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/AMS5605FRATIONALEAMS5605F revises Reports (4.4) and is a Five Year Review and update of this
5、specification.1. SCOPE1.1 FormThis specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate 1.00 inch (25.4 mm) and under in nominal thickness.1.2 ApplicationThese products have been used typically for parts requiring good machinability and high strengt
6、h at room and cryogenic temperatures and for short-time use up to 1000 F (538 C), particularly for those parts which are formed or welded and then heat treated to develop required properties, but usage is not limited to such applications.2. APPLICABLE DOCUMENTSThe issue of the following documents in
7、 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 specified. When the referenced document has been cancelled and no superseding document has bee
8、n specified, the last published issue of that document shall apply.AEROSPACE MATERIAL SPECIFICATIONAMS5605REV. FIssued 1971-11Revised 2013-08Superseding AMS5605ENickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate41.5Ni - 16Cr - 37Fe - 2.9Cb (Nb) - 1.8TiConsumable Electrode or Vacuum
9、Induction Melted1800 F (982 C) Solution Heat Treated(Composition similar to UNS N09706)SAE INTERNATIONAL AMS5605F Page 2 of 72.1 SAE PublicationsAvailable from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA
10、), or www.sae.org.AMS2262 Tolerances, Nickel, Nickel Alloy, and Cobalt Alloy Sheet, Strip, and PlateAMS2269 Chemical Check Analysis Limits, Nickel, Nickel Alloys and Cobalt AlloysAMS2371 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steels and Alloys, Wrought Products and Forg
11、ing StockAMS2807 Identification, Carbon and Low-Alloy Steels, Corrosion and Heat-Resistant Steels and Alloys, Sheet, Strip, Plate, and Aircraft TubingAS4194 Sheet and Strip Surface Finish Nomenclature2.2 ASTM PublicationsAvailable from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West C
12、onshohocken, PA 19428-2959, Tel: 610-832-9585, or www.astm.org.ASTM A 480/A 480M Flat-Rolled Stainless and Heat-Resisting Steel Plate, Sheet, and StripASTM E 8/E 8M Tension Testing of Metallic MaterialsASTM E 18 Rockwell Hardness of Metallic MaterialsASTM E 112 Determining Average Grain SizeASTM E 2
13、90 Bend Test of Materials for DuctilityASTM E 354 Chemical Analysis of High-Temperature, Electrical, Magnetic, and Other Similar Iron, Nickel, and Cobalt AlloysASTM E 384 Knoop and Vickers Hardness of Materials3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the percentages by weight shown i
14、n Table 1, determined by wet chemical methods in accordance with ASTM E 354, by spectrochemical methods, or by other analytical methods acceptable to purchaser.SAE INTERNATIONAL AMS5605F Page 3 of 7TABLE 1 COMPOSITIONElement min maxCarbon - 0.06Manganese - 0.35Silicon - 0.35Phosphorus - 0.020Sulfur
15、- 0.015Chromium 14.50 17.50Nickel 39.00 44.00Columbium (Niobium) 2.50 3.30Tantalum - 0.05Titanium 1.50 2.00Aluminum - 0.40Boron - 0.006Copper - 0.30Iron remainder3.1.1 Check AnalysisComposition variations shall meet the applicable requirements of AMS2269.3.2 Melting PracticeAlloy shall be produced b
16、y multiple melting using consumable electrode practice in the remelt cycle or shall be induction melted under vacuum. If consumable electrode remelting is not performed in vacuum, electrodes which have been produced by vacuum induction melting shall be used for remelting.3.3 ConditionThe product sha
17、ll be supplied in the following condition:3.3.1 Sheet and StripCold rolled, solution heat treated free from continuous carbide network and, unless solution heat treatment is performed in an atmosphere yielding a bright finish, descaled having a surface appearance comparable to the following commerci
