ASTM B880-2003(2008) Standard Specification for General Requirements for Chemical Check Analysis Limits for Nickel Nickel Alloys and Cobalt Alloys《镍、镍合金及钴合金化学检验分析限值一般要求的标准规范》.pdf

上传人:syndromehi216 文档编号:462624 上传时间:2018-11-27 格式:PDF 页数:4 大小:58.78KB
下载 相关 举报
ASTM B880-2003(2008) Standard Specification for General Requirements for Chemical Check Analysis Limits for Nickel Nickel Alloys and Cobalt Alloys《镍、镍合金及钴合金化学检验分析限值一般要求的标准规范》.pdf_第1页
第1页 / 共4页
ASTM B880-2003(2008) Standard Specification for General Requirements for Chemical Check Analysis Limits for Nickel Nickel Alloys and Cobalt Alloys《镍、镍合金及钴合金化学检验分析限值一般要求的标准规范》.pdf_第2页
第2页 / 共4页
ASTM B880-2003(2008) Standard Specification for General Requirements for Chemical Check Analysis Limits for Nickel Nickel Alloys and Cobalt Alloys《镍、镍合金及钴合金化学检验分析限值一般要求的标准规范》.pdf_第3页
第3页 / 共4页
ASTM B880-2003(2008) Standard Specification for General Requirements for Chemical Check Analysis Limits for Nickel Nickel Alloys and Cobalt Alloys《镍、镍合金及钴合金化学检验分析限值一般要求的标准规范》.pdf_第4页
第4页 / 共4页
亲,该文档总共4页,全部预览完了,如果喜欢就下载吧!
资源描述

1、Designation: B 880 03 (Reapproved 2008)Standard Specification forGeneral Requirements for Chemical Check Analysis Limitsfor Nickel, Nickel Alloys and Cobalt Alloys1This standard is issued under the fixed designation B 880; the number immediately following the designation indicates the year oforigina

2、l adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. Asuperscript epsilon (e) indicates an editorial change since the last revision or reapproval.1. Scope1.1 This specification covers limits of variation for deter-mining ac

3、ceptability of the chemical composition of cast orwrought nickel, nickel alloy, and cobalt alloy parts and/ormaterial supplied by a producer. Check analysis limits forelements or for ranges of elements not currently listed hereinshall be as specified in the applicable material specification oras agr

4、eed upon by purchaser and supplier.1.2 In case of any conflicting requirements, the require-ments of the purchase order, the individual material specifica-tion, and this general specification shall prevail in the sequencenamed.1.3 When specifically referenced in the material specifica-tion, the buye

5、r may elect to apply check analysis limit todetermine acceptability at his final acceptance or verificationprocedures. Check analysis limits are not permitted or are to beused by the producer for their own ladle or ingot analysisacceptance testing.1.4 This standard does not purport to address all of

6、 thesafety concerns if any, associated with its use. It is theresponsibility of the user of this standard to become familiarwith all hazards including those identified in the appropriateMaterial Safety Data Sheet (MSDS) for this product/materialas provided by the manufacturer, to establish appropria

7、tesafety and health practices, and determine the applicability ofregulatory limitations prior to use.2. Referenced Documents2.1 ASTM Standards:2E55 Practice for Sampling Wrought Nonferrous Metals andAlloys for Determination of Chemical CompositionE88 Practice for Sampling Nonferrous Metals and Alloy

8、sin Cast Form for Determination of Chemical CompositionE 1473 Test Methods for Chemical Analysis of Nickel,Cobalt, and High-Temperature Alloys2.2 SAE Standards:AMS 2269 Chemical Check Analysis Limits Nickel, NickelAlloys and Cobalt alloys3. Terminology3.1 Definitions:3.1.1 check (product or verifica

9、tion) analysis, nanalysismade by buyer of parts and materials to verify conformity tospecification, or to determine variations in compositions withina heat or lot.3.1.1.1 DiscussionHeat or lot acceptance or rejection ofparts and materials may be made by applying check limits asdescribed in 3.1.2. Ch

10、eck limits of finished parts or material donot apply to elements whose percentage can be varied byfabricating techniques employed unless the sample is taken insuch a manner as to exclude such variations.3.1.2 variation limit, under minimum or over maximum,nit is the amount of variation for a specifi

11、ed element, whichmay vary either under or over the specified composition limitduring an individual check analysis.3.1.2.1 DiscussionIn no case shall the reported determi-nations of any element in a heat, using the same analyticalprocedure, vary both above and below the specified range.3.1.3 remainde

