1、Designation: F467 081F467 13Standard 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.Anumber in pa
2、rentheses indicates the year of last reapproval.Asuperscriptepsilon () indicates an editorial change since the last revision or reapproval.This standard has been approved for use by agencies of the Department of Defense.1 NOTE7.1 was editorially corrected in October 2009.1. Scope*1.1 This specificat
3、ion covers the requirements for commercial wrought nonferrous nuts 0.250 to 1.500 in. inclusive in diameterin a number of alloys in common use and intended for general service applications.1.2 Applicable bolts, cap screws, and studs for use with nuts covered by this specification are covered by Spec
4、ification F468.1.3 This specification is the inch-pound companion to SpecificationThe values stated in inch-pound units are to be F467M;therefore, no SI equivalents are presented in the specification.regarded as standard. No other units of measurement are includedin this standard.NOTE 1This specific
5、ation is the inch-pound companion to Specification F467M; therefore, no SI equivalents are presented in the specification.2. Referenced Documents2.1 ASTM Standards:2B154 Test Method for Mercurous Nitrate Test for Copper AlloysB574 Specification for Low-Carbon Nickel-Chromium-Molybdenum, Low-Carbon N
6、ickel-Molybdenum-Chromium, Low-Carbon Nickel-Molybdenum-Chromium-Tantalum, Low-Carbon Nickel-Chromium-Molybdenum-Copper, and Low-CarbonNickel-Chromium-Molybdenum-Tungsten Alloy RodD3951 Practice for Commercial PackagingE18 Test Methods for Rockwell Hardness of Metallic MaterialsE29 Practice for Usin
7、g Significant Digits in Test Data to Determine Conformance with SpecificationsE34 Test Methods for Chemical Analysis of Aluminum and Aluminum-Base AlloysE38 Methods for Chemical Analysis of Nickel-Chromium and Nickel-Chromium-Iron Alloys (Withdrawn 1989)3E53 Test Method for Determination of Copper i
8、n Unalloyed Copper by GravimetryE54 Test Methods for Chemical Analysis of Special Brasses and Bronzes (Withdrawn 2002)3E55 Practice for Sampling Wrought Nonferrous Metals and Alloys for Determination of Chemical CompositionE62 Test Methods for Chemical Analysis of Copper and Copper Alloys (Photometr
9、ic Methods) (Withdrawn 2010)3E75 Test Methods for Chemical Analysis of Copper-Nickel and Copper-Nickel-Zinc Alloys (Withdrawn 2010)3E76 Test Methods for Chemical Analysis of Nickel-Copper Alloys (Withdrawn 2003)3E92 Test Method for Vickers Hardness of Metallic Materials (Withdrawn 2010)3E101 Test Me
10、thod for SpectrographicAnalysis ofAluminum andAluminumAlloys by the Point-to-PlaneTechnique (Withdrawn1996)3E120 Test Methods for Chemical Analysis of Titanium and Titanium Alloys (Withdrawn 2003)3E165 Practice for Liquid Penetrant Examination for General IndustryE227 Test Method for Optical Emissio
11、n Spectrometric Analysis of Aluminum and Aluminum Alloys by the Point-to-PlaneTechnique (Withdrawn 2002)31 This specification is under the jurisdiction of ASTM Committee F16 on Fasteners and is the direct responsibility of Subcommittee F16.04 on Nonferrous Fasteners.Current edition approved May 1, 2
12、008April 1, 2013. Published June 2008May 2013. Originally approved in 1976. Last previous edition approved in 2006 asF467 06aF467 081 . DOI: 10.1520/F0467-08E01.10.1520/F0467-13.2 For referencedASTM standards, visit theASTM website, www.astm.org, or contactASTM Customer Service at serviceastm.org. F
13、or Annual Book of ASTM Standardsvolume information, refer to the standards Document Summary page on the ASTM website.3 The last approved version of this historical standard is referenced on www.astm.org.This document is not an ASTM standard and is intended only to provide the user of an ASTM standar
14、d 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 consult prior editions as appropriate. In all cases only the current versionof the standard as published by ASTM i
15、s 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, PA 19428-2959. United States1E354 Test Methods for Chemical Analysis of High-Temperature, Electrical, Magneti
16、c, and Other Similar Iron, Nickel, andCobalt AlloysE478 Test Methods for Chemical Analysis of Copper AlloysE1409 Test Method for Determination of Oxygen and Nitrogen in Titanium and Titanium Alloys by the Inert Gas FusionTechniqueF468 Specification for Nonferrous Bolts, Hex Cap Screws, Socket Head C
17、ap Screws, and Studs for General UseF606 Test Methods for Determining the Mechanical Properties of Externally and Internally Threaded Fasteners, Washers, DirectTension Indicators, and RivetsF1470 Practice for Fastener Sampling for Specified Mechanical Properties and Performance Inspection2.2 ASME St
18、andards:4B 1.1 Unified Inch Screw Threads (UN and UNR Thread Form)B 18.2.2 Square and Hex Nuts3. Ordering Information3.1 Orders for nuts under this specification shall include the following information:3.1.1 Quantity (number of pieces of each item and size);3.1.2 Name of item;3.1.3 Size (diameter an
19、d 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 requirements,
20、 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 published date).NOTE 2Atypical ordering description is as follows: 10 000 pieces, Hex Nut, 0.250“ -20,Alloy 270, Furnish Certificat
21、e of Compliance, SupplementaryRequirement S 1, ASTM Specification F 467-XX4. Materials and Manufacture4.1 Materials:4.1.1 The nuts shall be manufactured from material having a chemical composition conforming to the requirements in Table 2and capable of developing the required mechanical properties f
22、or the specified alloy in the finished fastener. See Specification B574for nickel alloys.4.1.2 The starting condition of the raw material shall be at the discretion of the fastener manufacturer but shall be such that thefinished products conform to all the specified requirements.4.2 Manufacture:4.2.
