SAE AMS 4164H-2003 Aluminum Alloy Extrusions 4 4Cu - 1 5Mg - 0 60Mn (2024-T3510) Stress-Relief Stretched Unstraightened (UNS A92024)《4 4Cu 1 5Mg 0 60Mn(2024-T3510)应力消除拉伸、非拉直的铝合金挤压制.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 2013 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:/www.sae.org/technical/standards/AMS4164H AEROSPACE MATERIAL SPECIFICATION AMS4164 REV. H Issued 1960-06 Revised 2

5、003-10 Reaffirmed 2013-12 Superseding AMS4164G Aluminum Alloy, Extrusions 4.4Cu - 1.5Mg - 0.60Mn (2024-T3510) Stress-Relief Stretched, Unstraightened (Composition similar to UNS A92024) RATIONALE AMS4164H has been reaffirmed to comply with the SAE five-year review policy. 1. SCOPE: 1.1 Form: This sp

6、ecification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing. 1.2 Application: These products have been used typically for parts subject to excessive warpage during machining, and for parts requiring high strength and whose fabrication does not normally involve

7、 welding, but usage is not limited to such applications. 1.2.1 Certain design and processing procedures may cause these extrusions to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions. 2. APPLICABLE DOCUMENTS: The issue of the following document

8、s 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 issue is specified. When the referenced document has been cancelled and no superseding document has

9、 been specified, the last published issue of that document shall apply. SAE INTERNATIONAL AMS4164H Page 2 of 6 2.1 SAE Publications: Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001 or www.sae.org. AMS 2355 Quality Assurance Sampling and Testing, Aluminum Alloys and Magnesium Al

10、loys, Wrought Products, Except Forging Stock, and Rolled, Forged, or Flash Welded Rings AMS 2772 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

11、 from ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959 or www.astm.org. ASTM B 594 Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications ASTM B 660 Packing/Packaging of Aluminum-Alloy Products for Aerospace Application ASTM B 666/B 666M Identification Marki

12、ng of Aluminum and Magnesium Products 2.3 ANSI Publications: Available from ANSI, 25 West 43rd Street, New York, NY 10036 or 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:

13、3.1 Composition: Shall conform to the percentages by weight shown in Table 1, determined in accordance with AMS 2355. SAE INTERNATIONAL AMS4164H Page 3 of 6 TABLE 1 - Composition 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 - 0.2

14、5 Titanium - 0.15 Other Elements, each - 0.05 Other Elements, total - 0.15 Aluminum remainder 3.2 Condition: Solution heat treated in accordance with AMS 2772 and stress-relieved by stretching to produce a nominal permanent set of 1.5%, but not less than 1% nor more than 3%, to the T3510 temper (see

15、 AS1990). 3.2.1 Extrusions shall receive no straightening after stretching. 3.2.2 Extrusions shall be supplied with an as-extruded surface finish; light polishing to remove minor surface imperfections is permissible provided such imperfections can be removed within specified dimensional tolerances.

16、3.3 Properties: Extrusions shall conform to the following requirements shown in Tables 2 and 3, determined in accordance with AMS 2355 on the mill product. 3.3.1 Tensile Properties: Shall be as shown in Table 2 or Table 3 as applicable. 3.3.1.1 Bars, Rods, Wire and Profiles: TABLE 2A - Minimum Longi

17、tudinal Tensile Properties, Inch/Pound Units Nominal Diameter or Thickness Inches Nominal Cross-Sectional Area Square Inches Tensile Strengthksi Yield Strength at 0.2% Offset ksi Elongation in2 Inches or 4D% Up to 0.249, incl All areas 57.0 42.0 12 Over 0.249 to 0.749, incl All areas 60.0 44.0 12 Ov

18、er 0.749 to 1.499, incl All areas 65.0 46.0 10 Over 1.499 Up to 25, incl 70.0 52.0 10 Over 1.499 Over 25 to 32, incl 68.0 48.0 8 SAE INTERNATIONAL AMS4164H Page 4 of 6 TABLE 2B - Minimum Longitudinal Tensile Properties, SI Units Nominal Diameter or Thickness Millimeters Nominal Cross-Sectional Area

19、Square Centimeters Tensile StrengthMPa Yield Strength at 0.2% Offset MPa Elongation in50.8 mm or 4D% Up to 6.32, incl All areas 393 290 12 Over 6.32 to 19.02, incl All areas 414 303 12 Over 19.02 to 38.07, incl All areas 448 317 10 Over 38.07 Up to 161, incl 483 359 10 Over 38.07 Over 161 to 206, in

20、cl 469 331 8 3.3.1.2 Round Tubing: TABLE 3A - Minimum Tensile Properties, Inch/Pound Units Nominal Wall Thickness Inches Nominal Cross-Sectional Area Square Inches TensileStrengthksi Yield Strength at 0.2% Offset ksi Elongation in2 Inches or 4D% Up to 0.249, incl All areas 57.0 42.0 10 Over 0.249 to