12、r or balance, nrefers to main element,which forms the basis of that particular alloy and from whichthe alloy is made.3.1.3.1 DiscussionIt is assumed to be present in anamount approximately equal to the difference between 100 %and the sum percentage of the alloying elements and listedimpurities or re

13、sidual elements. It need not be analyzed or needan actual percentage figure for reporting purposes.3.1.4 residual elements, each, maximum, nthe maximumamount of an individual element not mentioned specifically inthe specified composition, but which may be present, due topresence in starting raw mate

14、rials or manufacturing processes.3.1.4.1 DiscussionProducers will not normally analyzefor such elements, unless specifically asked for in the specifi-cation or purchase order.1This specification is under the jurisdiction of Committee B02 on NonferrousMetals and Alloys and is the direct responsibilit

15、y of Subcommittee B02.07 onRefined Nickel and Cobalt and Their Alloys.Current edition approved March 1, 2008. Published March 2008. Originallyapproved in 1998. Last previous edition approved in 2003 as B 880 - 03.2For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact ASTM Cu

16、stomer Service at serviceastm.org. For Annual Book of ASTMStandards volume information, refer to the standards Document Summary page onthe ASTM website.1Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.3.1.4.2 DiscussionReporting analy

17、ses of unspecified ele-ments is permitted.3.1.5 residual elements, total, maximum, nthe sum total ofthe residual elements (see 3.1.4) which may be possiblypresent.3.1.5.1 DiscussionIt is not inferred by this statement thatan analysis need be made for each element of the periodic tablenot mentioned s

18、pecifically in the composition section.4. Technical Requirements4.1 Analytical ProceduresReferee analysis shall be byany method acceptable to purchaser and vendor.4.2 Check Analysis LimitsShall be as shown in Table 1.TABLE 1 Check Analysis VariationElementLimit or Maximum ofSpecified Element, %Varia

19、tionUnder min or Over maxCarbon Up to 0.02, incl 0.005Over 0.02 to 0.20, incl 0.01Over 0.20 to 0.60, incl 0.02Over 0.60 to 1.00, incl 0.03Manganese Up to 1.00, incl 0.03Over 1.00 to 3.00, incl 0.04Over 3.00 to 6.00, incl 0.07Over 6.00 to 10.00, incl 0.10Silicon Up to 0.05, incl 0.01Over 0.05 to 0.25

20、, incl 0.02Over 0.25 to 0.50, incl 0.03Over 0.50 to 1.00, incl 0.05Over 1.00 to 4.50, incl 0.10Phosphorus All 0.005Sulfur Up to 0.02, incl 0.003Over 0.02 to 0.06, incl 0.005Chromium Up to 5.00, incl 0.10Over 5.00 to 15.00, incl 0.15Over 15.00 to 25.00, incl 0.25Over 25.00 to 35.00, incl 0.30Over 35.

21、00 to 45.00, incl 0.40Over 45.00 to 50.00, incl 0.50Nickel Up to 1.00, incl 0.05Over 1.00 to 5.00, incl 0.10Over 5.00 to 10.00, incl 0.15Over 10.00 to 20.00, incl 0.20Over 20.00 to 30.00, incl 0.25Over 30.00 to 40.00, incl 0.30Over 40.00 to 60.00, incl 0.35Over 60.00 to 80.00, incl 0.45Over 80.00 to

22、 99.00, incl 0.60Cobalt Up to 0.10, incl 0.01Over 0.10 to 0.20, incl 0.02Over 0.20 to 1.00, incl 0.03Over 1.00 to 5.00, incl 0.05Over 5.00 to 10.00, incl 0.10Over 10.00 to 15.00, incl 0.15Over 15.00 to 20.00, incl 0.20Over 20.00 to 25.00, incl 0.25Over 25.00 to 30.00, incl 0.30Over 30.00 to 35.00, i

23、ncl 0.35Over 35.00 to 50.00, incl 0.50Molybdenum Up to 1.00, incl 0.03Over 1.00 to 3.00, incl 0.05Over 3.00 to 5.00, incl 0.10Over 5.00 to 20.00, incl 0.15Over 20.00 to 30.00, incl 0.25Over 30.00 to 40.00, incl 0.35Tungsten Up to 1.00, incl 0.04Over 1.00 to 3.00, incl 0.10Over 3.00 to 5.00, incl 0.1

