ASTM A565 A565M-2005a Standard Specification for Martensitic Stainless Steel Bars for High-Temperature Service《高温用马氏体不锈钢棒材标准规范》.pdf

1、Designation: A 565/A 565M 05aStandard Specification forMartensitic Stainless Steel Bars for High-TemperatureService1This standard is issued under the fixed designationA 565/A 565M; the number immediately following the designation indicates the yearof original adoption or, in the case of revision, th

2、e year of last revision. A number in parentheses indicates the year of last reapproval.A superscript epsilon (e) 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. Scope*1.1 This specification covers

3、 hot-finished and cold-finishedmartensitic chromium steel bars for high-temperature service.The mechanical properties are developed by suitable heattreatment, as indicated for each alloy.1.2 Where strength at temperature is a factor, these steelsare generally limited to a maximum service temperature

4、 of1200F 650C. For oxidation (scaling) resistance and at lowstresses, these steels are useful to 1450F 790C.1.3 This specification is expressed in both inch-pound unitsand SI units; however, unless the purchase order or contractspecifies the applicable M specification designation (SI units),the inch

5、-pound units shall apply. The values stated in eitherinch-pound units or SI units are to be regarded separately asstandard. Within the text, the SI units are shown in brackets.The values stated in each system may not be exact equivalents;therefore, each system shall be used independently of the othe

6、r.Combining values from the two systems may result in noncon-formance with the specification.2. Referenced Documents2.1 ASTM Standards:2A 370 Test Methods and Definitions for Mechanical Testingof Steel ProductsA 484/A 484M Specification for General Requirements forStainless Steel Bars, Billets, and

7、ForgingsA 751 Test Methods, Practices, and Terminology forChemical Analysis of Steel ProductsA 994 Guide for Editorial Procedures and Form of ProductSpecifications for Steel, Stainless Steel, and RelatedAlloysE112 Test Methods for Determining Average Grain SizeE 292 Test Methods for Conducting Time-

8、for-RuptureNotch Tension Tests of MaterialsE 527 Practice for Numbering Metals and Alloys (UNS)E 562 Test Method for Determining Volume Fraction bySystematic Manual Point Count2.2 SAE Document:3SAE J1086 Recommended Practice for Numbering Metalsand Alloys (UNS)3. Ordering Information3.1 It is the re

9、sponsibility of the purchaser to specify allrequirements that are necessary for material ordered under thisspecification. Such requirements may include, but are notlimited to, the following:3.1.1 Quantity (weight or number of pieces);3.1.2 Name of material (martensitic stainless steel);3.1.3 Form (b

10、ar, etc.);3.1.4 Condition;3.1.5 Finish;3.1.6 Size, or applicable dimension including diameter,thickness, width, length, etc.;3.1.7 Grade designation (Table 1); and3.1.8 ASTM designation number and date of issue.4. General Requirements4.1 Product furnished to this specification shall conform tothe re

11、quirements of Specification A 484/A 484M, includingany supplementary requirements indicated in the purchaseorder. Failure to comply with the general requirements ofSpecification A 484/A 484M constitutes nonconformance withthis specification. In case of conflict between the requirementsof this specif

12、ication and Specification A 484/A 484M, thisspecification shall prevail.5. Manufacture5.1 Heat Treatment:5.1.1 The product forms covered in this specification maybe furnished in one of the following conditions:5.1.1.1 Condition AAnnealed,5.1.1.2 Condition THeat treated (for machining),1This specific

13、ation is under the jurisdiction of ASTM Committee A01 on Steel,Stainless Steel and Related Alloys and is the direct responsibility of SubcommitteeA01.17 on Flat-Rolled and Wrought Stainless Steel.Current edition approved Sept. 1, 2005. Published September 2005. Originallyapproved in 1966. Last previ

14、ous edition approved in 2005 as A 565 05.2For 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.3Available from Soci

15、ety of Automotive Engineers (SAE), 400 CommonwealthDr., Warrendale, PA 15096-0001.1*A Summary of Changes section appears at the end of this standard.Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.5.1.1.3 Condition HTHeat treated (for

16、 high-temperatureservice), or5.1.1.4 Condition HHeat treated.5.2 Condition and Finish:5.2.1 Bars may be furnished in one of the followinghot-finished conditions:5.2.1.1 Hot rolled, or5.2.1.2 Rough turned (rounds only).5.2.2 Bars may be furnished in one of the followingcold-finished conditions:5.2.2.

