1、_SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising theref
2、rom, is the sole responsibility of the user.”SAE reviews each technical report at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions.Copyright 2013 SAE InternationalAll rights reserved. No part of this publi
3、cation may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE.TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada)Tel: +1 724-776-4970 (out
4、side USA)Fax: 724-776-0790Email: CustomerServicesae.orgSAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedbackon this Technical Report, please visithttp:/www.sae.org/technical/standards/AMS5614EAEROSPACE MATERIAL SPECIFICATIONAMS5614 REV. EIssued 1952-06Revised 2001-11Reaffirmed
5、 2013-08Superseding AMS5614DSteel, Corrosion and Heat Resistant, Bars, Wire, and Forgings12Cr - 0.50MoAnnealed(Composition similar to UNS S41025)RATIONALEAMS5614E has been reaffirmed to comply with the SAE 5-year Review policy.1. SCOPE1.1 FormThis specification covers a corrosion and heat resistant
6、steel in the form of bars, wire, forgings, and forging stock.1.2 ApplicationThese products have been used typically for parts, such as compressor blades and vanes, requiring oxidation resistance up to 1000 F (538 C), useful at the higher temperatures only when stresses are low, but usage is not limi
7、ted to such applications.2. APPLICABLE DOCUMENTSThe issue of the following documents in effect on the date of the purchase order forms a part of this specification to the extent specified herein. The supplier may work to a subsequent revision of a document unless a specific document issue is specifi
8、ed. When the referenced document has been canceled and no superseding document has been specified, the last published issue of that document shall apply.2.1 SAE PublicationsAvailable from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001 or www.sae.org.AMS 2241 Tolerances, Corrosion and Heat Re
9、sistant Steel, Iron Alloy, Titanium, and Titanium Alloy Bars and WireMAM 2241 Tolerances, Metric, Corrosion and Heat Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Bars and WireSAE INTERNATIONAL AMS5614E Page 2 of 6AMS 2248 Chemical Check Analysis Limits, Corrosion and Heat Resistant Stee
10、ls and Alloys, Maraging and Other Highly-Alloyed Steels, and Iron AlloysAMS 2371 Quality Assurance Sampling and Testing, Corrosion and Heat Resistant Steels and Alloys, Wrought Products and Forging StockAMS 2374 Quality Assurance Sampling and Testing, Corrosion and Heat Resistant Steel and Alloy For
11、gingsAMS 2806 Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat Resistant Steels and AlloysAMS 2808 Identification, Forgings2.2 ASTM PublicationsAvailable from ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959 or www.astm.org.AS
12、TM A 370 Mechanical Testing of Steel ProductsASTM E 353 Chemical Analysis of Stainless, Heat-Resisting, Maraging, and Other Similar Chromium-Nickel-Iron AlloysASTM E 381 Macroetch Testing Steel Bars, Billets, Blooms, and Forgings3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the percentage
13、s by weight shown in Table 1, determined by wet chemical methods in accordance with ASTM E 353, by spectrochemical methods, or by other analytical methods acceptable to purchaser.TABLE 1 - COMPOSITIONElement min maxCarbonManganeseSiliconPhosphorusSulfurChromiumMolybdenumNickelCopperAluminumTinNitrog
14、en0.070.30-11.500.40-0.120.600.350.0400.03012.500.600.600.500.050.050.083.1.1 Check AnalysisComposition variations shall meet the applicable requirements of AMS 2248.3.2 ConditionThe product shall be supplied in the following condition; hardness and tensile strength shall be determined in accordance
15、 with ASTM A 370:SAE INTERNATIONAL AMS5614E Page 3 of 63.2.1 BarsHot rolled, annealed, and either descaled or ground, having hardness not higher than 223 HB, or equivalent (See 8.2).3.2.2 WireCold drawn and annealed having tensile strength not higher then 115 ksi (793 MPa), or equivalent hardness (S
16、ee 8.3).3.2.3 ForgingsAs ordered.3.2.4 Forging StockAs ordered by the forging manufacturer.3.3 PropertiesThe product shall conform to the following requirements; tensile and hardness testing shall be performed in accordance with ASTM A 370:3.3.1 MacrostructureVisual examination of transverse full cr
17、oss sections from bars, wire, billets, and forging stock, etched in hot hydrochloric acid in accordance with ASTM E 381 shall show no pipe or cracks. Porosity, segregation, inclusions, and other imperfections shall be no worse than the macrographs of ASTM E 381 acceptable to purchaser.3.3.2 Response
18、 to Heat TreatmentProduct 7.0 inches (178 mm) and under in nominal diameter or least distance between parallel sides shall have the following properties after being hardened by heating to 1750 F 10 (954 C 5), holding at heat for 25 to 30 minutes, and cooling in air and tempered by heating to a tempe
19、rature not lower than 1100 F (593 C), holding at heat for 60 minutes 5, and cooling in air:3.3.2.1 Tensile PropertiesShall be as shown in Table 2; requirements apply in both the longitudinal and transverse directions but tests in the transverse direction need be made only on product from which a spe
