ASTM F467-2013e1 Standard Specification for Nonferrous Nuts for General Use《通用有色金属螺母的标准规范》.pdf

《ASTM F467-2013e1 Standard Specification for Nonferrous Nuts for General Use《通用有色金属螺母的标准规范》.pdf》由会员分享，可在线阅读，更多相关《ASTM F467-2013e1 Standard Specification for Nonferrous Nuts for General Use《通用有色金属螺母的标准规范》.pdf（10页珍藏版）》请在麦多课文档分享上搜索。

1、Designation: F467 131Standard Specification forNonferrous Nuts for General Use1This standard is issued under the fixed designation F467; the number immediately following the designation indicates the year of originaladoption or, in the case of revision, the year of last revision. A number in parenth

2、eses indicates the year of last reapproval. A superscriptepsilon () indicates an editorial change since the last revision or reapproval.This standard has been approved for use by agencies of the U.S. Department of Defense.1NOTETable 2 was editorially corrected in February 2014.1. Scope*1.1 This spec

3、ification covers the requirements for commer-cial wrought nonferrous nuts 0.250 to 1.500 in. inclusive indiameter in a number of alloys in common use and intended forgeneral service applications.1.2 Applicable bolts, cap screws, and studs for use with nutscovered by this specification are covered by

4、 SpecificationF468.1.3 The values stated in inch-pound units are to be regardedas standard. No other units of measurement are included in thisstandard.NOTE 1This specification is the inch-pound companion to Specifica-tion F467M; therefore, no SI equivalents are presented in the specification.2. Refe

5、renced Documents2.1 ASTM Standards:2B154 Test Method for Mercurous Nitrate Test for CopperAlloysB574 Specification for Low-Carbon Nickel-Chromium-Molybdenum, Low-Carbon Nickel-Molybdenum-Chromium, Low-Carbon Nickel-Molybdenum-Chromium-Tantalum, Low-Carbon Nickel-Chromium-Molybdenum-Copper, and Low-C

6、arbon Nickel-Chromium-Molybdenum-Tungsten Alloy RodD3951 Practice for Commercial PackagingE18 Test Methods for Rockwell Hardness of Metallic Ma-terialsE29 Practice for Using Significant Digits in Test Data toDetermine Conformance with SpecificationsE34 Test Methods for Chemical Analysis of Aluminum

7、andAluminum-Base AlloysE38 Methods for Chemical Analysis of Nickel-Chromiumand Nickel-Chromium-Iron Alloys (Withdrawn 1989)3E53 Test Method for Determination of Copper in UnalloyedCopper by GravimetryE54 Test Methods for Chemical Analysis of Special Brassesand Bronzes (Withdrawn 2002)3E55 Practice f

8、or Sampling Wrought Nonferrous Metals andAlloys for Determination of Chemical CompositionE62 Test Methods for Chemical Analysis of Copper andCopperAlloys (Photometric Methods) (Withdrawn 2010)3E75 Test Methods for Chemical Analysis of Copper-Nickeland Copper-Nickel-Zinc Alloys (Withdrawn 2010)3E76 T

9、est Methods for Chemical Analysis of Nickel-CopperAlloys (Withdrawn 2003)3E92 Test Method for Vickers Hardness of Metallic Materials(Withdrawn 2010)3E101 Test Method for SpectrographicAnalysis ofAluminumand Aluminum Alloys by the Point-to-Plane Technique(Withdrawn 1996)3E120 Test Methods for Chemica

10、l Analysis of Titanium andTitanium Alloys (Withdrawn 2003)3E165 Practice for Liquid Penetrant Examination for GeneralIndustryE227 Test Method for Optical Emission SpectrometricAnalysis of Aluminum and Aluminum Alloys by thePoint-to-Plane Technique (Withdrawn 2002)3E354 Test Methods for Chemical Anal

11、ysis of High-Temperature, Electrical, Magnetic, and Other Similar Iron,Nickel, and Cobalt AlloysE478 Test Methods for Chemical Analysis of Copper AlloysE1409 Test Method for Determination of Oxygen and Nitro-gen in Titanium and Titanium Alloys by Inert Gas FusionF468 Specification for Nonferrous Bol

12、ts, Hex Cap Screws,Socket Head Cap Screws, and Studs for General UseF606 Test Methods for Determining the Mechanical Proper-ties of Externally and Internally Threaded Fasteners,Washers, Direct Tension Indicators, and Rivets1This specification is under the jurisdiction of ASTM Committee F16 onFastene

13、rs and is the direct responsibility of Subcommittee F16.04 on NonferrousFasteners.Current edition approved April 1, 2013. Published May 2013. Originallyapproved in 1976. Last previous edition approved in 2006 as F467 081. DOI:10.1520/F0467-13E01.2For referenced ASTM standards, visit the ASTM website

