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 there
2、from, 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 2018 SAE International All rights reserved. No part of this p
3、ublication 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: +1 724-776-497
4、0 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/standards.sae.org/AMS5553H AEROSPACE MATERIAL SPECIFICATION AMS5553 REV. H Issued 1965-02 Reaffirmed 2006-10 Revi
5、sed 2018-01 Superseding AMS5553G Nickel, Sheet and Strip Low (0.02 max) Carbon Annealed (Composition similar to UNS N02201) RATIONALE AMS5553H revises Properties (3.3.1.1), Reports (4.4.1) and Identification (5.1.1), and results from a Five-Year Review and update of this specification. 1. SCOPE 1.1
6、Form This specification covers nickel in the form of sheet and strip 0.001 to 0.250 inch (0.03 to 0.65 mm) inclusive, in nominal thickness (see 8.5). 1.2 Application These products have been used typically for parts requiring excellent corrosion resistance, and/or strong magnetic properties, but usa
7、ge is not limited to such applications. 2. APPLICABLE DOCUMENTS The 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
8、issue is specified. When the referenced document has been cancelled and no superseding document has been specified, the last published issue of that document shall apply. 2.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (insi
9、de USA and Canada) or +1 724-776-4970 (outside USA), www.sae.org. AMS2262 Tolerances Nickel, Nickel Alloy, and Cobalt Alloy Sheet, Strip, and Plate AMS2269 Chemical Check Analysis Limits Nickel, Nickel Alloys, and Cobalt Alloys SAE INTERNATIONAL AMS5553H Page 2 of 5 AMS2371 Quality Assurance Samplin
10、g and Testing Corrosion and Heat-Resistant Steels and Alloys Wrought Products and Forging Stock AMS2807 Identification Carbon and Low-Alloy Steels, Corrosion and Heat-Resistant Steels and Alloys Sheet, Strip, Plate, and Aircraft Tubing ARP1917 Clarification of Terms Used in Aerospace Metals Specific
11、ations AS4194 Sheet and Strip Surface Finish Nomenclature 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM A480/A480M Flat-Rolled Stainless and Heat-Resisting Steel Plate, Sheet, and
12、 Strip ASTM E8/E8M Tension Testing of Metallic Materials ASTM E18 Rockwell Hardness of Metallic Materials ASTM E140 Hardness Conversion Tables for Metals Relationship Among Brinell Hardness, Vickers Hardness, Rockwell Hardness, Superficial Hardness, Knoop Hardness, Scleroscope Hardness, and Leeb Har
13、dness ASTM E384 Microindentation Hardness of Materials 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Table 1, determined by spectrochemical methods, or by other analytical methods acceptable to purchaser. Table 1 - Composition Element Min Max Nickel Ca
14、rbon Manganese Silicon Sulfur Cobalt Iron Copper 99.0 - - - - - - - - 0.02 0.35 0.35 0.010 1.00 0.40 0.25 3.1.1 Check Analysis Composition variations shall meet the applicable requirements of AMS2269. 3.2 Condition Cold rolled, annealed, and, unless annealing is performed in an atmosphere yielding a
15、 bright finish, descaled having a surface appearance in accordance with ASTM A480/A480M and AS4194 comparable to 3.2.1.1 or 3.2.1.2 as applicable. 3.2.1 Sheet No. 2D finish. SAE INTERNATIONAL AMS5553H Page 3 of 5 3.2.2 Strip No. 1 strip finish. 3.3 Properties The product shall conform to the followi
16、ng requirements: 3.3.1 Tensile Properties Shall be as shown in Table 2, determined in accordance with ASTM E8/E8M. 3.3.1.1 Mechanical property requirements for product outside of the range covered by 1.1 shall be agreed upon between purchaser and producer. Table 2 Table 2A - Tensile properties, inch
17、/pound units Nominal Thickness Inch Tensile Strength ksi, Min Yield Strength at 0.2% Offset ksi Elongation in 2 Inches or 4D %, Min 0.001 to 0.010, excl 0.010 to 0.015, incl Over 0.015 to 0.049, incl Over 0.049 to 0.109, incl Over 0.109 to 0.250, incl 45.0 50 50 50 50 - 30.0, max 12.0, min 12.0, min
