ASTM F290-1994(2015) Standard Specification for Round Wire for Winding Electron Tube Grid Laterals《电子管栅极侧绕组用圆形电线的标准规格》.pdf

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1、Designation: F290 94 (Reapproved 2015)Standard Specification forRound Wire for Winding Electron Tube Grid Laterals1This standard is issued under the fixed designation F290; the number immediately following the designation indicates the year of originaladoption or, in the case of revision, the year o

2、f last revision.Anumber in parentheses indicates the year of last reapproval.Asuperscriptepsilon () indicates an editorial change since the last revision or reapproval.1. Scope1.1 This specification covers round wire up to 0.006 in.(0.15 mm) in diameter for use as electron tube grid lateralwinding w

3、ire.1.2 Five classes of wire are covered based on their tensileproperties (see 5.2 and 5.3).1.3 The values stated in inch-pound units are to be regardedas standard. The values given in parentheses are mathematicalconversions to SI units that are provided for information onlyand are not considered st

4、andard.1.4 This standard does not purport to address all of thesafety concerns, if any, associated with its use. It is theresponsibility of the user of this standard to establish appro-priate safety and health practices and determine the applica-bility of regulatory limitations prior to use.2. Refer

5、enced Documents2.1 ASTM Standards:2E39 Methods for Chemical Analysis of Nickel (Withdrawn1995)3E107 Test Methods for Chemical Analysis of ElectronicNickel (Withdrawn 2003)3E129 Test Method for Spectrographic Analysis of Thermi-onic NickelAlloys by the Powder Techniques (Withdrawn1999)3F16 Test Metho

6、ds for Measuring Diameter or Thickness ofWire and Ribbon for Electronic Devices and LampsF205 Test Method for Measuring Diameter of Fine Wire byWeighingF288 Specification for Tungsten Wire for Electron Devicesand LampsF289 Specification for Molybdenum Wire and Rod forElectronic Applications3. Termin

7、ology3.1 Description of Terms:3.1.1 The following description of terms shall apply to therequirements specified in Table 1:3.1.1.1 breaking strengthThe stress at which the specimenbreaks.3.1.1.2 elongationThe maximum percent of stretch in aspecimen of 10-in. (250-mm) gage length.3.1.1.3 tensile stre

8、ngthThe ultimate strength of the mate-rial expressed either as grams per milligram per 200 mm lengthof wire or pounds per square inch.3.1.1.4 ultimate strengthThe maximum stress developedin a specimen.3.1.1.5 work loadThe difference between the yield loadand the ultimate load.3.1.1.6 yield strengthT

9、he stress developed at 1 percentelongation when testing a specimen of 10-in. (250-mm) gagelength.4. Chemical Composition4.1 The wire shall conform to the requirements as tochemical composition as prescribed in Table 2.5. Tensile Properties5.1 The wire shall conform to the requirements as to tensiles

10、trength, yield strength, working range, and elongation prop-erties as prescribed in Table 1 for the class of wire designated.5.2 The class designations for the nickel-titanium-magnesium alloy UNS N03300; the nickel-manganese alloyUNS N02211; molybdenum wire, and the nickel-molybdenum-iron alloy UNS

11、N10001; are based on their tensile properties asfollows:5.2.1 Class IThe wire shall conform to elongation prop-erties as specified in ranges in Table 1.5.2.2 Class IIThe wire shall conform to the followingtensile properties:5.2.2.1 Yield strength with a spread of approximately615 %, as shown in gram

12、s-force, minimum and maximum, inTable 2,5.2.2.2 Working range, as specified in Table 1, and1This specification is under the jurisdiction of ASTM Committee F01 onElectronicsand is the direct responsibility of Subcommittee F01.03 on MetallicMaterials, Wire Bonding, and Flip Chip.Current edition approv

13、ed July 1, 2015. Published October 2015. Originallyapproved in 1954 as B290 54 T; redesignated F290 in 1955. Last previous editionapproved in 2010 as F290 94 (2010). DOI: 10.1520/F0290-94R15.2For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact ASTM Customer Service at serv

14、iceastm.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.Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, P

15、A 19428-2959. United States1TABLE 1 Tensile Properties for Nickel-Titanium-Magnesium Alloy (UNS N03300), Nickel-Manganese Alloy (UNS N02211),Molybdenum Wire, and Nickel-Molybdenum-Iron Alloy (UNS N10001) WireCLASS INOTE 1Wire supplied as Class I shall conform to the following elongation values as sp