14、, 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.3The last approved version of this historical standard is referenced onwww.astm.org.*A Summary of Changes section a

15、ppears at the end of this standardCopyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States1F1470 Practice for Fastener Sampling for Specified Me-chanical Properties and Performance Inspection2.2 ASME Standards:4B 1.1 Unified Inch Screw Threads

16、 (UN and UNR ThreadForm)B 18.2.2 Square and Hex Nuts3. Ordering Information3.1 Orders for nuts under this specification shall include thefollowing information:3.1.1 Quantity (number of pieces of each item and size);3.1.2 Name of item;3.1.3 Size (diameter and threads per inch);3.1.4 Alloy number (Tab

17、le 1);3.1.5 Stress relieving, if required (4.2.3);3.1.6 “Shipment lot” testing, as required (Section 9);3.1.7 Source inspection, if required (Section 14);3.1.8 Certificate of compliance or test report, if required(Section 16);3.1.9 Additional requirements, if any, to be specified onthe purchase orde

18、r (4.2.1, 7.2, 8.2, 12.1, and 13.1),3.1.10 Supplementary requirements, if any; and3.1.11 ASTM designation (including year or publisheddate).NOTE 2A typical ordering description is as follows: 10 000 pieces,Hex Nut, 0.250“ -20, Alloy 270, Furnish Certificate of Compliance,Supplementary Requirement S

19、1, ASTM Specification F 467-XX4. Materials and Manufacture4.1 Materials:4Available from Global Engineering Documents, 15 Inverness Way, EastEnglewood, CO 80112-5704, http:/.TABLE 2 Mechanical Property RequirementsAlloy MechanicalProperty MarkingHardness,minAProof Stress,Hex Nutmin, ksiProof Stress,H

20、eavy Hex Nutmin, ksiBCu 110 F 467A 65 HRF 30 32Cu 260 F 467AB 55 HRF 60 65Cu 270 F 467B 55 HRF 60 65Cu 462 F 467C 65 HRB 50 54Cu 464 F 467D 55 HRB 50 54Cu 510 F 467E 60 HRB 60 65Cu 613 F 467F 70 HRB 80 86Cu 614 F 467G 70 HRB 75 81Cu 630 F 467H 85 HRB 100 108Cu 642 F 467J 75 HRB 75 81Cu 651 F 467K 75

21、 HRB 70 76Cu 655 F 467L 60 HRB 50 54Cu 661 F467M 75 HRB 70 76Cu 675 F 467N 60 HRB 55 59Cu 710 F 467P 50 HRB 45 49Cu 715 F 467R 60 HRB 55 59Ni 59 Grade 1 F 467FN 21HRC 120 130Ni 59 Grade 2 F 467GN 23HRC 135 146Ni 59 Grade 3 F 467HN 25HRC 160 173Ni 59 Grade 4 F 467JN 80HRB 100 108Ni 335 F 467S 20 HRC

22、115 124Ni 276 F 467T 20 HRC 110 119Ni 400 F 467U 75 HRB 80 86Ni 405 F 467V 60 HRB 70 76Ni 500 F 467W 24 HRC 130 140Ni 625 Grade 1F 467AC85 HRB-35 HRC 60 65Ni 625 Grade 2F 467AD 85 HRB-35 HRC 120 130Ni 686 Grade 1 F 467BN 21 HRC 120 130Ni 686 Grade 2 F 467CN 23 HRC 135 146Ni 686 Grade 3 F 467DN 25 HR

23、C 160 173Ni 686 Grade 4 F 467EN 65 HRB-25HRC 100 108Al 2024-T4CF 467X 70 HRB 55 59Al 6061-T6 F 467Y 40 HRB 40 43Al 6262-T9 F 467Z 60 HRB 52 56Ti 1 F 467AT 140 HV 40 43Ti 2 F 467BT 150 HV 55 59Ti 4 F 467CT 200 HV 85 92Ti 5 F 467DT 30 HRC 135 146Ti 7 F 467ET 160 HV 55 59Ti-19 F 467FT 24 HRC 120 130Ti

24、23 F 467GT 25 HRC 125 135Ti-5-1-1-1 F 467HT 24 HRC 105 113AFor aluminum and titanium alloys hardness values are for information only.BProof stress values for heavy hex nuts are based on 1.08 times the value for corresponding regular hex nuts.CAluminum alloy 2024-T4 shall be supplied in naturally age

25、d condition. This material is not recommended for nuts in sizes greater than14 (0.250) in.Editorially corrected in January 2008. Typographical error should be F467AC; both F467AC or 647AC are acceptable Mechanical Property Mark.Editorially corrected in February 2014.F467 1312TABLE1ChemicalRequiremen