21、 0.749, incl All areas 60.0 44.0 10 Over 0.749 to 1.499, incl All areas 65.0 46.0 10 Over 1.499 Up to 25, incl 70.0 48.0 10 Over 1.499 Over 25 to 32, incl 68.0 46.0 8 TABLE 3B - Minimum Tensile Properties, SI Units Nominal Wall Thickness Millimeters Nominal Cross-Sectional Area Square Centimeters Te

22、nsileStrengthMPa Yield Strength at 0.2% Offset MPa Elongation in 50.8 mm or 4D% Up to 6.32, incl All areas 393 290 10 Over 6.32 to 19.02, incl All areas 414 303 10 Over 19.02 to 38.07, incl All areas 448 317 10 Over 38.07 Up to 161, incl 483 331 10 Over 38.07 Over 161 to 206, incl 469 317 8 3.4 Qual

23、ity: Extrusions, 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 extrusions. 3.4.1 When specified, extrusions shall be subjected to ultrasonic inspection in accordance with ASTM B 594. Bars

24、 and profiles 0.500 inch (12.70 mm) and over in thickness, not exceeding 600 pounds (272 kg) in weight per piece, and not exceeding a width-to-thickness ratio of 10 to 1 shall meet discontinuity Class B. SAE INTERNATIONAL AMS4164H Page 5 of 6 3.5 Tolerances: Shall conform to all applicable requireme

25、nts of ANSI H35.2 or ANSI H35.2M. 4. QUALITY ASSURANCE PROVISIONS: 4.1 Responsibility for Inspection: The vendor of extrusions shall supply all samples for vendors tests and shall be responsible for the performance of all required tests. Purchaser reserves the right to sample and to perform any conf

26、irmatory testing deemed necessary to ensure that the extrusions conform to specified requirements. 4.2 Classification of Tests: Composition (3.1), tensile properties (3.3.1), ultrasonic inspection when specified (3.4.1), and tolerances (3.5) are acceptance tests and, except for composition, shall be

27、 performed on each inspection lot. 4.3 Sampling and Testing: Shall be in accordance with AMS 2355. 4.4 Reports: The vendor of extrusions shall furnish with each shipment a report stating that the extrusions conform to the chemical composition, ultrasonic inspection when required, and tolerances, and

28、 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 number, AMS 4164H, size or section identification number, and quantity. The report shall also identif

29、y the producer, product form, product lot number, and the size of the mill product. 4.5 Resampling and Retesting: Shall be in accordance with AMS 2355. 5. PREPARATION FOR DELIVERY: 5.1 Identification: Shall be in accordance with ASTM B 666/B 666M. 5.2 Packaging: Extrusions shall be prepared for ship

30、ment in accordance with ASTM B 660 and in compliance with applicable rules and regulations pertaining to the handling, packaging, and transportation of the extrusions to ensure carrier acceptance and safe delivery. SAE INTERNATIONAL AMS4164H Page 6 of 6 6. ACKNOWLEDGMENT: A vendor shall mention this

31、 specification number and its revision letter in all quotations and when acknowledging purchase orders. 7. REJECTIONS: Extrusions not conforming to this specification, or to modifications authorized by purchaser, will be subject to rejection. 8. NOTES: 8.1 A change bar (|) located in the left margin

32、 is for the convenience of the user in locating areas where technical revisions, not editorial changes, have been made to the previous issue of a specification. An (R) symbol to the left of the document title indicates a complete revision of the specification, including technical revision. Change ba

33、rs and (R) are not used in original publications, nor in specifications that contain editorial changes only. 8.2 Hardness should be not lower than 100 HB/10/500 or 106 HB/10/1000, determined in accordance with ASTM E 10. Hardness has been used to verify that extrusions are properly processed, but an

34、 out-of-range hardness number is not always indicative of extrusions with out-of-specification tensile properties. Further analysis, including material composition verification, heat treat process parameter review, and/or tensile property measurement on extrusions with out-of-range hardness, may be

35、necessary. 8.3 Terms used in AMS are clarified in ARP1917. 8.4 Dimensions and properties in inch/pound units are primary; dimensions and properties in SI units are shown as the approximate equivalents of the primary units and are presented only for information. 8.5 Purchase documents should specify

36、not less than the following: AMS 4164H Form and size or section identification number of extrusions desired Quantity of extrusions desired Ultrasonic inspection report when specified (See 3.4.1). 8.6 Similar Specifications: AMS QQ-A-200/3, Temper T3510, is listed for information only and shall not be construed as an acceptable alternate unless all requirements of this AMS are met. 8.7 Key Words: Bars, rods, wire, profiles, tubing PREPARED UNDER THE JURISDICTION OF AMS COMMITTEE “D”