1、Designation: F467 13 (Reapproved 2018)Standard 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
2、number in parentheses 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.1. Scope*1.1 This specification covers the requirements for c
3、ommer-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 SpecificationF468.1.3 The values state
4、d 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.1.4 This international standard was developed
5、in accor-dance with internationally recognized principles on standard-ization established in the Decision on Principles for theDevelopment of International Standards, Guides and Recom-mendations issued by the World Trade Organization TechnicalBarriers to Trade (TBT) Committee.2. Referenced Documents
6、2.1 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-Carbon Nickel-Chr
7、omium-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 andAluminum-Base
8、 Alloys (Withdrawn 2017)3E38 Methods for Chemical Analysis of Nickel-Chromiumand Nickel-Chromium-Iron Alloys (Withdrawn 1989)3E53 Test Method for Determination of Copper in UnalloyedCopper by GravimetryE54 Test Methods for Chemical Analysis of Special Brassesand Bronzes (Withdrawn 2002)3E55 Practice
9、 for 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
10、 Test Methods for Chemical Analysis of Nickel-CopperAlloys (Withdrawn 2003)3E92 Test Methods for Vickers Hardness and Knoop Hard-ness of Metallic MaterialsE101 Test Method for SpectrographicAnalysis ofAluminumand Aluminum Alloys by the Point-to-Plane Technique(Withdrawn 1996)3E120 Test Methods for C
11、hemical 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 Chemica
12、l Analysis 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 Nonferro
13、us Bolts, Hex Cap Screws,1This specification is under the jurisdiction of ASTM Committee F16 onFasteners and is the direct responsibility of Subcommittee F16.04 on NonferrousFasteners.Current edition approved Sept. 1, 2018. Published September 2018. Originallyapproved in 1976. Last previous edition
14、approved in 2013 as F467 132. DOI:10.1520/F0467-13R18.2For 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.3The la
15、st approved version of this historical standard is referenced onwww.astm.org.*A Summary of Changes section appears at the end of this standardCopyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United StatesThis international standard was developed in
16、accordance with internationally recognized principles on standardization established in the Decision on Principles for theDevelopment of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.1Socket Head Cap Screws, and
17、 Studs for General UseF606/F606M Test Methods for Determining the MechanicalProperties of Externally and Internally ThreadedFasteners, Washers, Direct Tension Indicators, and RivetsF1470 Practice for Fastener Sampling for Specified Me-chanical Properties and Performance Inspection2.2 ASME Standards:
18、4B 1.1 Unified Inch Screw Threads (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
19、per inch);3.1.4 Alloy number (Table 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
20、 be specified onthe purchase order (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 Compli
21、ance,Supplementary Requirement S 1, ASTM Specification F 467-XX4. Materials and Manufacture4.1 Materials:4.1.1 The nuts shall be manufactured from material havinga chemical composition conforming to the requirements inTable 2 and capable of developing the required mechanicalproperties for the specif
22、ied 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 require-ments.4.2 Manufacture:4.2.1 FormingUnle
23、ss 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 ConditionCopper (all alloys) As formed or stress reliev
24、ed 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-T9 Solution treated, artificially aged, and c
25、oldworkedTitanium 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 thechemical composition specified in Table 1 for
26、 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 to be shipped and report theresults to the pur
27、chaser. 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 furnish a certificate of conformance certifying
28、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 inTable 1.5.3.2 In the event of disagreement,
29、 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 specifi
30、ed alloy.6.2 Where both proof load and hardness tests are performed,the proof load test results shall take precedence for acceptancepurposes.7. Dimensions7.1 NutsUnless otherwise specified, the dimensions ofnuts shall be in accordance with the requirements of ASMEB18.2.2.7.2 ThreadsUnless otherwise
31、specified, the nuts shallhave Class 2B threads in accordance with ASME B1.1.4Available from American Society of Mechanical Engineers (ASME), ASMEInternational Headquarters, Two Park Ave., New York, NY 10016-5990, http:/www.asme.org.F467 13 (2018)2TABLE1ChemicalRequirementsComposition,%UNSDesignation
32、NumberCopperandCopper-BaseAlloysAlloyGeneralNameAluminumCopper,minIron, maxManganese,maxNickel,maxPhos-phorusSiliconZinc, maxALead,maxTinArsenic,maxC11000110ETPcopper99.9C26000260brass68.571.50.05balance0.07C27000270brass63.068.50.07balance0.10C46200462navalbrass62.065.00.10balance0.200.51.0C4640046
33、4navalbrass59.062.00.10balance0.200.51.0C51000510phosphorbronzebalanceA0.100.030.350.300.054.25.8C61300613aluminumbronze6.0 7.5B2.03.00.100.15C0.0150.100.050.010.200.50C61400614aluminumbronze6.0 8.088.0D1.53.51.0C63000630aluminumbronze9.0 11.078.0D2.04.01.54.05.50.25max0.20maxC64200642aluminumsilico
34、nbronze6.3 7.688.65D0.300.100.251.52.2E0.500.050.20max0.15C65100651siliconbronze96.0D0.80.70.82.01.50.05C65500655siliconbronze94.8D0.81.50.62.83.81.50.05C66100661siliconbronze94.0D0.251.52.83.51.50.200.8C67500675manganesebronze0.25max57.060.00.82.00.050.5balance0.200.51.5C71000710cupro-nickel74.0D0.