26、tsComposition,%UNSDesignationNumberCopperandCopper-BaseAlloysAlloyGeneralNameAluminumCopper,minIron, maxManganese,maxNickel,maxPhos-phorusSiliconZinc, maxALead,maxTinArsenic,maxC11000110ETPcopper99.9C26000260brass68.571.50.05balance0.07C27000270brass63.068.50.07balance0.10C46200462navalbrass62.065.0

27、0.10balance0.200.51.0C46400464navalbrass59.062.00.10balance0.200.51.0C51000510phosphorbronzebalanceA0.100.030.350.300.054.25.8C61300613aluminumbronze6.0 7.5B2.03.00.100.15C0.0150.100.050.010.200.50C61400614aluminumbronze6.0 8.088.0D1.53.51.0C63000630aluminumbronze9.0 11.078.0D2.04.01.54.05.50.25max0

28、.20maxC64200642aluminumsiliconbronze6.3 7.688.65D0.300.100.251.52.2E0.500.050.20max0.15C65100651siliconbronze96.0D0.80.70.82.01.50.05C65500655siliconbronze94.8D0.81.50.62.83.81.50.05C66100661siliconbronze94.0D0.251.52.83.51.50.200.8C67500675manganesebronze0.25max57.060.00.82.00.050.5balance0.200.51.

29、5C71000710cupro-nickel74.0D0.601.0019.023.0C1.000.05C71500715cupro-nickel65.0D0.400.71.0029.033.0C1.000.05AElementsshownasbalanceshallbearithmeticallycomputedbydeductingthesumoftheothernamedelementsfrom100.BCopperplusspecifiedelements=99.8min;copperplussilver=88.591.5.CCobaltistobecountedasnickel.DM

30、inimumcontentofcopperplusallotherelementswithspecifiedlimitsshallbe99.5%.EAnalloycontainingashighas2.6%siliconisacceptableprovidedthesumofalltheelementsotherthancopper,silicon,andirondoesnotexceed0.30%.F467 1313TABLE1ContinuedNickelandNickel-BaseAlloysUNSDesigna-tionNumberAlloyGeneralNameAlumi-numCa

31、rbon,maxChro- miumCopperAIron, maxManganese,maxNickelAPhosphous,maxSilicon,maxTitaniumCobalt,maxMolyb- denumSulfur,maxVana-diumTung-stenNio-biumN10001335Ni-Mo0.051.0max4.0 6.01.0balance0.0251.002.5026.030.00.0300.2 0.4N10276276Ni-Mo-Cr0.0214.5 16.54.0 7.01.00balance0.0400.082.5015.017.00.0300.35max3

32、.04.5N04400400Ni-Cu ClassA0.3balance2.52.063.0 70.00.5B0.024N04405405Ni-Cu ClassB0.3balance2.52.063.0 70.00.5B0.025 0.060N05500500Ni-Cu-Al2.303.150.25balance2.01.563.0 70.00.50.350.85B0.01N0605959Ni Cr-Mo0.10.40.010max22.0 24.00.5max1.5 max0.5 maxbalance0.015max0.10 max0.3max15.016.50.010 maxN066256

33、25CNi-Cr-Mo-Cb0.40 max0.1020.0 23.05.0 max0.5058.0 min0.0150.50 max0.40 max1.00 max8.0 10.00.0153.24.2N06686686Ni-Cr-Mo-W0.010max19.0 23.05.0 max0.75 maxbalance0.04 max0.08 max0.020.2515.017.00.02 max3.04.4AElementsshownasbalanceshallbearithmeticallycomputedbydeductingthesumoftheothernamedelementsfr

34、om100.BCobaltistobecountedasnickel.CAlloy625materialshallberefinedusingtheelectroslagremeltingprocess(ESR),orthevacuumarcremeltingprocess(VAR).EditoriallycorrectedinJanuary2008.F467 1314TABLE1ContinuedComposition,%Aluminum-BaseAlloysAUNSDesig- nationNum-berAl- loyGeneralNameAlumi-numAChro- miumCoppe

35、rIron, maxManganese,maxSilicon,maxTitanium,maxZinc,maxMagne-siumOtherElements,maxEachTotalA920242024Aluminum 2024balance0.10 max3.8 4.90.500.30 0.90.500.15B0.251.2 1.80.050.15A960616061Aluminum 6061balance0.04 0.350.15 0.400.70.150.400.80.150.250.8 1.20.050.15A962626262Aluminum 6262balance0.04 0.140

36、.15 0.400.70.150.400.80.150.250.8 1.2CAAnalysisshallregularlybemadeonlyfortheelementsspecifiedinthistable.If,however,thepresenceofotherelementsissuspectedorindicatedinamountsgreaterthanthespecifiedlimits,furtheranalysisshallbemadetodeterminethattheseelementsarenotpresentinexcessofthespecifiedlimits.

