ASTM B575-2017 Standard Specification for Low-Carbon Nickel-Chromium-Molybdenum Low-Carbon Nickel-Chromium-Molybdenum-Copper Low-Carbon Nickel-Chromium-Molybdenum-Tantalum Low-Carb.pdf
《ASTM B575-2017 Standard Specification for Low-Carbon Nickel-Chromium-Molybdenum Low-Carbon Nickel-Chromium-Molybdenum-Copper Low-Carbon Nickel-Chromium-Molybdenum-Tantalum Low-Carb.pdf》由会员分享,可在线阅读,更多相关《ASTM B575-2017 Standard Specification for Low-Carbon Nickel-Chromium-Molybdenum Low-Carbon Nickel-Chromium-Molybdenum-Copper Low-Carbon Nickel-Chromium-Molybdenum-Tantalum Low-Carb.pdf(5页珍藏版)》请在麦多课文档分享上搜索。
1、Designation: B575 151B575 17Standard Specification forLow-Carbon Nickel-Chromium-Molybdenum, Low-CarbonNickel-Chromium-Molybdenum-Copper, Low-Carbon Nickel-Chromium-Molybdenum-Tantalum, Low-Carbon Nickel-Chromium-Molybdenum-Tungsten, and Low-Carbon Nickel-Molybdenum-Chromium Alloy Plate, Sheet, and
2、Strip1This standard is issued under the fixed designation B575; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. Asuperscript epsilon () indic
3、ates 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 NOTEThe chemistry for aluminum in N06058 in Table 1 was editorially corrected in April 2016.1. Scope*1.1 This specification2 covers plate, sheet, and
4、 strip of low-carbon nickel-chromium-molybdenum alloys (UNS N10276,N06022, N06455, N06035, N06044, UNS N06058, UNS N06059),3 low-carbon nickel-chromium-molybdenum-copper alloy(UNS N06200), low-carbon nickel-molybdenum-chromium (UNS N10362), low-carbon nickel-chromium-molybdenum-tantalumalloy (UNS N0
5、6210), and low-carbon nickel-chromium-molybdenum-tungsten alloy (UNS N06686) as shown in Table 1, for usein general corrosive service.1.2 The following products are covered under this specification:1.2.1 Sheet and StripHot or cold rolled, solution annealed, and descaled unless solution anneal is per
6、formed in an atmosphereyielding a bright finish.1.2.2 PlateHot or cold rolled, solution annealed, and descaled.1.3 The values stated in inch-pound units are to be regarded as standard. The values given in parentheses are mathematicalconversions to SI units that are provided for information only and
7、are not considered standard.1.4 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibilityof the user of this standard to become familiar with all hazards including those identified in the appropriate Safety Data Sheet(SDS) for thi
8、s product/material as provided by the manufacturer, to establish appropriate safety and health practices, anddetermine the applicability of regulatory limitations prior to use.1.5 This international standard was developed in accordance with internationally recognized principles on standardizationest
9、ablished in the Decision on Principles for the Development of International Standards, Guides and Recommendations issuedby the World Trade Organization Technical Barriers to Trade (TBT) Committee.2. Referenced Documents2.1 ASTM Standards:4B906 Specification for General Requirements for Flat-Rolled N
10、ickel and Nickel Alloys Plate, Sheet, and StripE112 Test Methods for Determining Average Grain SizeE140 Hardness Conversion Tables for Metals Relationship Among Brinell Hardness, Vickers Hardness, Rockwell Hardness,Superficial Hardness, Knoop Hardness, Scleroscope Hardness, and Leeb HardnessE527 Pra
11、ctice for Numbering Metals and Alloys in the Unified Numbering System (UNS)1 This specification is under the jurisdiction ofASTM Committee B02 on Nonferrous Metals andAlloys and is the direct responsibility of Subcommittee B02.07 on RefinedNickel and Cobalt and Their Alloys.Current edition approved
12、Oct. 1, 2015June 1, 2017. Published November 2015June 2017. Originally approved in 1972. Last previous edition approved in 20142015 asB575 14.151. DOI: 10.1520/B0575-15E01.10.1520/B0575-17.2 For ASME Boiler and Pressure Vessel Code applications, see related Specification SB-575 in Section II of that