18、 12.0, min - 30 30 35 40 Table 2B - Tensile properties, SI units Nominal Thickness Millimeters Tensile Strength MPa, Min Yield Strength at 0.2% Offset MPa Elongation in 50.8 mm or 4D %, Min 0.03 to 0.25, excl 0.25 to 0.38, incl Over 0.38 to 1.24, incl Over 1.24 to 2.77, incl Over 2.77 to 6.35, incl
19、310 345 345 345 345 - 207, max 83, min 83, min 83, min - 30 30 35 40 3.3.2 Hardness Shall be not higher than 66 HRB, or equivalent (see 8.2), determined in accordance with ASTM E18; for thin gages where superficial hardness testing is impractical, microhardness testing in accordance with ASTM E384 m
20、ay be used. Product shall not be rejected on the basis of hardness if the tensile properties of 3.3.1 are acceptable, determined on product taken from the same sample as that with nonconforming hardness or from another sample with similar nonconforming hardness. 3.4 Quality The product, as received
21、by purchaser, shall be uniform in quality and condition, sound, and free from foreign materials and from imperfections detrimental to usage of the product. 3.5 Tolerances Shall conform to all applicable requirements of AMS2262. SAE INTERNATIONAL AMS5553H Page 4 of 5 4. QUALITY ASSURANCE PROVISIONS 4
22、1 Responsibility for Inspection The producer of the product shall supply all samples for producers 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 con
23、forms to specified requirements. 4.2 Classification of Tests All technical requirements are acceptance tests and shall be performed on each heat or lot as applicable. 4.3 Sampling and Testing Shall be in accordance with AMS2371. 4.4 Reports The producer of the product shall furnish with each shipmen
24、t a report showing the results of tests for chemical composition 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 shall include the purchase order number, heat and lot numbers, AMS5553H, size, and
25、 quantity. 4.4.1 When material produced to this specification is beyond the sizes allowed in the scope of tables, or other exceptions are taken to the technical requirements listed in Section 3 (see 5.1.1), the report shall contain a statement “This material is certified as AMS5553H(EXC) because of
26、the following exceptions.” and the specific exceptions shall be listed. 4.5 Resampling and Retesting Shall be in accordance with AMS2371. 5. PREPARATION FOR DELIVERY 5.1 Identification Shall be in accordance with AMS2807. 5.1.1 When technical exceptions are taken (see 4.4.1), the material shall be m
27、arked with AMS5553H(EXC). 5.2 Packaging The product shall be 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 acceptance and safe delivery. 6
28、 ACKNOWLEDGMENT A producer shall mention this specification number and its revision letter in all quotations and when acknowledging purchase orders. 7. REJECTIONS Product not conforming to this specification, or to modifications authorized by purchaser, will be subject to rejection. SAE INTERNATION
29、AL AMS5553H Page 5 of 5 8. NOTES 8.1 Revision Indicator A change bar (I) located in the 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 document. An (R) symbol to the left of the document
30、title indicates a complete revision of the document, including technical revisions. Change bars and (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 E140. 8.3 Terms used in AMS are clarifi
31、ed in ARP1917. 8.4 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. 8.5 Unless otherwise
32、specified, the material producer shall work to the revision of AMS5553 in effect on the date of order placement. Unless otherwise specific, material manufactured and certified to the immediately previous revision of AMS5553 may be procured and used until inventory is depleted. 8.6 Purchase documents should specify not less than the following: AMS5553H Product Form and size of product desired Property and acceptance requirements from the cognizant engineering organization applicable to sizes outside the range listed in 1.1 Quantity of product desired PREPARED BY AMS COMMITTEE “F“