16、ecified by range:Material Range Wire Diameter,in. (mm)Elongation,%Nickel-titanium-magnesium alloy (UNS N03300)and nickel-manganese alloy (UNS N02211) 1 All 8 to 162 All 14 to 223 0.003 (0.08) and under 20 and over4 Above 0.003 (0.08) 22 and overMolybdenum 1 All 8 to 162 All 14 to 22Nickel-molybdenum

17、-iron alloy (UNS N10001) 1 0.001 (0.025) 8 to 182 0.0015 (0.038) 18 to 323 0.002 (0.050) and above 25 and overCLASS IINOTE 1Wire supplied as Class II shall conform to the following requirements as to yield strength ( 15 percent), working range, and elongation:MaterialWire Diameter Yield StrengthWork

18、ingLoad, min, gfElongation,min, %in. (mm)Approximate Center LoadStress psi (Mpa) min, gf max, gfNickel-titanium-magnesiumalloy (UNS N03300)0.0015 (0.038) 74 000 (510) 51 67 17 80.0016 (0.041) 74 000 (510) 56 76 17 80.0017 (0.043) 70 500 (486) 62 84 17 80.0018 (0.046) 70 500 (486) 69 93 20 80.0019 (0

19、.048) 70 500 (486) 76 104 20 100.0020 (0.051) 70 000 (483) 85 115 35 100.0025 (0.064) 68 500 (472) 130 175 60 100.0027 (0.069) 64 500 (445) 145 190 75 100.0030 (0.076) 63 500 (438) 175 235 90 150.0033 (0.084) 63 000 (434) 210 280 115 150.0035 (0.089) 63 000 (434) 235 315 135 200.0040 (0.102) 61 500

20、(424) 300 400 190 200.0045 (0.114) 60 000 (414) 370 500 250 200.0050 (0.127) 60 000 (414) 450 610 330 200.0055 (0.140) 60 000 (414) 550 745 400 200.0060 (0.152) 60 000 (414) 655 885 475 20Nickel-manganese al-loy (UNS N02211)0.0020 (0.051) 59 600 (411) 70 100 30 140.0025 (0.064) 58 400 (403) 110 150

21、50 140.0027 (0.067) 56 800 (392) 125 170 60 140.0030 (0.076) 56 600 (390) 150 210 80 180.0033 (0.084) 50 400 (347) 175 245 105 180.0035 (0.089) 50 400 (347) 200 270 120 180.004 (0.102) 51 000 (352) 250 340 170 220.0045 (0.114) 47 000 (324) 295 395 230 220.005 (0.127) 46 000 (317) 350 470 305 220.006

22、 (0.152) 43 000 (296) 465 635 490 22Molybdenum 0.0008 (0.020) 120 000 (827) 24 34 1 80.0010 (0.025) 120 000 (827) 35 50 4 80.0012 (0.030) 118 500 (817) 50 70 6 80.0013 (0.033) 118 500 (817) 60 80 8 80.00133 (0.034) 118 500 (817) 65 85 8 80.00150 (0.038) 113 500 (782) 77 105 10 120.0017 (0.043) 113 5

23、00 (782) 95 135 15 120.0020 (0.051) 105 000 (724) 127 173 25 120.0025 (0.064) 101 000 (696) 191 259 40 150.0030 (0.076) 96 000 (662) 262 354 65 170.0033 (0.084) 96 000 (662) 317 429 80 170.0035 (0.089) 96 000 (662) 356 482 90 170.0040 (0.102) 96 000 (662) 466 630 115 170.0045 (0.114) 96 000 (662) 58

24、9 797 145 170.0050 (0.127) 96 000 (662) 728 984 180 170.0055 (0.140) 96 000 (662) 880 1190 220 170.0060 (0.152) 96 000 (662) 1047 1417 260 17Nickel-molybdenum-ironalloy (UNS N10001)0.0016 (0.041) 92 000 (634) 70 95 40 100.0020 (0.051) 85 000 (586) 102 138 65 100.0025 (0.064) 85 000 (586) 160 215 110

25、 100.0030 (0.076) 80 000 (552) 219 297 165 150.0033 (0.084) 80 000 (552) 272 368 205 150.0035 (0.089) 80 000 (552) 287 389 240 15F290 94 (2015)2TABLE 1 ContinuedCLASS IINOTE 1Wire supplied as Class II shall conform to the following requirements as to yield strength ( 15 percent), working range, and

26、elongation:MaterialWire Diameter Yield StrengthWorkingLoad, min, gfElongation,min, %in. (mm)Approximate Center LoadStress psi (Mpa) min, gf max, gf0.0040 (0.102) 80 000 (552) 371 503 320 200.0050 (0.127) 80 000 (552) 606 820 485 20Class IIINOTE 1Wire supplied as Class III shall conform to the follow