13、 Code.3 Designation established in accordance with Practice E527 and SAE J1086, Practice for Numbering Metals and Alloys (UNS).4 For referencedASTM standards, visit theASTM website, www.astm.org, or contactASTM Customer Service at serviceastm.org. For Annual Book of ASTM Standardsvolume information,
14、 refer to the standards Document Summary page on the ASTM website.This document is not an ASTM standard and is intended only to provide the user of an ASTM standard an indication of what changes have been made to the previous version. Becauseit may not be technically possible to adequately depict al
15、l changes accurately, ASTM recommends that users consult prior editions as appropriate. In all cases only the current versionof the standard as published by ASTM is to be considered the official document.*A Summary of Changes section appears at the end of this standardCopyright ASTM International, 1
16、00 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States1TABLE 1 Chemical RequirementsElement Composition Limits, %AlloyN06035AlloyN10276AlloyN06022AlloyN06455AlloyN06059AlloyN06058AlloyN06200AlloyN06210AlloyN10362AlloyN06686Molybdenum 7.609.00 15.017.0 12.514.5 14.017.0 15
17、.016.5 18.521.0 15.017.0 18.020.0 21.523.0 15.0-17.0Chromium 32.2534.25 14.516.5 20.022.5 14.018.0 22.024.0 20.023.0 22.024.0 18.020.0 13.815.6 19.0-23.0Iron 2.00 max 4.07.0 2.06.0 3.0 max 1.5, max 1.5, max 3.0 max 1.0 max 1.25 max 5.0 maxTungsten 0.60 max 3.04.5 2.53.5 . . 0.3 max . . . 3.0-4.4Coba
18、lt, max 1.00 2.5 2.5 2.0 0.3 0.3 2.0 max 1.0 . .Carbon, max 0.050 0.010 0.015 0.015 0.010 0.010 0.010 0.015 0.010 0.010Silicon, max 0.60 0.08 0.08 0.08 0.10 0.10 0.08 0.08 0.08 0.08Manganese, max 0.50 1.0 0.50 1.0 0.5 0.5 0.50 0.5 0.60 0.75Vanadium, max 0.20 0.35 0.35 . . . . 0.35 . .Phosphorus, max
19、 0.030 0.04 0.02 0.04 0.015 0.015 0.025 0.02 0.025 0.04Sulfur, max 0.015 0.03 0.02 0.03 0.010 0.010 0.010 0.02 0.010 0.02Titanium . . . 0.7 max . . . . . 0.02-0.25Nickel remainderA remainderA remainderA remainderA Bal Bal remainderA remainderA remainderA remainderAAluminum 0.40 max . . . 0.10.4 0.40
20、 max 0.50 max . 0.50 max .Copper 0.30 max . . . 0.50 max 0.50 max 1.31.9 . . .Tantalum . . . . . . . 1.52.2 . .Nitrogen . . . . . 0.020.15TABLE 1 Chemical RequirementsElement Composition Limits, %AlloyN06035AlloyN06044AlloyN10276AlloyN06022AlloyN06455AlloyN06059AlloyN06058AlloyN06200AlloyN06210Alloy
21、N10362AlloyN06686Molybdenum 7.609.00 0.80-1.20 15.017.0 12.514.5 14.017.0 15.016.5 18.521.0 15.017.0 18.020.0 21.523.0 15.0-17.0Chromium 32.2534.25 43.5-45.3 14.516.5 20.022.5 14.018.0 22.024.0 20.023.0 22.024.0 18.020.0 13.815.6 19.0-23.0Iron 2.00 max 0.3 max 4.07.0 2.06.0 3.0 max 1.5, max 1.5, max
22、 3.0 max 1.0 max 1.25 max 5.0 maxTungsten 0.60 max . 3.04.5 2.53.5 . . 0.3 max . . . 3.0-4.4Cobalt, max 1.00 . 2.5 2.5 2.0 0.3 0.3 2.0 max 1.0 . .Carbon, max 0.050 0.02 0.010 0.015 0.015 0.010 0.010 0.010 0.015 0.010 0.010Silicon, max 0.60 0.20 0.08 0.08 0.08 0.10 0.10 0.08 0.08 0.08 0.08Manganese,
23、max 0.50 0.07-0.30 1.0 0.50 1.0 0.5 0.5 0.50 0.5 0.60 0.75Vanadium, max 0.20 . 0.35 0.35 . . . . 0.35 . .Phosphorus, max 0.030 0.020 0.04 0.02 0.04 0.015 0.015 0.025 0.02 0.025 0.04Sulfur, max 0.015 0.020 0.03 0.02 0.03 0.010 0.010 0.010 0.02 0.010 0.02Titanium . 0.10-0.30 . . 0.7 max . . . . . 0.02
24、-0.25Nickel remainderA Bal remainderA remainderA remainderA Bal Bal remainderA remainderA remainderA remainderAAluminum 0.40 max 0.30 max . . . 0.10.4 0.40 max 0.50 max . 0.50 max .Copper 0.30 max . . . . 0.50 max 0.50 max 1.31.9 . . .Tantalum . . . . . . . . 1.52.2 . .Nitrogen . . . . . . 0.020.15A
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