Steel FE-PA95 1750 MPa Less Than or Equal to Rm Less Than or Equal to 2000 MPa Sheet and Plate a Less Than or Equal to 40 mm Aerospace Series Edition 1《航空航天系列..pdf AECMA PREN 2276-1979 Steel FE-PA95 1750 MPa Less Than or Equal to Rm Less Than or Equal to 2000 MPa Sheet and Plate a Less Than or Equal to 40 mm Aerospace Series Edition 1《航空航天系列..pdf
  • AECMA PREN 2278-1979 Steel FE-PM37 900 MPa Less Than or Equal to Rm Less Than or Equal to 1100 MPa Bars De Less Than or Equal to 150 mm Aerospace Series Edition 1《航空航天系列.钢 FE-PM37 .pdf AECMA PREN 2278-1979 Steel FE-PM37 900 MPa Less Than or Equal to Rm Less Than or Equal to 1100 MPa Bars De Less Than or Equal to 150 mm Aerospace Series Edition 1《航空航天系列.钢 FE-PM37 .pdf
  • AECMA PREN 2279-1979 Steel FE-PM37 900 MPa Less Than or Equal to Rm Less Than or Equal to 1100 MPa Forgings De Less Than or Equal to 150 mm Aerospace Series Edition 1《航空航天系列.钢 FE-P.pdf AECMA PREN 2279-1979 Steel FE-PM37 900 MPa Less Than or Equal to Rm Less Than or Equal to 1100 MPa Forgings De Less Than or Equal to 150 mm Aerospace Series Edition 1《航空航天系列.钢 FE-P.pdf
  • AECMA PREN 2280-1979 Steel FE-PM37 900 MPa Less Than or Equal to Rm Less Than or Equal to 1100 MPa Sheet a Less Than or Equal to 6 mm Aerospace Series Edition 1《航空航天系列.钢 FE-PM37 90.pdf AECMA PREN 2280-1979 Steel FE-PM37 900 MPa Less Than or Equal to Rm Less Than or Equal to 1100 MPa Sheet a Less Than or Equal to 6 mm Aerospace Series Edition 1《航空航天系列.钢 FE-PM37 90.pdf
  • AECMA PREN 2281-1979 Steel FE-PM42 900 MPa Less Than or Equal to Rm Less Than or Equal to 1100 MPa Forgings De Less Than or Equal to 100 mm Aerospace Series Edition 1《航空航天系列.钢 FE-P.pdf AECMA PREN 2281-1979 Steel FE-PM42 900 MPa Less Than or Equal to Rm Less Than or Equal to 1100 MPa Forgings De Less Than or Equal to 100 mm Aerospace Series Edition 1《航空航天系列.钢 FE-P.pdf
  • AECMA PREN 2282-2002 Aerospace Series Characteristics of Aircraft Electrical Supplies Edition P 1《航空航天系列.飞行器电源特性.P1版》.pdf AECMA PREN 2282-2002 Aerospace Series Characteristics of Aircraft Electrical Supplies Edition P 1《航空航天系列.飞行器电源特性.P1版》.pdf
  • AECMA PREN 2283-2009 Aerospace series Testing of aircraft wiring Edition P 1《航空航天系列.航空用布线测试.版本P1》.pdf AECMA PREN 2283-2009 Aerospace series Testing of aircraft wiring Edition P 1《航空航天系列.航空用布线测试.版本P1》.pdf
  • AECMA PREN 2285-2002 Aerospace Series Bushes Plain Aluminium Alloy with Self-Lubricating Liner Dimensions and Loads Edition P 1《航空航天系列.具有自润滑衬套的铝合金轴套规范.尺寸和负荷 P.第1版》.pdf AECMA PREN 2285-2002 Aerospace Series Bushes Plain Aluminium Alloy with Self-Lubricating Liner Dimensions and Loads Edition P 1《航空航天系列.具有自润滑衬套的铝合金轴套规范.尺寸和负荷 P.第1版》.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > ASTM

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1