SAE AMS 4123H-2006 Aluminum Alloy Rolled or Cold Finished Bars and Rods (7075-T651) Solution and Precipitation Heat Treated (UNS A97075)《溶解和沉淀热处理铝合金轧制或冷精制棒材和杆材(7075-T651)》.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 2011 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/AMS4123H AEROSPACE MATERIAL SPECIFICATION AMS 4123 REV. H Issued 1946-11 Revised

5、2006-01 Reaffirmed 2011-11 Superseding AMS 4123G Aluminum Alloy, Rolled or Cold Finished Bars and Rods (7075-T651) Solution and Precipitation Heat Treated (Composition similar to UNS A97075) RATIONALE This document has been reaffirmed to comply with the SAE five-year review policy. 1. SCOPE: 1.1 For

6、m: This specification covers an aluminum alloy in the form of bars and rods. 1.2 Application: These products have been used typically for machined parts subject to excessive warpage during machining due to residual stresses and for parts requiring high strength and whose fabrication does not involve

7、 welding or forming, 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

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

9、ument has been specified, the last published issue of that document shall apply. SAE AMS 4123H Page 2 of 5 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 Alloys

10、, 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 AS 1990 Aluminum Alloy Tempers 2.2 ASTM Publications: Available fr

11、om ASTM, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959 or www.astm.org. ASTM B 660 Packing/Packaging of Aluminum and Magnesium Products ASTM B 666/B666M Identification Marking of Aluminum and Magnesium Products 2.3 ANSI Publications: Available from ANSI, 25 West 43rd Street,

12、 New York, NY 10036 or www.ansi.org. ANSI H35.2/H35.2M Dimensional Tolerances for Aluminum Mill Products 3. TECHNICAL REQUIREMENTS: 3.1 Composition: Shall conform to the percentages by weight shown in Table 1, determined in accordance with AMS 2355. TABLE 1 - Composition Element min max Silicon - 0.

13、40 Iron - 0.50 Copper 1.2 2.0 Manganese - 0.30 Magnesium 2.1 2.9 Chromium 0.18 0.28 Zinc 5.1 6.1 Titanium - 0.20 Other Elements, each - 0.05 Other Elements, total - 0.15 Aluminum remainder SAE AMS 4123H Page 3 of 5 3.2 Condition: Rolled or cold finished, solution heat treated, stress-relieved by str

14、etching to produce a nominal permanent set of 1-1/2% but not less than 1% nor more than 3% and precipitation heat treated. Heat treatments shall be performed in accordance with AMS 2772 (See AS 1990). 3.2.1 Product shall receive no further straightening operations after stretching unless specificall

15、y authorized by purchaser. 3.3 Properties: The product shall conform to the following requirements, determined in accordance with AMS 2355 on the mill produced size and as specified herein. 3.3.1 Tensile Properties: Shall be as shown in Table 2 for rods 0.50 to 4.00 inches (12.7 to 101.6 mm) in diam

16、eter, for square, hexagonal, and octagonal bar 0.50 to 3.50 inches (12.7 to 88.9 mm) in nominal distance between parallel faces, and for rectangular bar 3.00 inches (76.2 mm) in nominal thickness with width up to 6.00 inches (152.4 mm) or for rectangular bar 0.50 to 3.00 inches (12.7 to 76.2 mm) in

17、nominal thickness with width up to 10 inches (254 mm). TABLE 2 - Minimum Tensile Properties Property Value Tensile Strength 77.0 ksi (531 MPa) Yield Strength at 0.2% Offset 66.0 ksi (455 MPa) Elongation in 4D 7% 3.4 Quality: The product, as received by purchaser, shall be uniform in quality and cond

18、ition, 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 ANSI H35.2 or ANSI H35.2M. 4. QUALITY ASSURANCE PROVISIONS: 4.1 Responsibility for Inspection: The vendor of the product shall sup

19、ply 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 confirmatory testing deemed necessary to ensure that the product conforms to specified requirements. 4.2 Classification of Tests: Acceptance

20、 Tests: Composition (3.1), tensile properties (3.3) and tolerances (3.5) are acceptance tests and except for composition, shall be performed on each lot. SAE AMS 4123H Page 4 of 5 4.3 Sampling and Testing: Shall be in accordance with AMS 2355. 4.4 Reports: The vendor of the product shall furnish wit

21、h each shipment a report stating that the product conforms to the composition and tolerances, and showing the numerical results of tests on each inspection lot to determine conformance to the tensile property requirements. This report shall include the purchase order number, inspection lot number, A

22、MS 4123H, 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 AMS 2355. 5. PREPARATION FOR DELIVERY: 5.1 Identification: Shall be in accordance with ASTM B 666/B666M. 5.2 Packag

23、ing: 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. ACKNOWLEDGMENT: A vendor shall mention thi

24、s 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. 8. NOTES: 8.1 A change bar (|) located in the left margin i

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

26、bars and (R) are not used in original publications, nor in specifications that contain editorial changes only. SAE AMS 4123H Page 5 of 5 8.2 Hardness should not be lower than 135 HB/10/500 or 140 HB/10/1000, or equivalent, determined in accordance with ASTM E 10. Hardness has been used to verify tha

27、t product is properly processed, but an “out-of-range hardness number” is not always indicative of product with “out-of-specified tensile strength”. Further analysis, including material composition verification, heat treat process parameter review, and/or tensile property measurement may be necessar

28、y. 8.3 Hardness conversion tables for metals are presented in ASTM E 140. 8.4 Terms used in AMS are clarified in ARP1917. 8.5 Dimensions and properties in inch/pound units and Fahrenheit temperatures are primary; dimensions and properties in SI units and Celsius temperatures are shown as the approxi

29、mate equivalents of the primary units and are presented only for information. 8.6 Purchase documents should specify not less than the following: AMS 4123H Form and size of product desired Quantity of product desired. 8.7 Keywords: Bars and rods, aluminum alloy, rolled or cold finished, 7075-T651, UNS A97075 PREPARED UNDER THE JURISDICTION OF AMS COMMITTEE “D”