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    SAE AMS 4041R-2012 Aluminum Alloy Sheet and Plate Alclad 4 4Cu - 1 5Mg - 0 60Mn (2024 -T3 Sheet -T351 Plate with 1 % Alclad) Solution Heat Treated Cold Worked and Naturally Aged (U.pdf

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    SAE AMS 4041R-2012 Aluminum Alloy Sheet and Plate Alclad 4 4Cu - 1 5Mg - 0 60Mn (2024 -T3 Sheet -T351 Plate with 1 % Alclad) Solution Heat Treated Cold Worked and Naturally Aged (U.pdf

    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 2017 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/AMS4041R AEROSPACE MATERIAL SPECIFICATION AMS4041 REV. R Issued 1941-11 Revised 2012-07 Reaffir

    5、med 2017-11 Superseding AMS4041P Aluminum Alloy, Sheet and Plate, Alclad 4.4Cu - 1.5Mg - 0.60Mn (2024, -T3 Sheet/-T351 Plate with 1% Alclad) Solution Heat Treated, Cold Worked and Naturally Aged (Composition similar to UNS A82024) RATIONALE AMS4041R has been reaffirmed to comply with the SAE Five-Ye

    6、ar Review policy. 1. SCOPE 1.1 Form This specification covers an aluminum alloy in the form of alclad sheet and plate supplied in the T3/-T351 temper. 1.2 Supersession Notice Requirements for thin gage sheet (0.008 to 0.187 inch) in accordance with AMS4041 are superseded by AMS4462. AMS-QQ-A-250/5 a

    7、nd AMS4462 have the same requirements for alclad thickness and tensile properties for material less than 0.187” in thickness. 1.2.1 AMS4041 covers alclad material for sheet greater than 0.187 inch, and plate. The cladding thickness is minimized to provide a commensurate increase in tensile propertie

    8、s for this alclad reduction. Use of this product is not recommended without proper evaluation of corrosion resistance. 1.3 Application These products have been used typically for high strength parts requiring higher yield strength than is afforded by naturally aged tempers of this alloy and maximum

    9、corrosion resistance and whose fabrication does not involve welding, but usage 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

    10、 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 been specified, the last published issue of that document shall apply. 2.1 SAE Publications Available from SAE International

    11、, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 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 Welde

    12、d Rings AMS2772 Heat Treatment of Aluminum Alloy Raw Materials AS1990 Aluminum Alloy Tempers 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 B 594 Ultrasonic Inspection of Aluminum-

    13、Alloy Wrought Products for Aerospace Applications ASTM B 660 Packaging/Packing of Aluminum and Magnesium Products ASTM B 666/B 666M Identification Marking of Aluminum and Magnesium Alloy Products 2.3 ANSI Publications Available from American National Standards Institute, 25 West 43rd Street, New Yor

    14、k, NY 10036, Tel: 212-642-4900, www.ansi.org. ANSI H 35.2 Dimensional Tolerances for Aluminum Mill Products ANSI H 35.2M Dimensional Tolerances for Aluminum Mill Products (Metric) 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight as shown in Tables 1, determined in

    15、 accordance with AMS2355. TABLE 1A COMPOSITION, CORE (2024) Element min max Silicon - 0.50 Iron - 0.50 Copper 3.8 4.9 Manganese 0.30 0.9 Magnesium 1.2 1.8 Chromium - 0.10 Zinc - 0.25 Titanium - 0.15 Other Elements, each - 0.05 Other Elements, total - 0.15 Aluminum remainder SAE INTERNATIONAL AMS4041

    16、R Page 2 of 6_ TABLE 1B COMPOSITION, CLADDING (1230) Element min max Iron + Silicon - 0.70 Copper - 0.10 Manganese - 0.05 Magnesium - 0.05 Zinc - 0.10 Titanium - 0.03 Other Elements, each - 0.03 Aluminum 99.30 - 3.2 Condition The product shall be supplied in the following condition: 3.2.1 Sheet Solu

    17、tion heat treated, cold worked and naturally aged to the T3 temper in accordance with AMS2772 (See AS1990). 3.2.2 Plate Solution heat treated, stretched to produce a nominal permanent set of 2% but not less than 1-1/2% nor more than 3%, and naturally aged to the T351 temper in accordance with AMS277

    18、2 (See AS1990). 3.2.2.1 Plate shall receive no further straightening operations after stretching. 3.3 Properties The product shall conform to the following requirements, determined in accordance with AMS2355 on the mill produced size. 3.3.1 Tensile Properties Shall be as shown in Table 2 (See 8.3).

