1、_ SAE TechnLFDO6WDQGDUGV%RDUG5XOHVSURYLGHWKDW7KLVUHSRUWLVSXEOLVKHGE 6$(WRDGYDQFHWKHVWDWHRIWHFKQLFDODQGHQJLQHHULQJV ciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any SDWHQWLQIULQJHPHQWDULVLQJWKHUHIURPLVWKHVROHUHVSRQVLELO
2、LWRIWKH XVHU 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 2016 SAE International All rights reserved. No part of this publication may be reproduced, stor
3、ed 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 (outside USA) Fax: 724-776-0790
4、Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AMS4096D AEROSPACE MATERIAL SPECIFICATION AMS4096 REV. D Issued 1969-11 Revised 2016-02 Superseding AMS4096C Alumin
5、um Alloy Sheet and Plate, Alclad 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (Alclad 2219-O) Annealed (Composition similar to UNS A92219) RATIONALE AMS4096D revises Properties (3.3.1.1, 3.3.3, Tables 5 and 7) and Reports (4.4.1), and is a Five Year Review and update of this specification. 1. SCOPE 1.1
6、Form This specification covers an aluminum alloy in the form of sheet and plate 0.020 to 0.499 inch (0.50 to 12.50 mm), inclusive, in nominal thickness, clad on two sides (see 8.3). 1.2 Application This specification has been used typically for parts requiring high strength up to 600 F (315 C). Thes
7、e products are also well suited for cryogenic applications and where welding and maximum corrosion resistance are required, but usage is not limited to such applications. 1.2.1 Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking after
8、heat treatment; ARP823 recommends practices to minimize such conditions. 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 doc
9、ument unless a specific document 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 15
10、096-0001, Tel: 877-606-7323 (inside USA and Canada) or +1 724-776-4970 (outside USA), www.sae.org. AMS2355 Quality Assurance, Sampling and Testing, Aluminum Alloys and Magnesium Alloy, Wrought Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings AMS2772 Heat Treatment of Alumin
11、um Alloy Raw Materials SAE INTERNATIONAL $06 Page 2 of 6 ARP823 Minimizing Stress-Corrosion Cracking in Wrought Heat-Treatable Aluminum Alloy Products AS1990 Aluminum Alloy Tempers 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19
12、428-2959, Tel: 610-832-9585, www.astm.org. ASTM B660 Packaging/Packing of Aluminum and Magnesium Products ASTM B666/B666M Identification Marking of Aluminum and Magnesium Products 2.3 ANSI Accredited Publications Copies of these documents are available online at http:/webstore.ansi.org/. ANSI H35.2
13、Dimensional Tolerance for Aluminum Mill Products ANSI H35.2M Dimensional Tolerances for Aluminum Mill Products, Metric 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the following percentages by weight shown in Table 1 and Table 2, determined in accordance with AMS2355: Table 1 - Composi
14、tion, core (2219) Elements min max Silicon Iron Copper Manganese Magnesium Zinc Titanium Vanadium Zirconium Other Elements, each Other Elements, total Aluminum - - 5.8 0.20 - - 0.02 0.05 0.10 - - remainder 0.20 0.30 6.8 0.40 0.02 0.10 0.10 0.15 0.25 0.05 0.15 Table 2 - Composition, cladding (7072) E
15、lements min max Silicon + Iron Copper Manganese Magnesium Zinc Other Elements, each Other Elements, total Aluminum - - - - 0.8 - - remainder 0.7 0.10 0.10 0.10 1.3 0.05 0.15 SAE INTERNATIONAL $06 Page 3 of 6 3.2 Condition Annealed to the -O condition (see AS1990) in accordance with AMS2772. 3.3 Prop
16、erties The product shall conform to the following requirements, determined in accordance with AMS2355 on the mill product. 3.3.1 As Annealed 3.3.1.1 Tensile Properties Product 0.020 to 0.499 inch (0.50 to 12.50 mm), inclusive, in nominal thickness shall meet the requirements of Table 3. Table 3 - Te
17、nsile properties (-O temper) Tensile Strength, max 32.0 ksi (220 MPa) Yield Strength at 0.2% Offset, max 16.0 ksi (110 MPa) Elongation in 2 in. (50 mm) or 4D, min 12% 3.3.1.2 Bending Product 0.020 to 0.499 inch (0.50 to 12.50 mm) in nominal thickness shall withstand, without cracking, bending at roo
18、m temperature through an angle of 180 degrees around a diameter equal to the bend factor shown in Table 4 times the nominal thickness of the product with axis of bend parallel to the direction of rolling. Table 4 - Bend factors (-O temper) Nominal Thickness Inch Nominal Thickness Millimeters Bend Fa
19、ctor 0.020 to 0.249, incl 0.50 to 6.25, incl 4 Over 0.249 to 0.499, incl Over 6.25 to 12.50, incl 6 3.3.2 Response to Heat Treatment Product in the -O temper shall have the properties shown in Tables 5 and 6 after solution and precipitation heat treatment in accordance with AMS2772 to -T62 temper (s
20、ee AS1990): 3.3.2.1 Tensile Properties Shall be as specified in Table 5. Table 5A - Minimum tensile properties (-T62 temper), inch/pound units Nominal Thickness Inches Tensile Strength ksi, min Yield Strength at 0.2% Offset ksi, min Elongation in 2 Inches or 4D %, min 0.020 to 0.039, incl 44.0 29.0
21、6 Over 0.039 to 0.099, incl 49.0 32.0 7 Over 0.099 to 0.249, incl 51.0 34.0 7 Over 0.249 to 0.499, incl 51.0 34.0 8 SAE INTERNATIONAL $06 Page 4 of 6 Table 5B - Minimum tensile properties (-T62 temper), SI units Nominal Thickness Millimeters Tensile Strength MPa Yield Strength at 0.2% Offset MPa Elo