24、5Over 5.00 to 10.00, incl 0.20B 880 03 (2008)2TABLE 1 ContinuedElementLimit or Maximum ofSpecified Element, %VariationUnder min or Over maxOver 10.00 to 20.00, incl 0.25Columbium (Nb) Up to 1.50, incl 0.05and/or Tantalum Over 1.50 to 3.00, incl 0.10Over 3.00 to 5.00, incl 0.15Over 5.00 to 7.00, incl

25、 0.20Over 7.00 to 10.00, incl 0.25Over 10.00 to 13.00, incl 0.30Titanium Up to 0.10, incl 0.02Over 0.10 to 0.50, incl 0.03Over 0.50 to 1.00, incl 0.04Over 1.00 to 2.00, incl 0.05Over 2.00 to 3.50, incl 0.07Over 3.50 to 5.00, incl 0.10Over 5.00 to 10.00, incl 0.20Aluminum Up to 0.10, incl 0.02Over 0.

26、10 to 0.50, incl 0.05Over 0.50 to 2.00, incl 0.10Over 2.00 to 5.00, incl 0.20Over 5.00 to 10.00, incl 0.25Over 10.00 to 15.00, incl 0.30Boron Up to 0.01, incl 0.002Over 0.01 to 0.05, incl 0.005Over 0.05 to 0.15, incl 0.010Iron Up to 0.20, incl 0.02Over 0.20 to 0.75, incl 0.03Over 0.75 to 2.50, incl

27、0.05Over 2.50 to 5.00, incl 0.07Over 5.00 to 10.00, incl 0.10Over 10.00 to 15.00, incl 0.15Over 15.00 to 30.00, incl 0.30Over 30.00 to 50.00, incl 0.45Copper Up to 0.20, incl 0.02Over 0.20 to 0.50, incl 0.03Over 0.50 to 5.00, incl 0.04Over 5.00 to 10.00, incl 0.05Over 10.00 to 20.00, incl 0.10Over 2

28、0.00 to 30.00, incl 0.15Over 30.00 to 40.00, incl 0.20Over 40.00 to 50.00, incl 0.25Vanadium Up to 0.50, incl 0.04Over 0.50 to 1.50, incl 0.05Yttrium Up to 0.050, incl 0.005Over 0.050 to 0.10, incl 0.010Over 0.10 to 0.20, incl 0.015Zirconium Up to 0.10, incl 0.01Over 0.10 to 0.20, incl 0.02Lanthanum

29、 Up to 0.20, incl 0.01Cerium Up to 0.050, incl 0.005Over 0.050 to 0.10, incl 0.010Over 0.10 to 0.20, incl 0.015Hafnium Up to 1.50, incl 0.05Over 1.50 to 3.00, incl 0.10Rhenium Up to 1.50, incl 0.05Over 1.50 to 3.00, incl 0.10Over 3.00 to 5.00, incl 0.15Over 5.00 to 7.00, incl 0.20Platinum Up to 0.50

30、, incl 0.03Oxygen Up to 0.010, incl 0.005B 880 03 (2008)3TABLE 1 ContinuedElementLimit or Maximum ofSpecified Element, %VariationUnder min or Over maxNitrogen Up to 0.02, incl 0.005Over 0.02 to 0.19, incl 0.01Over 0.19 to 0.25, incl 0.02Over 0.25 to 0.35, incl 0.03Over 0.35 to 0.45, incl 0.04Over 0.

31、45 to 0.60, incl 0.05Magnesium Up to 0.10, incl 0.01Lead Up to 0.01, incl 0.002Tin Up to 0.01, incl 0.002Over 0.01 to 0.05, incl 0.005Zinc Up to 0.01, incl 0.002Over 0.01 to 0.05, incl 0.0055. Quality Assurance Provisions5.1 SamplingFor the purpose of determining conform-ance to the chemical composi

32、tion requirement, each heat or lotin a shipment shall be considered separately. All samples shallbe taken from finished part or material in the condition inwhich it is received, except that all protective surface treat-ments shall be removed before sampling. Sample material shallbe free from scale,

33、grease, dirt, and other foreign materials andshall be taken in such a manner as to prevent alteration of thechemical composition of the sample. Sampling shall be inaccordance with Practice E55for wrought material or PracticeE88for cast material, as applicable, insofar as practicable.6. Keywords6.1 c

34、obalt alloys; nickel alloys; product check analysisASTM 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 the validity of any such patent righ

35、ts, 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. Your comments are invited either for