23、1 FormingUnless otherwise specified, the nuts shall be hot pressed, cold formed, or machined from suitable material atthe option of the manufacturer.4.2.2 ConditionExcept as provided in 4.2.3, the nuts shall be furnished in the condition specified below:Alloy ConditionCopper (all alloys) As formed o
24、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
25、lly aged, and coldworkedTitanium As formed625 Annealed4.2.3 Stress RelievingWhen required, stress relieving shall be specified by the purchaser for all copper alloys and nickel alloys400 and 405.4 Available from Global Engineering Documents, 15 Inverness Way, East Englewood, CO 80112-5704, http:/.F4
26、67 132TABLE 1 Chemical RequirementsComposition, %UNSDesignationNumberCopper and Copper-Base AlloysAlloy General Name Aluminum Copper,min Iron,max Manganese,max Nickel,max Phos-phorus Silicon Zinc,maxA Lead,max Tin Arsenic,maxC11000 110 ETP copper 99.9C26000 260 brass 68.571.5 0.05 balance 0.07C27000
27、 270 brass 63.068.5 0.07 balance 0.10C46200 462 naval brass 62.065.0 0.10 balance 0.20 0.51.0C46400 464 naval brass 59.062.0 0.10 balance 0.20 0.51.0C51000 510 phosphor bronze balanceA 0.10 0.030.35 0.30 0.05 4.25.8C61300 613 aluminum bronze 6.07.5B 2.03.0 0.10 0.15C 0.015 0.10 0.05 0.01 0.200.50C61
28、400 614 aluminum bronze 6.08.088.0D 1.53.5 1.0C63000 630 aluminum bronze 9.011.078.0D 2.04.0 1.5 4.05.5 0.25 max 0.20 maxC64200 642 aluminum silicon bronze 6.37.688.65D 0.30 0.10 0.25 1.52.2E 0.50 0.05 0.20 max 0.15C65100 651 silicon bronze 96.0D 0.8 0.7 0.82.0 1.5 0.05C65500 655 silicon bronze 94.8
29、D 0.8 1.5 0.6 2.83.8 1.5 0.05C66100 661 silicon bronze 94.0D 0.25 1.5 2.83.5 1.5 0.200.8C67500 675 manganese bronze 0.25 max 57.060.0 0.82.0 0.050.5 balance 0.20 0.51.5C71000 710 cupro-nickel 74.0D 0.60 1.00 19.023.0C 1.00 0.05C71500 715 cupro-nickel 65.0D 0.400.7 1.00 29.033.0C 1.00 0.05A Elements
30、shown as balance shall be arithmetically computed by deducting the sum of the other named elements from 100.B Copper plus specified elements = 99.8 min; copper plus silver = 88.591.5.C Cobalt is to be counted as nickel.D Minimum content of copper plus all other elements with specified limits shall b
31、e 99.5 %.E An alloy containing as high as 2.6 % silicon is acceptable provided the sum of all the elements other than copper, silicon, and iron does not exceed 0.30 %.TABLE 1 ContinuedNickel and Nickel-Base AlloysUNSDesigna-tionNumberAlloy General Name Alumi-num Carbon,max Chro-mium CopperA Iron,max
32、 Manganese,max NickelAPhosphous,max Silicon,max Titanium Cobalt,max Molyb-denum Sulfur,max Vana-dium Tung-sten Nio-biumN10001 335 Ni-Mo 0.05 1.0max4.06.01.0 balance 0.025 1.00 2.50 26.030.00.030 0.20.4N10276 276 Ni-Mo-Cr 0.02 14.516.54.07.01.00 balance 0.040 0.08 2.50 15.017.00.030 0.35max3.04.5N044
33、00 400 Ni-CuClass A0.3 balance 2.5 2.0 63.070.00.5 B 0.024N04405 405 Ni-CuClass B0.3 balance 2.5 2.0 63.070.00.5 B 0.0250.060N05500 500 Ni-Cu-Al 2.303.150.25 balance 2.0 1.5 63.070.00.5 0.350.85B 0.01N06059 59 NiCr-Mo0.10.40.010max22.024.00.5max1.5max0.5maxbalance 0.015max0.10max0.3max15.016.50.010m
34、axF467133TABLE 3.1.4 ContinuedTABLE 1 ContinuedNickel and Nickel-Base AlloysUNSDesigna-tionNumberAlloy General Name Alumi-num Carbon,max Chro-mium CopperA Iron,max Manganese,max NickelAPhosphous,max Silicon,max Titanium Cobalt,max Molyb-denum Sulfur,max Vana-dium Tung-sten Nio-biumN06625 625C Ni-Cr-
35、Mo-Cb 0.40max0.10 20.023.05.0max0.50 58.0min0.015 0.50max0.40max1.00max8.010.00.015 3.24.2N06686 686 Ni-Cr-Mo-W 0.010max19.023.05.0max0.75maxbalance 0.04max0.08max0.020.2515.017.00.02max3.04.4A Elements shown as balance shall be arithmetically computed by deducting the sum of the other named element
