1、Designation: F467 132Standard 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 2014.2NOTE17.1 was editoria
3、lly corrected in May 2014.1. Scope*1.1 This specification 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
4、nutscovered by this specification are covered by 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 equiva
5、lents are presented in the specification.2. Referenced 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-Car
6、bon Nickel-Chromium-Molybdenum-Copper, and Low-Carbon 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
7、 Test Methods for Chemical Analysis of Aluminum andAluminum-Base AlloysE38 Methods for Chemical Analysis of Nickel-Chromiumand Nickel-Chromium-Iron Alloys (Withdrawn 1989)3E53 Test Method for Determination of Copper in UnalloyedCopper by GravimetryE54 Test Methods for Chemical Analysis of Special Br
8、assesand Bronzes (Withdrawn 2002)3E55 Practice for Sampling Wrought Nonferrous Metals andAlloys for Determination of Chemical CompositionE62 Test Methods for Chemical Analysis of Copper andCopperAlloys (Photometric Methods) (Withdrawn 2010)3E75 Test Methods for Chemical Analysis of Copper-Nickeland
9、Copper-Nickel-Zinc Alloys (Withdrawn 2010)3E76 Test Methods for Chemical Analysis of Nickel-CopperAlloys (Withdrawn 2003)3E92 Test Method for Vickers Hardness of Metallic Materials(Withdrawn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 Techniq
10、ue(Withdrawn 1996)3E120 Test Methods for Chemical 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 (Wit
11、hdrawn 2002)3E354 Test Methods for Chemical 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
12、 Gas FusionF468 Specification for Nonferrous Bolts, Hex Cap Screws,Socket Head Cap Screws, and Studs for General Use1This specification is under the jurisdiction of ASTM Committee F16 onFasteners and is the direct responsibility of Subcommittee F16.04 on NonferrousFasteners.Current edition approved
13、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, www.astm.org, orcontact ASTM Customer Service at serviceastm.org. For Annual Book of ASTMStandards volume
14、 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 appears at the end of this standardCopyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Co
15、nshohocken, PA 19428-2959. United States1F606 Test Methods for Determining the Mechanical Proper-ties of Externally and Internally Threaded Fasteners,Washers, Direct Tension Indicators, and RivetsF1470 Practice for Fastener Sampling for Specified Me-chanical Properties and Performance Inspection2.2
16、ASME Standards: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 (diamet
17、er and threads 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 requireme
18、nts, if any, to 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 Certif
19、icate of Compliance,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
20、 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 require-ments.4.2 Manufacture:4.
21、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 ConditionCopper (all alloys) As formed o
22、r 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-T9 Solution treated, artificia
23、lly 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 thechemical composition specified
24、 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 to be shipped and report theres
25、ults 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 furnish a certificate of conforma
26、nce 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 inTable 1.5.3.2 In the event o
27、f 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
28、for the specified 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 ThreadsUn
29、less otherwise specified, the nuts shallhave Class 2B threads in accordance with ASME B1.1.4Available from Global Engineering Documents, 15 Inverness Way, EastEnglewood, CO 80112-5704, http:/.F467 1322TABLE1ChemicalRequirementsComposition,%UNSDesignationNumberCopperandCopper-BaseAlloysAlloyGeneralNa