27、ing requirements as to yield strength (10 %), working range, and elongation:MaterialWire Diameter Yield StrengthWorkingLoad, min, gfElongation,min, %in. (mm)Approximate Center LoadStress psi (Mpa) min, gf max, gfNickel-titanium-magnesiumalloy (UNS N03300)0.0015 (0.038) 74 000 (510) 53 65 20 100.0016

28、 (0.041) 74 000 (510) 59 73 25 100.0017 (0.043) 70 500 (486) 66 80 30 120.0018 (0.046) 70 500 (486) 72 89 35 120.0019 (0.048) 70 500 (486) 81 99 35 120.0020 (0.051) 70 000 (483) 90 110 45 150.0025 (0.064) 68 500 (472) 135 165 75 150.0027 (0.069) 64 500 (445) 150 185 90 15Class IIINOTE 1Wire supplied

29、 as Class III shall conform to the following requirements as to yield strength (10 %), working range, and elongation:MaterialWire Diameter Yield StrengthWorkingLoad, min, gfElongation,min, %in. (mm)Approximate Center LoadStress psi (Mpa) min, gf max, gfNickel-titanium-magnesiumalloy (UNS N03300)0.00

30、30 (0.076) 63 500 (438) 185 225 120 150.0033 (0.084) 63 000 (434) 220 270 145 150.0035 (0.089) 63 000 (434) 250 305 170 200.0040 (0.102) 61 500 (424) 315 385 230 200.0045 (0.114) 60 000 (414) 390 480 310 200.0050 (0.127) 60 000 (414) 475 585 400 200.0055 (0.140) 60 000 (414) 580 710 485 200.0060 (0.

31、152) 60 000 (414) 690 850 575 20Nickel-manganese al-loy (UNS N02211)0.0020 (0.051) 59 600 (411) 75 95 40 140.0025 (0.064) 58 400 (403) 115 145 65 140.0027 (0.069) 56 800 (392) 130 165 80 140.0030 (0.076) 56 600 (390) 160 200 100 180.0033 (0.084) 50 400 (347) 190 235 125 180.0035 (0.090) 50 400 (347)

32、 210 260 145 180.0040 (0.102) 51 500 (355) 265 325 200 220.0045 (0.114) 47 500 (328) 310 380 265 220.0050 (0.127) 46 000 (317) 370 450 355 220.006 (0.152) 54 000 (372) 495 605 560 22Molybdenum 0.0008 (0.020) 120 000 (827) 25 33 1 80.0010 (0.025) 120 000 (827) 40 50 4 80.0012 (0.030) 118 500 (817) 55

33、 65 6 80.0013 (0.033) 118 500 (817) 65 75 8 80.00133 (0.034) 118 500 (817) 70 80 8 80.0015 (0.038) 113 500 (782) 82 100 10 120.0017 (0.043) 113 500 (782) 105 129 15 120.0020 (0.051) 96 000 (662) 135 165 25 150.0025 (0.064) 96 000 (662) 202 248 40 150.0030 (0.076) 96 000 (662) 277 339 65 170.0033 (0.

34、084) 96 000 (662) 336 410 80 170.0035 (0.089) 96 000 (662) 377 461 90 170.0040 (0.102) 96 000 (662) 493 603 115 170.0045 (0.114) 96 000 (662) 624 762 145 170.0050 (0.127) 96 000 (662) 770 942 180 170.0055 (0.140) 96 000 (662) 932 1139 220 170.0060 (0.152) 96 000 (662) 1109 1355 260 17Nickel-molybden

35、um-ironalloy (UNS N10001)0.0016 (0.041) 92 000 (634) 76 92 45 150.0020 (0.051) 85 000 (586) 109 133 75 150.0025 (0.064) 85 000 (586) 167 205 125 150.0030 (0.076) 80 000 (552) 232 284 185 200.0033 (0.084) 80 000 (552) 289 353 230 200.0035 (0.089) 80 000 (552) 305 373 270 20F290 94 (2015)35.2.2.3 Elon

36、gation as specified in Table 1.5.2.3 Class IIIThe wire shall conform to the followingtensile properties:5.2.3.1 Yield strength with a spread of approximately610 %, as shown in grams-force, minimum and maximum, inTable 1.5.2.3.2 A larger working range as specified in Table 1, and5.2.3.3 Elongation as

37、 specified in Table 1.5.3 The class designations for tungsten wire are as follows:5.3.1 Classes IV and VTungsten wire UNS R07005 shallconform to the tensile properties for both classes as prescribedin Table 3.6. Dimensions and Permissible Variations6.1 The wire shall not vary from the specified diam