20、cimen not less than 2.50 inches (63.5 mm) in length can be taken midway between the surface and the center. Tests in the longitudinal direction are not required on product tested in the transverse direction.TABLE 2 - MINIMUM TENSILE PROPERTIESProperty ValueTensile Strength 100 ksi (689 MPa)Yield Str
21、ength at 0.2% Offset 80 ksi (552 MPa)Elongation in 4D 21%Reduction of Area 60%3.3.2.2 HardnessProduct, 0.375 inch (9.52 mm) and under in nominal diameter or least distance between parallel sides and specimens 0.375 inch 0.010 (9.52 mm 0.25) thick cut from larger product, shall have hardness of 207 t
22、o 248 HB, or equivalent (See 8.2).SAE INTERNATIONAL AMS5614E Page 4 of 63.4 QualityThe product, as received by purchaser, shall be uniform in quality and condition, sound, and free from foreign materials and from imperfections detrimental to usage of the product.3.4.1 Grain flow of die forgings, exc
23、ept in areas which contain flash-line end grain, shall follow the general contour of the forgings showing no evidence of reentrant grain flow.3.5 TolerancesBars and wire shall conform to all applicable requirements of AMS 2241 or MAM 2241.4. QUALITY ASSURANCE PROVISIONS4.1 Responsibility for Inspect
24、ionThe vendor of the product shall supply all samples for vendors tests and shall be responsible for the performance of all required tests. Purchaser reserves the right to sample and to perform any confirmatory testing deemed necessary to ensure that the product conforms to specified requirements.4.
25、2 Classification of Tests4.2.1 Acceptance TestsComposition (3.1), condition (3.2), macrostructure (3.3.1), tensile properties (3.3.2.1), hardness (3.3.2.2), and tolerances (3.5) are acceptance tests and shall be performed on each heat or lot as applicable.4.2.2 Periodic TestsGrain flow of die forgin
26、gs (3.4.1) is a periodic test and shall be performed at a frequency selected by the vendor unless a frequency of testing is specified by purchaser.4.3 Sampling and TestingShall be as follows:4.3.1 Bars, Wire, and Forging StockIn accordance with AMS 2371.4.3.2 ForgingsIn accordance with AMS 2374.4.4
27、ReportsThe vendor of the product shall furnish with each shipment a report showing the results of tests for chemical composition and macrostructure of each heat and for tensile properties and hardness of each lot, and stating that the product conforms to the other technical requirements. This report
28、 shall include the purchase order number, heat and lot numbers, AMS 5614E, size, and quantity. If forgings are supplied, the size and melt source of stock used to make the forgings shall also be included.SAE INTERNATIONAL AMS5614E Page 5 of 64.5 Resampling and RetestingShall be as follows:4.5.1 Bars
29、, Wire, and Forging StockIn accordance with AMS 2371.4.5.2 ForgingsIn accordance with AMS 2374.5. PREPARATION FOR DELIVERY5.1 SizesExcept when exact lengths or multiples of exact lengths are ordered, straight bars and wire will be acceptable in mill lengths of 6 to 20 feet (1.8 to 6.1 m) but not mor
30、e than 10% of any shipment shall be supplied in lengths shorter than 10 feet (3 m).5.2 IdentificationShall be as follows:5.2.1 Bars and WireIn accordance with AMS 2806.5.2.2 ForgingsIn accordance with AMS 2808.5.2.3 Forging StockAs agreed upon by purchaser and vendor.5.3 PackagingThe product shall b
31、e prepared for shipment in accordance with commercial practice and in compliance with applicable rules and regulations pertaining to the handling, packaging, and transportation of the product to ensure carrier acceptanceand safe delivery. 6. ACKNOWLEDGMENTA vendor shall mention this specification nu
32、mber and its revision letter in all quotations and when acknowledging purchase orders.7. REJECTIONSProduct not conforming to this specification, or to modifications authorized by purchaser, will be subject to rejection.SAE INTERNATIONAL AMS5614E Page 6 of 68. NOTES8.1 A change bar ( l ) located in t
33、he left margin is for the convenience of the user in locating areas where technical revisions, not editorial changes, have been made to the previous issue of this specification. An (R) symbol to the left of the document title indicates a complete revision of the specification, including technical re
34、visions. Change bars and (R) are not used in original publications, nor in specifications that contain editorial changes only.8.2 Hardness conversion tables for metals are presented in ASTM E 140.8.3 Tensile strength to hardness conversions are presented in ASTM A 370.8.4 Terms used in AMS are clari
35、fied in ARP1917.8.5 Dimensions and properties in inch/pound units and the Fahrenheit temperatures are primary; dimensions and properties in SI units and the Celsius temperatures are shown as the approximate equivalents of the primary units and are presented only for information.8.6 Purchase documents should specify not less than the following:AMS 5614EForm and size or part number of product desiredQuantity of product desired.PREPARED UNDER THE JURISDICTION OF AMS COMMITTEE “F“