18、al corrosion resistant steel finishes as described in ASTM A 480/A 480M and AS4194 and the following:3.3.1.1 SheetNo. 2D finish.3.3.1.2 StripNo. 1 Strip finish.3.3.2 PlateHot rolled, solution heat treated, and descaled.SAE INTERNATIONAL AMS5605F Page 4 of 73.4 Heat Treatment No specific solution hea
19、t treatment is specified but it is recommended that the product be solution heat treated by heating in a suitable protective atmosphere to a temperature within the range 1750 to 1850 F (954 to 1010 C), holding at the selected temperature within 25 F (14 C) for a time commensurate with section thickn
20、ess but not less than five minutes, and cooling at a rate equivalent to an air cool or faster.3.5 Properties The product shall conform to the following requirements:3.5.1 As Solution Heat Treated3.5.1.1 Tensile Properties Shall be as shown in Table 2, determined in accordance with ASTM E 8/E 8M.TABL
21、E 2A - TENSILE PROPERTIES, INCH/POUND UNITSNominal ThicknessInchTensileStrengthksi, maxYield Strengthat 0.2% Offsetksi, maxElongation in2 Inches or 4D%, minUp to 0.1875, excl0.1875 and over13014080.090.03030TABLE 2B - TENSILE PROPERTIES, SI UNITSNominal ThicknessMillimetersTensileStrengthMPa, maxYie
22、ld Strengthat 0.2% OffsetMPa, maxElongation in50.8 mm or 4D%, minUp to 4.762, excl4.762 and over89696555262130303.5.1.2 Hardness Shall be not higher than shown in Table 3, or equivalent (See 8.2), determined in accordance with ASTM E 18; for thin gages, where superficial hardness testing is impracti
23、cal, microhardness testing in accordance with ASTM E 384 may be used. Product shall not be rejected on the basis of hardness if the tensile properties of 3.5.1.1 are acceptable, determined on specimens taken from the same sample as that with nonconforming hardness or from another sample with similar
24、 nonconforming hardness. TABLE 3 - MAXIMUM HARDNESSNominal ThicknessInchNominal ThicknessMillimeters HardnessUp to 0.1875, excl0.1875 and overUp to 4.762, excl4.762 and over102 HRB25 HRC3.5.1.3 BendingProduct under 0.1875 inch (4.762 mm) in nominal thickness shall be tested in accordance with ASTM E
25、 290 using a sample nominally 0.75 inch (19.0 mm) in width, with its axis of bending parallel to the direction of rolling, and shall withstand, without cracking, when bending at room temperature through an angle of 180 degrees around a diameter equalto the bend factor shown in Table 4 times the nomi
26、nal thickness of the product. In case of dispute, the results of tests using the guided bend test of ASTM E 290 shall govern.SAE INTERNATIONAL AMS5605F Page 5 of 7TABLE 4 - BENDING PARAMETERSNominal ThicknessInchNominal ThicknessMillimeters Bend FactorUp to 0.050, inclOver 0.050 to 0.1875, exclUp to
27、 1.27, inclOver 1.27 to 4.762, excl123.5.1.4 Average Grain SizeShall be as shown in Table 5, determined in accordance with ASTM E 112.TABLE 5 - AVERAGE GRAIN SIZENominal ThicknessInchNominal ThicknessMillimetersASTMGrain Size No.Up to 0.1875, excl0.1875 and overUp to 4.762, excl4.762 and over5 or fi
28、ner4 or finer3.5.2 After Precipitation Heat TreatmentThe product shall have the following properties after being precipitation heat treated by heating to 1350 F 15 (732 C 8), holding at heat for 8 hours 0.25, cooling at a rate of 100 F (56 C) degrees per hour to 1150 F 15 (621 C 8), holding at 1150
29、F 15 (621 C 8) for 8 hours 0.25, and cooling in air. Instead of the 100 F (56 C) degrees per hour cooling rate to 1150 F 15 (621 C 8), the furnace cooling may be at any rate provided the time at 1150 F 15 (621 C 8) is adjusted to give a total precipitation heat treatment time of not less than 18 hou
30、rs.3.5.2.1 Tensile PropertiesShall be as shown in Table 6, determined in accordance with ASTM E 8/E 8M.TABLE 6A - MINIMUM TENSILE PROPERTIES, INCH/POUND UNITSNominal ThicknessInchTensileStrengthksiYield Strengthat 0.2% OffsetksiElongation in2 Inches or 4D%Up to 0.1875, excl0.1875 and over17517014514