    19、TABLE 2A MINIMUM TENSILE PROPERTIES, INCH/POUND UNITS Temper Nominal Thickness, Inches Tensile Strength, ksi Yield Strength at 0.2% Offset, ksi Elongation in 2 inches or 4D, % -T3 Over 0.187 to 0.249, incl 63.0 41.0 15 -T351 0.250 to 0.499, incl Over 0.499 to 1.000, incl Over 1.000 to 1.500, incl Ov

    20、er 1.500 to 2.000, incl Over 2.000 to 3.000, incl Over 3.000 to 4.000, incl 63.0 63.0 62.0 62.0 60.0 57.0 41.0 42.0 42.0 42.0 42.0 41.0 12 8 7 6 4 4 SAE INTERNATIONAL AMS4041R Page 3 of 6_ TABLE 2B MINIMUM TENSILE PROPERTIES, SI UNITS Temper Nominal Thickness, Millimeters Tensile Strength, mPa Yield

    21、 Strength at 0.2% Offset, mPa Elongation in 50.8 mm or 4D, % -T3 Over 4.750 to 6.324, incl 434 283 15 -T351 6.350 to 12.675, incl Over 12.675 to 25.400, incl Over 25.400 to 38.100, incl Over 38.100 to 50.800, incl Over 50.800 to 76.200, incl Over 76.200 to 101.600, incl 434 434 428 428 414 393 283 2

    22、90 290 290 290 283 12 8 7 6 4 4 3.3.2 Bending Product shall withstand, without cracking, bending at room temperature through an angle of 180 degrees around a diameter equal to the bend factor shown in Table 3 times the nominal thickness of the product with axis of bend parallel to the direction of r

    23、olling. TABLE 3 BENDING PARAMETERS Nominal Thickness; Inches Nominal Thickness; Millimeters Bend Factor Over 0.187 to 0.249, incl Over 0.249 to 0.499, incl Over 4.750 to 6.324, incl Over 6.324 to 12.675, incl 8 10 3.3.3 Cladding Thickness The aluminum alloy plates that are bonded to the two sides of

    24、 the aluminum alloy (2024) ingot or slab, to form a composite that is to be rolled, shall each have a thickness as specified in Table 4. TABLE 4 CLADDING THICKNESS Nominal Thickness, Inch Nominal Thickness, mm Average Cladding Thickness Per Side; % of Total Thickness; minimum Average Cladding Thickn

    25、ess Per Side; % of Total Thickness; maximum Over 0.187 to 0.499, incl Over 0.499 Over 4.750 to 12.675, incl Over 12.675 1.2 1.2 - 3.0 3.4 Quality The product, as received by purchaser, shall be uniform in quality and condition, sound, and free from foreign materials and from imperfections detrimenta

    26、l to usage of the product. 3.5 Tolerances Shall conform to all applicable requirements of ANSI H 35.2/H 35.2M. SAE INTERNATIONAL AMS4041R Page 4 of 6_ 4. QUALITY ASSURANCE PROVISIONS 4.1 Responsibility for Inspection The vendor of the product shall supply all samples for vendors tests and shall be r

    27、esponsible 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 4.2.1 Acceptance Tests Composition (3.1), tensile propertie

    28、s (3.3.1), and tolerances (3.5) are acceptance tests and except for composition, shall be performed on each lot. 4.2.2 Periodic Tests Bending (3.3.2) and cladding thickness (3.3.3) are periodic tests and shall be performed at a frequency selected by the vendor unless frequency of testing is specifie

    29、d by purchaser. 4.3 Sampling and Testing Shall be in accordance with AMS2355. 4.4 Reports The vendor of the product shall furnish with each shipment a report stating that the product conforms to the composition and tolerances, and showing numerical results of tests for the other acceptance test requ

    30、irements. This report shall include the purchase order number, lot number, AMS4041R, size, and quantity. The report shall also identify the producer, the product form, and the size of the mill product. 4.5 Resampling and Retesting Shall be in accordance with AMS2355. 5. PREPARATION FOR DELIVERY 5.1

    31、Identification Shall be in accordance with ASTM B 666/B 666M. 5.2 Packaging 5.2.1 Product shall be protected from damage during storage and shipment by a method determined by the vendor unless specified by purchaser. Examples of typical protective methods include but are not limited to interleaving

    32、with paper or oiling of the surface. 5.2.2 The product shall be prepared for shipment in accordance with ASTM B 660 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. ACKN

    33、OWLEDGMENT A vendor shall mention this specification number and its revision letter in all quotations and when acknowledging purchase orders. SAE INTERNATIONAL AMS4041R Page 5 of 6_ 7. REJECTIONS Product not conforming to this specification, or to modifications authorized by purchaser, will be subje

    34、ct to rejection. 8. NOTES 8.1 A change bar (|) 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 title indicates a complete

    35、 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 Terms used in AMS are clarified in ARP1917. 8.3 Dimensions and properties in inch/pound units and Fahrenheit temperatures are

    36、 primary; dimensions and properties in SI units and Celsius temperatures are shown 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: AMS4041R Product form and size of product desired Quantity of product desired. PREPARED BY AMS COMMITTEE “D“ SAE INTERNATIONAL AMS4041R Page 6 of 6_


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