35、601.0019.023.0C1.000.05C71500715cupro-nickel65.0D0.400.71.0029.033.0C1.000.05AElementsshownasbalanceshallbearithmeticallycomputedbydeductingthesumoftheothernamedelementsfrom100.BCopperplusspecifiedelements=99.8min;copperplussilver=88.591.5.CCobaltistobecountedasnickel.DMinimumcontentofcopperplusallo
36、therelementswithspecifiedlimitsshallbe99.5%.EAnalloycontainingashighas2.6%siliconisacceptableprovidedthesumofalltheelementsotherthancopper,silicon,andirondoesnotexceed0.30%.F467 13 (2018)3TABLE1ContinuedNickelandNickel-BaseAlloysUNSDesigna-tionNumberAlloyGeneralNameAlumi-numCarbon,maxChro- miumCoppe
37、rAIron, 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 7.01.00balance0.0400.082.5015.017.00.0300.35max3.04.5N04400400Ni-Cu Cla
38、ssA0.3balance2.52.063.0 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 maxN06625625CNi-Cr-Mo-Cb0.40 max0
39、.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 max3.04.4AElementsshownasbalanceshallbearithmeticallycomputedbydeductingthesumoftheothernamedelementsfrom100.BCobaltistobecoun
40、tedasnickel.CAlloy625materialshallberefinedusingtheelectroslagremeltingprocess(ESR),orthevacuumarcremeltingprocess(VAR).F467 13 (2018)4TABLE1ContinuedComposition,%Aluminum-BaseAlloysAUNSDesig- nationNum-berAl- loyGeneralNameAlumi-numAChro- miumCopperIron, maxManganese,maxSilicon,maxTitanium,maxZinc,
41、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 0.140.15 0.400.70.150.400.80.150.250.8 1.2CAAnalysisshal
42、lregularlybemadeonlyfortheelementsspecifiedinthistable.If,however,thepresenceofotherelementsissuspectedorindicatedinamountsgreaterthanthespecifiedlimits,furtheranalysisshallbemadetodeterminethattheseelementsarenotpresentinexcessofthespecifiedlimits.BTitanium+zirconium0.20%,max.CLead0.40.7%;bismuth0.
43、40.7%.F467 13 (2018)5TABLE1ContinuedTitaniumandTitanium-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,SnSilicon,SiRuthe-nium,RuResidualsBeach,maxtotal,max
44、R502501TitaniumGr10.100.20balance0.01250.050.180.10.4R504002TitaniumGr20.100.30balance0.01250.050.250.10.4R507004TitaniumGr40.100.50balance0.01250.070.400.10.4R564005TitaniumGr55.56.750.100.40balance0.01250.050.203.54.50.10.4R5640123TitaniumTi-6Al-4VELI5.56.50.080.25balance0.01250.050.133.54.50.10.4
45、R524007TitaniumGr70.100.30balance0.01250.050.250.12 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 0.140.10.4AAllreportedvaluesaremaximums,unless
46、arangeisspecified.BAresidualisanelementpresentinametaloranalloyinsmallquantitiesinherenttothemanufacturingprocessbutnotaddedintentionally.Residualelementsneednotbereportedunlessareportisspecificallyrequiredbythepurchaser.CRutheniumandPalladium,orboth,maybeaddedtoGrade19forenhancedcorrosionresistance
47、asnegotiatedbetweenpurchaserandvendor.Chemicalanalysisisnotrequiredunlessspecificallynegotiated.F467 13 (2018)68. Workmanship, Finish, and Appearance8.1 WorkmanshipNuts shall have a workmanlike finishfree of injurious burrs, seams, laps, irregular surfaces, andother imperfections affecting serviceab
48、ility.8.2 FinishUnless otherwise specified, the nuts shall befurnished without any additive chemical or metallic finish.9. Sampling9.1 A lot, for the purposes of selecting test specimens, shallconsist of not more than 100 000 pieces offered for inspectionat one time having the following common chara
49、cteristics:9.1.1 One type of item,9.1.2 Same alloy and temper, and9.1.3 One nominal diameter and thread series.10. Number of Tests and Retests10.1 Normal TestingThe requirements of this specifica-tion shall be met in continuous mass production for stock (seeTable 3). The manufacturer shall make sample inspections asTABLE 2 Mechanical Property RequirementsAlloy MechanicalProperty MarkingHardness,minAProof Stress,Hex Nutmin, ksiProof Stress,Heavy Hex Nutmin, ksiBCu 110 F 467A 65