31、51212TABLE 6B - MINIMUM TENSILE PROPERTIES, SI UNITSNominal ThicknessMillimetersTensileStrengthMPaYield Strengthat 0.2% OffsetMPaElongation in50.8 mm or 4D%Up to 4.762, excl4.762 and over12071172100096512123.5.2.2 HardnessShall be not lower than 34 HRC, or equivalent (See 8.2), determined in accorda
32、nce with ASTM E 18; for thin gages, where superficial hardness testing is impractical, microhardness testing in accordance with ASTM E 384 may be used. Product shall not be rejected on the basis of hardness if the tensile properties of 3.5.2.1 are acceptable, determined on specimens taken from the s
33、ame sample as that with nonconforming hardness or from another sample with similar nonconforming hardness.SAE INTERNATIONAL AMS5605F Page 6 of 73.6 QualityThe product, as received by purchaser, shall be uniform in quality and condition, sound, and free from foreign materials and from imperfections d
34、etrimental to usage of the product.3.7 Tolerances Shall conform to all applicable requirements of AMS2262.4. QUALITY ASSURANCE PROVISIONS4.1 Responsibility for InspectionThe vendor of the product shall supply all samples for vendors tests and shall be responsible for the performance of all required
35、tests. Purchaser reserves the right to sample and to perform any confirmatory testing deemed necessary to ensure that the product conforms to specified requirements.4.2 Classification of TestsAll technical requirements are acceptance tests and shall be performed on each heat or lot as applicable.4.3
36、 Sampling and TestingShall be in accordance with AMS2371.4.4 ReportsThe vendor of the product shall furnish with each shipment a report showing producer identity and country where the metal was melted (e.g., final melt in the case of metal processed by multiple melting operations), the results of te
37、sts for composition of each heat and for tensile properties, hardness, bending and average grain size solution heat treated, and for tensile properties and hardness precipitation heat treated, and stating the product conforms to the other technical requirements. This report shall include the purchas
38、e order number, heat and lot numbers, AMS5605F, solution heat treatment temperature used, size, and quantity.4.5 Resampling and RetestingShall be in accordance with AMS2371.5. PREPARATION FOR DELIVERY5.1 IdentificationShall be in accordance with AMS2807.5.2 PackagingThe product shall be prepared for
39、 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 acceptance and safe delivery.6. ACKNOWLEDGMENTA vendor shall mention this specification number and its r
40、evision letter in all quotations and when acknowledging purchase orders.SAE INTERNATIONAL AMS5605F Page 7 of 77. REJECTIONSProduct not conforming to this specification, or to modifications authorized by purchaser, will be subject to rejection.8. NOTES8.1 A change bar (|) located in the left margin i
41、s for the convenience of the user in locating areas where technical revisions, not editorial changes, have been made to the previous issue of this document. An (R) symbol to the left of the document title indicates a complete revision of the document, including technical revisions. Change bars and (
42、R) are not used in original publications, nor in documents that contain editorial changes only.8.2 Hardness conversion tables for metals are presented in ASTM E 140.8.3 Terms used in AMS are clarified in ARP1917.8.4 Dimensions and properties in inch/pound units and the Fahrenheit temperatures are pr
43、imary; dimensions andproperties in SI units and the Celsius temperatures are shown as the approximate equivalents of the primary units and are presented only for information.8.5 Purchase documents should specify not less than the following:AMS5605FProduct form and size of product desiredQuantity of product desired.PREPARED BY AMS COMMITTEE “F“