30、meAluminumCopper,minIron, maxManganese,maxNickel,maxPhos-phorusSiliconZinc, maxALead,maxTinArsenic,maxC11000110ETPcopper99.9C26000260brass68.571.50.05balance0.07C27000270brass63.068.50.07balance0.10C46200462navalbrass62.065.00.10balance0.200.51.0C46400464navalbrass59.062.00.10balance0.200.51.0C51000
31、510phosphorbronzebalanceA0.100.030.350.300.054.25.8C61300613aluminumbronze6.0 7.5B2.03.00.100.15C0.0150.100.050.010.200.50C61400614aluminumbronze6.0 8.088.0D1.53.51.0C63000630aluminumbronze9.0 11.078.0D2.04.01.54.05.50.25max0.20maxC64200642aluminumsiliconbronze6.3 7.688.65D0.300.100.251.52.2E0.500.0
32、50.20max0.15C65100651siliconbronze96.0D0.80.70.82.01.50.05C65500655siliconbronze94.8D0.81.50.62.83.81.50.05C66100661siliconbronze94.0D0.251.52.83.51.50.200.8C67500675manganesebronze0.25max57.060.00.82.00.050.5balance0.200.51.5C71000710cupro-nickel74.0D0.601.0019.023.0C1.000.05C71500715cupro-nickel65
33、.0D0.400.71.0029.033.0C1.000.05AElementsshownasbalanceshallbearithmeticallycomputedbydeductingthesumoftheothernamedelementsfrom100.BCopperplusspecifiedelements=99.8min;copperplussilver=88.591.5.CCobaltistobecountedasnickel.DMinimumcontentofcopperplusallotherelementswithspecifiedlimitsshallbe99.5%.EA
34、nalloycontainingashighas2.6%siliconisacceptableprovidedthesumofalltheelementsotherthancopper,silicon,andirondoesnotexceed0.30%.F467 1323TABLE1ContinuedNickelandNickel-BaseAlloysUNSDesigna-tionNumberAlloyGeneralNameAlumi-numCarbon,maxChro- miumCopperAIron, maxManganese,maxNickelAPhosphous,maxSilicon,
35、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 ClassA0.3balance2.52.063.0 70.00.5B0.024N04405405Ni-Cu
36、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 max0.1020.0 23.05.0 max0.5058.0 min0.0150.50 max0.40 max
37、1.00 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.BCobaltistobecountedasnickel.CAlloy625materialshallberefinedusingthee
38、lectroslagremeltingprocess(ESR),orthevacuumarcremeltingprocess(VAR).EditoriallycorrectedinJanuary2008.F467 1324TABLE1ContinuedComposition,%Aluminum-BaseAlloysAUNSDesig- nationNum-berAl- loyGeneralNameAlumi-numAChro- miumCopperIron, maxManganese,maxSilicon,maxTitanium,maxZinc,maxMagne-siumOtherElemen
39、ts,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 1.2CAAnalysisshallregularlybemadeonlyfort
40、heelementsspecifiedinthistable.If,however,thepresenceofotherelementsissuspectedorindicatedinamountsgreaterthanthespecifiedlimits,furtheranalysisshallbemadetodeterminethattheseelementsarenotpresentinexcessofthespecifiedlimits.BTitanium+zirconium0.20%,max.CLead0.40.7%;bismuth0.40.7%.F467 1325TABLE1Con
41、tinuedTitaniumandTitanium-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,maxR502501TitaniumGr10.100.20bala
42、nce0.01250.050.180.10.4R504002TitaniumGr20.100.30balance0.01250.050.250.10.4R507004TitaniumGr40.100.50balance0.01250.070.400.10.4R564005TitaniumGr55.56.750.100.40balance0.01250.050.203.54.50.10.4R5640123TitaniumTi-6Al-4VELI5.56.50.080.25balance0.01250.050.133.54.50.10.4R524007TitaniumGr70.100.30bala
43、nce0.01250.050.250.12 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,unlessarangeisspecified.BAresidualis
44、anelementpresentinametaloranalloyinsmallquantitiesinherenttothemanufacturingprocessbutnotaddedintentionally.Residualelementsneednotbereportedunlessareportisspecificallyrequiredbythepurchaser.CRutheniumandPalladium,orboth,maybeaddedtoGrade19forenhancedcorrosionresistanceasnegotiatedbetweenpurchaseran
45、dvendor.Chemicalanalysisisnotrequiredunlessspecificallynegotiated.F467 13268. Workmanship, Finish, and Appearance8.1 WorkmanshipNuts shall have a workmanlike finishfree of injurious burrs, seams, laps, irregular surfaces, andother imperfections affecting serviceability.8.2 FinishUnless otherwise spe
46、cified, 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 characteristics:9.1.1 One type of item,9.
47、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 asspecified below to
48、ensure that the product conforms to theTABLE 2 Mechanical Property RequirementsAlloy MechanicalProperty MarkingHardness,minAProof Stress,Hex Nutmin, ksiProof Stress,Heavy 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
49、 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 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 4