22、ngation in 50 mm or 4D %, min 0.50 to 1.00, incl 303 200 6 Over 1.00 to 2.50, incl 338 221 7 Over 2.50 to 6.25, incl 352 234 7 Over 6.25 to 12.50, incl 352 234 8 3.3.2.2 Bending Product 0.020 to 0.499 inch (0.50 to 12.50 mm) in nominal thickness shall withstand, without cracking, bending at room tem
23、perature through an angle of 180 degrees around a diameter equal to the bend factor shown in Table 6 times the nominal thickness of the product with axis of bend parallel to the direction of rolling. Table 6 - Bend factors (-T62 temper) Nominal Thickness Inch Nominal Thickness Millimeters Bend Facto
24、r 0.020 to 0.062, incl 0.50 to 1.55, incl 8 Over 0.062 to 0.249, incl Over 1.55 to 6.25, incl 12 Over 0.249 to 0.499, incl Over 6.25 to 12.50, incl 16 3.3.3 Property requirements for product outside the range covered by Tables 3, 4, 5 and 6 shall be agreed upon between purchaser and producer. 3.3.4
25、Cladding Thickness After rolling, the average cladding thickness shall conform to the requirements shown in Table 7. Table 7 - Cladding thickness Nominal Thickness Inch Nominal Width Inches Average Cladding Thickness Per Side % of Total Thickness min Average Cladding Thickness Per Side % of Total Th
26、ickness max 0.020 to 0.039, incl 0.50 to 1.00, incl 8 - Over 0.039 to 0.099, incl Over 1.00 to 2.50, incl 4 - Over 0.099 to 0.499, incl Over 2.50 to 12.50, incl 2 - 3.4 Quality The product, as received by purchaser, shall be uniform in quality and condition, sound, and free from foreign materials an
27、d from internal and external imperfections detrimental to usage of the product. 3.5 Tolerances Shall conform to all applicable requirements of ANSI H35.2 or ANSI H35.2M. SAE INTERNATIONAL $06 Page 5 of 6 4. QUALITY ASSURANCE PROVISIONS 4.1 Responsibility for Inspection The producer of the product sh
28、all 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 conforms to specified requirements. 4.2 Classification of Tests 4.
29、2.1 Acceptance Tests Composition (3.1), tensile properties as annealed (3.3.1.1) and after solution and precipitation heat treatment (3.3.2.1), and tolerances (3.5) are classified as acceptance tests and, except for composition, shall be performed on each lot. 4.2.2 Periodic Tests Bending as anneale
30、d (3.3.1.2), bending after solution and precipitation heat treatment (3.3.2.2) and cladding thickness (3.3.4) are classified as periodic tests and shall be performed at a frequency selected by the producer unless frequency of testing is specified by purchaser. 4.3 Sampling Shall be in accordance wit
31、h AMS2355. 4.4 Reports The producer of the product shall furnish with each shipment a report stating that the product conforms to the chemical composition and tolerances showing the numerical results of tests on each inspection lot to determine conformance to the other acceptance test requirements a
32、nd stating that the product conforms to the other specified requirements. This report shall include the purchase order number, inspection lot number(s), AMS4096D, size, and quantity. The report shall also identify the producer, the mill product form, and the mill produced size. 4.4.1 When product si
33、ze is outside the range covered by 1.1, the report shall contain a statement to that effect. 4.5 Resampling and Retesting Shall be in accordance with AMS2355. 5. PREPARATION FOR DELIVERY 5.1 Identification Shall be in accordance with ASTM B666/B666M. 5.2 Protective Treatment Product shall be protect
34、ed from damage during storage and shipment by a method determined by the producer unless specified by purchaser. Examples of typical methods include but are not limited to interleafing with paper or oiling of the surface. 5.3 Packaging The product shall be prepared for shipment in accordance with AS
35、TM B660/B660M 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. SAE INTERNATIONAL $06 Page 6 of 6 6. ACKNOWLEDGMENT A producer shall mention this specification number and it
36、s revision letter in all quotations and when acknowledging purchase order. 7. REJECTIONS Material not conforming to this specification or to modifications authorized by purchaser will be subject to rejection. 8. NOTES 8.1 Revision Indicator A change bar (l) located in the left margin is for the conv
37、enience 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 (R) are not use
38、d in original publications, nor in documents that contain editorial changes only. 8.2 Terms used in AMS are clarified in ARP1917. 8.3 Dimensions and properties in inch/pound units and the Fahrenheit temperatures are primary; dimensions and properties in SI units and the Celsius temperatures are show
39、n as the approximate equivalents of the primary units and are presented only for information. 8.4 Purchase documents should specify not less than the following: AMS4096D Form and size of product desired Quantity of product desired Property and acceptance requirements from the cognizant engineering organization applicable to sizes outside the range listed in 1.1. PREPARED BY AMS COMMITTEE “D“
