SAE AMS 4601-2011 Aluminum Alloy Sheet and Plate 6 3Cu 0 30Mn 0 06Ti 0 10V 0 18Zr Solution Heat Treated Cold Worked and Naturally Aged (2219-T31 T-351)《固溶热处理 冷加工和自然老化(2219-T31 T-35.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 reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2011 SAE International All rights reserved. No part of this publication m

3、ay 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 (outside U

4、SA) 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:/www.sae.org/technical/standards/AMS4601AEROSPACEMATERIALSPECIFICATIONAMS4601 Issued 2011-07 Aluminum Alloy, Sheet and Plate 6

5、.3Cu - 0.30Mn - 0.06Ti - 0.10V - 0.18Zr Solution Heat Treated, Cold Worked and Naturally Aged (2219 -T31/-T351) (Composition similar to UNS A92219) RATIONALE AMS4601 is a new specification for 2219T31/-T351 sheet and plate to facilitate cancellation of AMS4295 and AMS-QQ-A-250/30. 1. SCOPE 1.1 Form

6、This specification covers an aluminum alloy in the form of sheet and plate. 1.2 Application This product form has been used typically for structural parts requiring high strength up to 500 F (260 C) after proper precipitation heat treatment and which may require forming or welding during fabrication

7、, 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; ARP823 recommends practices to minimize such conditions. 2. APPLICABLE DOCUMENTS The issue of the following documents in effect

8、 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 been speci

9、fied, 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 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org.AMS2355 Quality Assurance, Sampling and Testing,

10、 Aluminum Alloys and Magnesium Alloy, Wrought Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings AMS2770 Heat Treatment of Wrought Aluminum Alloy Parts Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted with

11、out license from IHS-,-,-SAE AMS4601 Page 2 of 6 AMS2772 Heat Treatment of Aluminum Alloy Raw Materials 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

12、 Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org.ASTM B 594 Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications ASTM B 666/B 666M Identification Marking of Aluminum Products 2.3 ANSI Publications Available from American National

13、 Standards Institute, 25 West 43rd Street, New York, NY 10036-8002, Tel: 212-642-4900, www.ansi.org.ANSI H35.2 Dimensional Tolerances for Aluminum Mill Products ANSI H35.2M Dimensional Tolerances for Aluminum Mill Products (Metric) 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the perce

14、ntages by weight shown in Table 1, determined in accordance with AMS2355. TABLE 1 - COMPOSITION Element min max Silicon - 0.20 Iron - 0.30 Copper 5.8 6.8 Manganese 0.20 0.40Magnesium - 0.02 Zinc - 0.10 Titanium 0.02 0.10Vanadium 0.05 0.15 Zirconium 0.10 0.25Other Elements, each - 0.05 Other Elements

15、, total - 0.15 Aluminum remainder 3.2 Condition Product shall be supplied in one of the following conditions as specified by purchaser. 3.2.1 Sheet Solution heat treated, cold worked and naturally aged to the T31 temper (See AS9100). Copyright SAE International Provided by IHS under license with SAE

16、Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS4601 Page 3 of 6 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 temper T351 (See AS1990). 3.2.2.1 Plate sh

17、all receive no further straightening operations after stretching. 3.3 Properties Product shall conform to the following requirements, determined on the mill produced size in accordance with AMS2355. In addition, test specimens in the T31 and T351 condition shall not be required to be tested within 4

18、 days after completion of the heat treatment. If the manufacturer so elects, samples may be tested after less than 4 days aging, but if they fail to show the specified properties, the test samples may be discarded and additional specimens may be tested after 4 days aging. These specimens shall be ta

19、ken from the same locations in the production lot or sample from which the prior specimens were taken. 3.3.1 As Received 3.3.1.1 Tensile Properties Shall be as shown in Table 2 (See 8.2). All values are minimum, unless otherwise specified. TABLE 2A - TENSILE PROPERTIES, INCH/POUND UNITS Temper Nomin

20、al Thickness Inches Tensile Strength ksi Yield Strength at 0.2% Offset ksi Elongation in 2 inches or 4D %T31 0.020 to 0.039, inclOver 0.039 to 0.249, incl46.0 46.0 29.0 28.0 810 T351 0.250 to 2.000, inclOver 2.000 to 3.000, inclOver 3.000 to 4.000, inclOver 4.000 to 5.000, inclOver 5.000 to 6.000, i

21、ncl46.0 44.0 42.0 40.0 39.0 28.0 28.0 27.0 26.0 25.0 10 10 998TABLE 2B - TENSILE PROPERTIES, SI UNITS Temper Nominal Thickness MillimetersTensile Strength MPaYield Strength at 0.2% Offset MPaElongation in 50.8 mm or 4D %T31 0.51 to 0.99, incl Over 0.99 to 6.32, incl 317 317 200 193 810 T351 6.35 to

22、50.80, incl Over 50.80 to 76.20, incl Over 76.20 to 101.60, incl Over 101.60 to 127.00, incl Over 127.00 to 152.40, incl 317 303 290 276 269 193 193 186 179 172 10 10 998Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without li