17、1 Cold drawn,5.2.2.2 Centerless ground (rounds only), or5.2.2.3 Polished (rounds only).6. Chemical Requirements6.1 Each alloy covered by this specification shall conform tothe chemical composition specified in Table 1.6.2 Methods and practices relating to chemical analysisrequired by this specificat

18、ion shall be in accordance with TestMethods, Practices, and Terminology A 751.7. Metallurgical Requirements7.1 The microstructure shall not contain more than 5 %delta-ferrite after full heat treatment as described in Table 2.Visual examination for the volume fraction of delta ferrite ofvarious repre

19、sentative areas of examination is acceptable.When the visual estimation method indicates the delta ferritecontent is greater than the allowed limit, the manufacturer mayemploy Test Method E 562 for determining the acceptability ofthe lot.8. Mechanical Properties Requirements8.1 The material shall co

20、nform to the mechanical propertieslisted in Table 3 for the ordered condition.8.2 Material furnished in Condition A or T shall be capableof developing the room-temperature properties specified forCondition HT when subjected to heat treatment as specified inTable 2.8.3 The yield strength shall be det

21、ermined by the offsetmethod as described in the current edition of Test Methods andDefinitions A 370.8.4 The impact strength shall be determined at 70 to 80F21 to 27C, by Charpy V-notch specimen TypeAas describedin Test Methods and Definitions A 370.8.5 Stress rupture testing of UNS S42226 shall be

22、con-ducted as specified in Table 4 using a combination test bar inaccordance with Test Methods E 292. Rupture must occur inthe smooth section of each test specimen. The test may bediscontinued after the time specified, provided the certificationTABLE 1 Chemical RequirementsGrade UNSDesig-nationACarb

23、on Man-ganesePhos-phorusSulfur Silicon Chromium Nickel Molyb-denumVana-diumTungsten Nitrogen Alumi-numColum-biumCopperXM-32 S64152 0.080.15 0.500.90 0.025max0.025max0.35 max 11.0012.50 2.003.00 1.502.00 0.250.40 . . . 0.010.05 . . . . . . . . . . . S41041 0.130.18 0.400.60 0.030max0.030max0.50 max 1

24、1.5013.00 0.50 max 0.20 max . . . . . . . . . 0.05max0.150.45. . . S41425 0.05 max 0.501.00 0.02 max 0.005max0.50 max 12.0015.00 4.007.00 1.502.00 . . . . . . 0.060.12 . . . . . . 0.30max615 S41800 0.150.20 0.50 max 0.040max0.030max0.50 max 12.0014.00 1.802.20 0.50 max . . . 2.503.50 . . . . . . . .

25、 . . . .616 S42200 0.200.25 0.501.00 0.025max0.025max0.50 max 11.0012.50 0.501.00 0.901.25 0.200.30 0.901.25 . . . . . . . . . . . .619 S42300 0.270.32 0.951.35 0.025max0.025max0.50 max 11.0012.00 0.50 max 2.503.00 0.200.30 . . . . . . . . . . . . . . . . . S42226 0.150.20 0.500.80 0.020 0.010 0.200

26、.60 10.011.5 0.300.60 0.801.10 0.150.25 0.25 0.040.08 0.05 0.350.55.ANew designation established in accordance with Practice E 527 and SAE J1086.TABLE 2 Heat TreatmentNOTE 1 If straightened, a stress-relieving treatment is necessary. Stress-relieving temperature should be 50F 28C below the final tem

27、peringtemperature.NOTE 2Air or oil quenching depends on section size; heavier sections, approximately 3 in. 76.2 mm or greater, should be oil quenched. Suitablesynthetic quenchants may be substituted for oil.Grade UNS DesignationACondition Heat Treatment615 S41800 HT 1800 to 1850F 980 to 1010C, quen

28、ch in air or oil and double temper at 1150F 620C min for 2 h min for eachtempering treatment. . . S41425 HT 1700 to 1800F 925 to 980C, quench in air and temper at 1100F 595C min for 1 h, min, per inch thickness.616 S42200 HT 1875 to 1925F 1020 to 1050C, quench in air or oil and temper at 1150F 620C

29、min for 2 h min.H 1875 to 1925F 1020 to 1050C, quench in air or oil and temper at 1250F 675C min for 2 h min.619 S42300 HT 1875 to 1925F 1020 to 1050C, quench in air or oil and temper at 1150F 620C min for 2 h min.XM-32 K64152 HT 1825 to 1875F 995 to 1020C, quench in air or oil and temper at 1050F 5

30、65C min for 2 h min. . . S41041 HT 2075 to 2125F 1135 to 1165C for 2 h min, quench in air or oil and temper at 1250F 675C min for 2 h min. . . S42226 HT 2000 to 2500F 1095 to 1150C, quench in rapid air, oil, or polymer and temper at 1185F 640C min.ANew designation established in accordance with Prac

31、tice E 527 and SAE J1086.A 565/A 565M 05a2so notes. Stress rupture testing is not required on bars less than12 in. in diameter or thickness.9. Keywords9.1 martensitic stainless steel; stainless steel bars; stainlesssteel billets; stainless steel forgings; temperature serviceapplicationshighSUPPLEMEN