36、s from 100.B Cobalt is to be counted as nickel.C Alloy 625 material shall be refined using the electroslag remelting process (ESR), or the vacuum arc remelting process (VAR). Editorially corrected in January 2008.TABLE 1 ContinuedComposition, %Aluminum-Base AlloysAUNSDesig-nationNum-berAl-loyGeneral
37、NameAlumi-numAChro-mium CopperIron,maxManganese,maxSilicon,maxTitanium,maxZinc,maxMagne-siumOther Elements,maxEach TotalA92024 2024 Aluminum2024balance 0.10max3.84.90.50 0.300.90.50 0.15B 0.25 1.21.80.05 0.15A96061 6061 Aluminum6061balance 0.040.350.150.400.7 0.15 0.400.80.15 0.25 0.81.20.05 0.15A96
38、262 6262 Aluminum6262balance 0.040.140.150.400.7 0.15 0.400.80.15 0.25 0.81.2CA Analysis shall regularly be made only for the elements specified in this table. If, however, the presence of other elements is suspected or indicated in amounts greater than the specified limits, further analysis shall b
39、emade to determine that these elements are not present in excess of the specified limits.B Titanium + zirconium 0.20 %, max.C Lead 0.40.7 %; bismuth 0.40.7 %.TABLE 1 ContinuedTitanium and Titanium-Base AlloysAUNSDes-ignationNumberAlloy GeneralName Alumi-num, AlCar-bon,CIron,FeTita-nium, TiHydro-gen,
40、 HNitro-gen,NOxy-gen,OPalla-dium, PdVana-dium, VChro-mium, CrMolyb-denum,MoZirco-nium,ZrTin,SnSilicon,SiRuthe-nium,RuResidualsBeach,maxtotal,maxR50250 1 Titanium Gr 1 0.10 0.20 balance 0.0125 0.05 0.18 0.1 0.4R50400 2 Titanium Gr 2 0.10 0.30 balance 0.0125 0.05 0.25 0.1 0.4R50700 4 Titanium Gr 4 0.1
41、0 0.50 balance 0.0125 0.07 0.40 0.1 0.4R56400 5 Titanium Gr 5 5.56.750.10 0.40 balance 0.0125 0.05 0.20 3.54.50.1 0.4R56401 23 Titanium Ti-6Al-4VELI5.56.50.08 0.25 balance 0.0125 0.05 0.13 3.54.50.1 0.4R52400 7 Titanium Gr 7 0.10 0.30 balance 0.0125 0.05 0.25 0.120.250.1 0.4R58640 19 Titanium Ti-38-
42、6-44 3.04.00.05 0.30 balance 0.0200 0.03 0.12 0.10A 7.58.55.56.53.54.53.54.50.10C 0.15 0.4R55111 32 Titanium Ti-5-1-1-1 4.55.50.08 0.25 balance 0.0125 0.03 0.11 0.61.40.61.20.61.40.61.40.060.140.1 0.4F467134A All reported values are maximums, unless a range is specified.B Aresidual is an element pre
43、sent in a metal or an alloy in small quantities inherent to the manufacturing process but not added intentionally. Residual elements need not be reported unless a report is specifically requiredby the purchaser.C Ruthenium and Palladium, or both, may be added to Grade 19 for enhanced corrosion resis
44、tance as negotiated between purchaser and vendor. Chemical analysis is not required unless specifically negotiated.F4671355. Chemical Composition5.1 Chemical CompositionThe nuts shall conform to the chemical composition specified in Table 1 for the specified alloy.5.2 Manufacturers Analysis:5.2.1 Ex
45、cept as provided in 5.2.2, when test reports are required on the inquiry or purchase order (3.1.8), the manufacturer shallmake individual analyses of randomly selected finished nuts from the product to be shipped and report the results to the purchaser.Alternatively, if heat and lot identities have
46、been maintained, the analysis of the raw material from which the nuts have beenmanufactured may be reported instead of product analysis.5.2.2 For aluminum nuts, instead of 5.2.1, the manufacturer may furnish a certificate of conformance certifying compliance withthe chemical composition specified in
47、 Table 1.5.3 Product Analysis:5.3.1 Product analyses may be made by the purchaser from finished products representing each lot. The chemical compositionthus determined shall conform to the requirements in Table 1.5.3.2 In the event of disagreement, a referee chemical analysis of samples from each lo
48、t shall be made in accordance with 12.1and 13.1.TABLE 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 5
49、4Cu 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 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