37、BTitanium+zirconium0.20%,max.CLead0.40.7%;bismuth0.40.7%.F467 1315TABLE1ContinuedTitaniumandTitanium-BaseAlloysAUNS Des-ignation NumberAlloyGeneralNameAlumi-num,AlCar- bon,CIron,FeTita-nium,TiHydro- gen,HNitro-gen,NOxy- gen,OPalla-dium,PdVana-dium,VChro-mium,CrMolyb-denum,MoZirco- nium,ZrTin,SnSilic

38、on,SiRuthe-nium,RuResidualsBeach,maxtotal,maxR502501TitaniumGr10.100.20balance0.01250.050.180.10.4R504002TitaniumGr20.100.30balance0.01250.050.250.10.4R507004TitaniumGr40.100.50balance0.01250.070.400.10.4R564005TitaniumGr55.56.750.100.40balance0.01250.050.203.54.50.10.4R5640123TitaniumTi-6Al-4VELI5.

39、56.50.080.25balance0.01250.050.133.54.50.10.4R524007TitaniumGr70.100.30balance0.01250.050.250.12 0.250.10.4R5864019TitaniumTi-38-6-443.04.00.050.30balance0.02000.030.120.10A7.58.55.56.53.54.53.54.50.10C0.150.4R5511132TitaniumTi-5-1-1-14.55.50.080.25balance0.01250.030.110.61.40.61.20.61.40.61.40.06 0

40、.140.10.4AAllreportedvaluesaremaximums,unlessarangeisspecified.BAresidualisanelementpresentinametaloranalloyinsmallquantitiesinherenttothemanufacturingprocessbutnotaddedintentionally.Residualelementsneednotbereportedunlessareportisspecificallyrequiredbythepurchaser.CRutheniumandPalladium,orboth,mayb

41、eaddedtoGrade19forenhancedcorrosionresistanceasnegotiatedbetweenpurchaserandvendor.Chemicalanalysisisnotrequiredunlessspecificallynegotiated.F467 13164.1.1 The nuts shall be manufactured from material havinga chemical composition conforming to the requirements inTable 2 and capable of developing the

42、 required mechanicalproperties for the specified alloy in the finished fastener. SeeSpecification B574 for nickel alloys.4.1.2 The starting condition of the raw material shall be atthe discretion of the fastener manufacturer but shall be suchthat the finished products conform to all the specified re

43、quire-ments.4.2 Manufacture:4.2.1 FormingUnless otherwise specified, the nuts shallbe hot pressed, cold formed, or machined from suitablematerial at the option of the manufacturer.4.2.2 ConditionExcept as provided in 4.2.3, the nuts shallbe furnished in the condition specified below:Alloy ConditionC

44、opper (all alloys) As formed or stress relieved at manufacturersoptionNickel alloys 400 and 405 As formed or stress relieved at manufacturersoptionNickel alloy 500 Solution annealed and agedAluminum alloys:2024-T4 Solution treated and naturally aged6061-T6 Solution treated and artificially aged6262-

45、T9 Solution treated, artificially aged, and coldworkedTitanium As formed625 Annealed4.2.3 Stress RelievingWhen required, stress relieving shallbe specified by the purchaser for all copper alloys and nickelalloys 400 and 405.5. Chemical Composition5.1 Chemical CompositionThe nuts shall conform to the

46、chemical composition specified in Table 1 for the specifiedalloy.5.2 Manufacturers Analysis:5.2.1 Except as provided in 5.2.2, when test reports arerequired on the inquiry or purchase order (3.1.8), the manu-facturer shall make individual analyses of randomly selectedfinished nuts from the product t

47、o be shipped and report theresults to the purchaser. Alternatively, if heat and lot identitieshave been maintained, the analysis of the raw material fromwhich the nuts have been manufactured may be reportedinstead of product analysis.5.2.2 For aluminum nuts, instead of 5.2.1, the manufacturermay fur

48、nish a certificate of conformance certifying compliancewith the chemical composition specified in Table 1.5.3 Product Analysis:5.3.1 Product analyses may be made by the purchaser fromfinished products representing each lot. The chemical compo-sition thus determined shall conform to the requirements

49、inTable 1.5.3.2 In the event of disagreement, a referee chemicalanalysis of samples from each lot shall be made in accordancewith 12.1 and 13.1.6. Mechanical Properties6.1 The nuts shall be tested in accordance with the mechani-cal testing requirements for the applicable type and shall meetthe mechanical requirements in Table 2 for the specified alloy.6.2 Where both proof load and hardness tests are performed,the proof load test results shall take pre