32、TARY REQUIREMENTSThe following supplementary requirements shall apply only when specified by the purchaser in theinquiry, contract, and order. Details of these supplementary requirements shall be agreed upon by themanufacturer and purchaser.S1. Non-Destructive ExaminationGrade DS1.1 MethodEach bar s

33、hall be subjected to NDE. Themethod used shall be: Eddy Current (ET), Magnetic Particle(MPI wet or dry), Liquid Penetrant (LPI), or Ultrasonic (UT),at the option of the vendor unless otherwise indicated in thepurchase order.S1.2 Acceptance CriteriaFor LPI or MPI, linear indica-tions (those indicatio

34、ns longer than116 in. 1.5 mm with alength greater than three times their width) are unacceptable.For UT or ET, reject levels for linear indications shall be basedon the alarm response from a 0.012-in. 0.3-mm maximumdeep surface notch in a calibration bar.S2. MicrostructureUNS S42226S2.1 Metallograph

35、ic inspection shall be performed at1003 magnification to determine the metallurgical structure,grain size, and delta ferrite content.S2.2 The microstructure shall be tempered martensite withno more than 1 % delta ferrite.S2.3 The average grain size shall be 4 or finer. Themaximum size of individual

36、grains, distributed at random, shallbe a 2. When the average grain size is 5 or finer, only theaverage size needs be reported. Grain size determination shallbe performed in accordance with Test Methods E112.TABLE 3 Mechanical Property RequirementsAGradeUNSDesignationBConditionTensile Strength min,ks

37、i MPaYield Strength, min,0.2 % Offset, ksiMPaElongation in 2in. 50 mm or4D, min, %Reduction ofArea, min, %Impact at RoomTemperature,Charpy V-notch,min, ftlbf JBrinell HardnessC615 S41800 A . . . . . . . . . . . . . . . 311 maxHT 140 965 110 760 15 45 . . . 302 to 352. . . S41425 HT 120 825 95 655 15

38、 45 50 70 321 max616 S42200 A . . . . . . . . . . . . . . . 248 maxT . . . . . 285maxHT 140 965 110 760 13 30 8 11 302 to 352H 120 825 85 585 17 35 . . . 241 to 285619 S42300 A . . . . . . . . . . . . . . . 248 maxT . . . . . 285maxHT 140 965 110 760 8 20 8 11 302 to 352XM-32 K64152 A . . . . . . .

39、. . . . . . . . 311 maxHT 145 1000 115 795 15 30 30 40 302 to 352. . . S41041 HT 115 795 75 515 15 50 20 27 277 max. . . S42226 A . . . . . . . . . . . . . . . 302 maxS42226 HT 140 965 100 690 15 45 8 11 321 maxAThe properties and associated heat treatments are those most commonly specified. For sec

40、tions greater than 30 in.2193 cm2 in cross-sectional area, it is suggestedthat an agreement be reached between purchaser and materials vendor.BNew designation established in accordance with Practice E 527 and SAE J1086.CHardness taken at the surface for control purposes only. For acceptance purposes

41、, tensile properties govern.TABLE 4 Rupture TestingUNS S42226Temperature F C 1200 650Stress ksi MPa, min. 33 230Time to rupture, h, min 25A 565/A 565M 05a3SUMMARY OF CHANGESCommittee A01 has identified the location of selected changes made to this standard since the last issue,A 565 05, that may imp

42、act the use of this standard. (Approved Sept. 1, 2005.)(1) Added Grade UNS S42226, S2.Committee A01 has identified the location of selected changes made to this standard since the last issue, A 565 03b, thatmay impact the use of this standard. (Approved March 1, 2005.)(1) Added dual units to title.(

43、2) Added new 1.3.(3) Rationalized values in Table 2 and Table 3 in accordancewith Guide A 994.(4) Added metric values to S1.2.ASTM International takes no position respecting the validity of any patent rights asserted in connection with any item mentionedin this standard. Users of this standard are e

44、xpressly advised that determination of the validity of any such patent rights, and the riskof infringement of such rights, are entirely their own responsibility.This standard is subject to revision at any time by the responsible technical committee and must be reviewed every five years andif not rev

45、ised, either reapproved or withdrawn. Your comments are invited either for revision of this standard or for additional standardsand should be addressed to ASTM International Headquarters. Your comments will receive careful consideration at a meeting of theresponsible technical committee, which you m

46、ay attend. If you feel that your comments have not received a fair hearing you shouldmake your views known to the ASTM Committee on Standards, at the address shown below.This standard is copyrighted by ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959,United States. Individual reprints (single or multiple copies) of this standard may be obtained by contacting ASTM at the aboveaddress or at 610-832-9585 (phone), 610-832-9555 (fax), or serviceastm.org (e-mail); or through the ASTM website(www.astm.org).A 565/A 565M 05a4