38、eter asdetermined by weight, by more than the amounts prescribed inTable 4. Center weights of various types of wire are given inTable 5.6.2 In the case of finished plated wires, the percentage ofplating shall be calculated on the basis of the bare wire weight.In specifying rod plated and drawn plate

39、d wire, the platingweight will be based on finished wire weight. Orders shallspecify the manner of plating.7. Surface7.1 Bare WireThe surface of the wire shall be bright, andfree from cracks, slivers, fissures, lubricants, or other detrimen-tal defects as determined at a magnification of 10.7.2 Plat

40、ed WireThe bare wire shall conform to the re-quirements specified in 7.1; the plating shall be free frombubbles, flakes, blisters, porosity, and plating salts, and shallnot show peeled containing when tested in accordance with9.2.8. Chemical Analysis8.1 Chemical analysis of the material shall be mad

41、e inaccordance with the methods described in the followingparagraphs (8.1.1 to 8.1.3):8.1.1 Nickel Alloy Wire (UNS N03300; UNS N02211; UNSN10001)The chemical analysis shall be made in accordancewith either or both Test Methods E39 and Test Methods E107.The material may alternatively be analyzed in a

42、ccordance withTest Method E129.8.1.2 Molybdenum WireThe molybdenum content shall bedetermined gravimetrically or by a combination of analyses forimpurities by spectrochemical and chemical methods.8.1.3 Tungsten Wire (UNS R07005)The tungsten contentshall be determined gravimetrically or by a combinat

43、ion ofanalyses for impurities by spectrochemical and chemical meth-ods.9. Test Methods9.1 Tensile PropertiesDetermine the yield strength, work-ing range, breaking strength, and elongation by using aconstant rate of traverse tester calibrated in terms of constantrate of traverse. Rate of traverse sho

44、uld be approximately 1 in.(25 mm)/min with a gage length of 10 in. (250 mm).TABLE 1 ContinuedClass IIINOTE 1Wire supplied as Class III shall conform to the following requirements as to yield strength (10 %), working range, and elongation:MaterialWire Diameter Yield StrengthWorkingLoad, min, gfElonga

45、tion,min, %in. (mm)Approximate Center LoadStress psi (Mpa) min, gf max, gf0.0040 (0.102) 80 000 (552) 394 482 360 200.0050 (0.127) 80 000 (552) 642 784 540 20TABLE 2 Chemical CompositionElement, percentNickel-Titanium-MagnesiumAlloy (UNS N03300)Nickel-ManganeseAlloy (UNS N02211)Molyb-denumTungsten(U

46、NS R07005)Nickel-Molybdenum-Iron Alloy(UNS N10001)Limit Nominal Limit Nominal Limit Limit Limit NominalNickel 97.0 min 98.5 93.7 min 95.2 . . remainder 66.5Carbon 0.4 max 0.25 0.20 max 0.10 . . 0.12 max 0.05Copper 0.25 max 0.03 0.25 max 0.05 . . . .Iron 0.60 max 0.10 0.75 max 0.15 . . 6.00 max 5.00M

47、agnesium 0.20 min 0.35 . . . . . .0.50 max . . . . . . .Manganese 0.50 max 0.20 4.25 min 4.5 . . 1.00 max 0.455.25 max . . . . .Molybdenum . . . . 99.9 min . 33.00 max 27.50Silicon 0.35 max 0.15 0.15 max 0.05 . . 1.00 max 0.45Sulfur 0.01 max 0.005 0.015 max . . . 0.030 max 0.012Titanium 0.20 min 0.4

48、0 . . . . . .0.60 max . . . . . . .Tungsten . . . . . 99.95 min . .Vanadium . . . . . . 0.60 min 0.25Phosphorus . . . . . . 0.040 max .Chromium . . . . . . 1.00 max .Cobalt . . . . . . 2.50 max .F290 94 (2015)49.2 Plate AdherenceDraw the wire over a 0.10-in. (2.5-mm) radius knife edge, holding the w

49、ire against the edge withthe thumb. Pull the wire at a 45 angle to the plane of the blade.In addition, draw the wire through a razor slit in a 0.25-in.(6-mm) thick leather pad with the wire riding on the bottom ofthe slit with approximately 30 angle of approach and a 30angle of departure. Note the approach side of the leather beltand wire for flaking or peeling of plating.9.3 Weight ToleranceDetermine size and uniformity inaccordance with Test Method F205.9.4 Diameter ToleranceIf specified, measure diametertolerance by equipment calibrated as