23、cense from IHS-,-,-SAE AMS4601 Page 4 of 6 3.3.2 After Precipitation Heat Treatment 3.3.2.1 Tensile Properties 3.3.2.1.1 Product, as received by purchaser in the -T31 or -T351 conditions, without the subsequent imposition of cold working or forming operations after precipitation heat treatment in ac

24、cordance with time and temperature parameters of AMS2770 to -T81 or -T851 condition respectively, shall have the tensile properties shown in Table 3 (See 8.2). All values are minimum, unless otherwise specified. TABLE 3A - TENSILE PROPERTIES, INCH/POUND UNITS Temper Nominal Thickness Inches Tensile

25、Strength ksi Yield Strength at 0.2% Offset ksi Elongation in 2 inches or 4D %T81 0.020 to 0.039, inclOver 0.039 to 0.249, incl62.0 62.0 46.0 46.0 67T851 0.250 to 1.000, inclOver 1.000 to 2.000, inclOver 2.000 to 3.000, inclOver 3.000 to 4.000, inclOver 4.000 to 5.000, inclOver 5.000 to 6.000, incl62

26、.0 62.0 62.0 60.0 59.0 57.0 46.0 46.0 45.0 44.0 43.0 42.0 876554TABLE 3B - TENSILE PROPERTIES, SI UNITS Temper Nominal Thickness MillimetersTensile Strength MPaYield Strength at 0.2% Offset MPaElongation in 50.8 mm or 4D %T81 0.51 to 0.99, incl Over 0.99 to 6.32, incl 427 427 317 317 67T851 6.35 to

27、25.40, incl Over 25.40 to 50.80, incl Over 50.80 to 76.20, incl Over 76.20 to 101.60, incl Over 101.60 to 127.00, incl Over 127.00 to 152.40, incl 427 427 427 414 407 393 317 317 310 303 296 290 8765543.3.2.2 Stress-Corrosion Cracking Resistance Specimens, cut from plate 0.750 inch (19.05 mm) and ov

28、er in nominal thickness, supplied in the T351 condition, shall show no evidence of stress-corrosion cracking when stressed in the short-transverse direction (perpendicular to grain flow) to 75% of the yield strength shown for that condition in Table 2 (See 8.1) after precipitation heat treatment in

29、accordance with the time and temperature parameters of AMS2770 to T851 condition. 3.4 Quality 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 When specified, plate s

30、hall be subjected to ultrasonic inspection in accordance with ASTM B 594, and shall meet the requirements shown in Table 4. Ultrasonic requirements for plate exceeding 4.500 inches thick shall be agreed upon by purchaser and supplier. Copyright SAE International Provided by IHS under license with SA

31、ENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS4601 Page 5 of 6 TABLE 4 - ULTRASONIC CLASS Nominal Thickness Inches Nominal Thickness Millimeters Class 0.500 to 1.499, incl 12.70 to 38.07, incl B Over 1.499 to 3.000, incl Over 38.07 to 76.20, incl A Over 3

32、.000 to 4.500, incl Over 76.20 to 114.30, incl B 3.5 Tolerances Shall conform to all applicable requirements of ANSI H35.2 or ANSI H35.2M. 4. QUALITY ASSURANCE PROVISIONS 4.1 Responsibility for Inspection The vendor of the product shall supply all samples for vendors tests and shall be responsible f

33、or 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), as-received tensile propertie

34、s (3.3.1.1), precipitation heat treated tensile properties (3.3.2.1), when specified, ultrasonic inspection (3.4.1) and tolerances (3.5) are acceptance tests and except for composition, shall be performed on each inspection lot. 4.2.2 Periodic Test Stress-corrosion cracking resistance (3.3.2.2) is a

35、 periodic test and shall be performed at a frequency selected by the vendor unless frequency of testing is specified 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 co

36、nforms to the composition, tolerances, and ultrasonic testing when specified, and showing the numerical results of tests on each inspection lot to determine conformance to the other acceptance test requirements. This report shall include the purchase order number, inspection lot numbers, condition,

37、AMS4601, 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 Identification Shall be in accordance with ASTM B 666/B 666M. Copyright SAE

38、International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS4601 Page 6 of 6 5.2 Packaging The product shall be prepared for shipment in accordance with commercial practice and in compliance with applicable rules and r

39、egulations pertaining to the handling, packaging, and transportation of the product to ensure carrier acceptance and safe delivery. 6. ACKNOWLEDGMENT A vendor shall mention this specification number and its revision letter in all quotations and when acknowledging purchase orders. 7. REJECTIONS Produ

40、ct not conforming to this specification, or to modifications authorized by purchaser, will be subject to rejection. 8. NOTES 8.1 A change bar (l) 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 pr

41、evious 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 used in original publications, nor in documents that contain editorial changes only. 8.2 Properties in Tables 2 and

42、 4 were not substantiated according to AMS statistical analysis procedures, but were taken from U.S. Federal Specification QQ-A-250/30. 8.3 Terms used in AMS are clarified in ARP1917. 8.4 Dimensions and properties in inch/pound units and Fahrenheit temperatures are primary; dimensions and properties

43、 in SI units and 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: AMS4601 Condition of product desired Product form and size of product desired Quantity of product desired. PREPARED BY AMS COMMITTEE “D” Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-