36、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 comments have not received a fair hearing

37、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).B 880 03 (2008)4

展开阅读全文
相关资源
猜你喜欢
  • AECMA PREN 4123-1994 Aerospace Series Shank Nuts Self-Locking in Heat Resisting Nickel Base Alloy NI-P100HT (Inconel 718) Silver Plated on Thread Classification 1 550 MPa (at Ambie.pdf AECMA PREN 4123-1994 Aerospace Series Shank Nuts Self-Locking in Heat Resisting Nickel Base Alloy NI-P100HT (Inconel 718) Silver Plated on Thread Classification 1 550 MPa (at Ambie.pdf
  • AECMA PREN 4124-1994 Aerospace Series Shank Nuts Self-Locking in Heat Resisting Nickel Base Alloy NI-P101HT (Waspaloy) Silver Plated on Thread for 60 Degree Swage Classification 1 .pdf AECMA PREN 4124-1994 Aerospace Series Shank Nuts Self-Locking in Heat Resisting Nickel Base Alloy NI-P101HT (Waspaloy) Silver Plated on Thread for 60 Degree Swage Classification 1 .pdf
  • AECMA PREN 4125-1994 Aerospace Series Nuts Anchor Self-Locking Fixed Two Lug Reduced Series with Incremental Counterbore in Heat Resisting Steel MoS2 Lubricated Classification 900 .pdf AECMA PREN 4125-1994 Aerospace Series Nuts Anchor Self-Locking Fixed Two Lug Reduced Series with Incremental Counterbore in Heat Resisting Steel MoS2 Lubricated Classification 900 .pdf
  • AECMA PREN 4126-1994 Aerospace Series Nuts Anchor Self-Locking Floating Two Lug Reduced Series with Incremental Counterbore in Heat Resisting Steel MoS2 Lubricated Classification 9.pdf AECMA PREN 4126-1994 Aerospace Series Nuts Anchor Self-Locking Floating Two Lug Reduced Series with Incremental Counterbore in Heat Resisting Steel MoS2 Lubricated Classification 9.pdf
  • AECMA PREN 4127-1999 Aerospace Series Bolts Normal Hexagonal Head Coarse Tolerance Normal Shank Short Thread in Titanium Alloy Aluminium IVD Coated Classification  1 100 MPa (at Am.pdf AECMA PREN 4127-1999 Aerospace Series Bolts Normal Hexagonal Head Coarse Tolerance Normal Shank Short Thread in Titanium Alloy Aluminium IVD Coated Classification 1 100 MPa (at Am.pdf
  • AECMA PREN 4128-1999 Aerospace Series Bolts Normal Hexagonal Head Coarse Tolerance Normal Shank Short Thread in Heat Resisting Nickel Base Alloy Aluminium IVD Coated Classification.pdf AECMA PREN 4128-1999 Aerospace Series Bolts Normal Hexagonal Head Coarse Tolerance Normal Shank Short Thread in Heat Resisting Nickel Base Alloy Aluminium IVD Coated Classification.pdf
  • AECMA PREN 4129-1994 Aerospace Series Bolts Normal Hexagonal Head Coarse Tolerance Normal Shank Medium Length Thread in Alloy Steel Cadmium Plated Classification 1 100 MPa (at Ambi.pdf AECMA PREN 4129-1994 Aerospace Series Bolts Normal Hexagonal Head Coarse Tolerance Normal Shank Medium Length Thread in Alloy Steel Cadmium Plated Classification 1 100 MPa (at Ambi.pdf
  • AECMA PREN 4130-1994 Aerospace Series Bolts Normal Hexagonal Head Coarse Tolerance Normal Shank Medium Length Thread in Titanium Alloy Aluminium IVD Coated Classification  1 100 MP.pdf AECMA PREN 4130-1994 Aerospace Series Bolts Normal Hexagonal Head Coarse Tolerance Normal Shank Medium Length Thread in Titanium Alloy Aluminium IVD Coated Classification 1 100 MP.pdf
  • AECMA PREN 4131-1994 Aerospace Series Bolts Normal Hexagonal Head Coarse Tolerance Normal Shank Medium Length Thread in Heat Resisting Nickel Base Alloy Aluminium IVD Coated Classi.pdf AECMA PREN 4131-1994 Aerospace Series Bolts Normal Hexagonal Head Coarse Tolerance Normal Shank Medium Length Thread in Heat Resisting Nickel Base Alloy Aluminium IVD Coated Classi.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