SAE AMS 4315A-2017 Aluminum Alloy Sheet and Plate 5 6Zn - 2 5Mg - 1 6Cu - 0 23Cr 7075 (-T76 Sheet -T7651 Plate) Solution and Precipitation Heat Treated (UNS R97075).pdf

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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 ther

2、efrom, 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

3、publication 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: +1 724-776-49

4、70 (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/AMS4315A AEROSPACE MATERIAL SPECIFICATION AMS4315 REV. A Issued 2005-07 Reaffirmed 2011-08 Rev

5、ised 2017-06 Superseding AMS4315 Aluminum Alloy Sheet and Plate 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr 7075: (-T76 Sheet, -T7651 Plate) Solution and Precipitation Heat Treated (Composition Similar to UNS R97075) RATIONALE AMS4315A revises Condition (3.2), Properties (3.3.1.1), Quality (3.4.1) Reports (4.4),

6、 and Identification (5.1.1), and is a Five-Year Review and update of this specification. 1. SCOPE 1.1 Form This specification covers an aluminum alloy in the form of sheet and plate up to 2.000 inch (54.80 mm) inclusive, in thickness (see 8.5). 1.2 Application This product has been used typically fo

7、r structural applications requiring material with high strength and resistance to exfoliation-corrosion, 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 practi

8、ces 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 document unless a specific document issue i

9、s specified. When the referenced document has been cancelled and no superseding document has been specified, the last published issue of that document shall apply. SAE INTERNATIONAL AMS4315A Page 2 of 6 2.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 150

10、96-0001, 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 Aluminum

11、Alloy Raw Materials ARP823 Minimizing Stress-Corrosion Cracking in Wrought Heat-Treatable Aluminum Alloy Products ARP1917 Clarification of Terms Used in Aerospace Metals Specifications 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, P

12、A 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM B594 Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications ASTM B660 Packaging/Packing of Aluminum and Magnesium Products ASTM B666/B666M Identification Marking of Aluminum Products ASTM G34 Exfoliation Corrosion Susce

13、ptibility in 2XXX and 7XXX Series Aluminum Alloys (EXCO Test) ASTM G47 Determining Susceptibility to Stress-Corrosion Cracking of High Strength Aluminum Alloy Products 2.3 ANSI Accredited Publications Copies of these documents are available online at http:/webstore.ansi.org/. ANSI H35.1/H35.1M Stand

14、ard Alloy and Temper Designation System For Aluminum ANSI H35.2 Dimensional Tolerances for Aluminum Mill Products ANSI H35.2M Dimensional Tolerances for Aluminum Mill Products (Metric) 2.4 U.S. Government Publications Copies of these documents are available online at http:/quicksearch.dla.mil. QQ-A-

15、250/24 Aluminum Alloy, 7075, Plate And Sheet (Improved Exfoliation Resistant) SAE INTERNATIONAL AMS4315A Page 3 of 6 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Table 1, determined in accordance with AMS2355. Table 1 - Composition Element Min Max Sil

16、icon - 0.40 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 3.2 Condition The product shall be supplied in the following condition; heat treatments shall be perfo

17、rmed in accordance with AMS2772. 3.2.1 Sheet Solution and precipitation heat treated to the T76 temper (see ANSI H35.1/H35.1M). 3.2.2 Plate Solution heat treated, stress-relieved by stretching to produce a nominal permanent set of 2%, but not less than 1-1/2%, nor more than 3%, and precipitation hea

18、t treated to the T7651 temper (see ANSI H35.1/H35.1M). 3.2.2.1 Plate shall receive no straightening operations after stretching. 3.3 Properties 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 s

19、pecified in Table 2. Table 2 Table 2A - Minimum tensile properties, inch/pound units (see 8.2) Temper Thickness Inches Tensile Strength ksi Yield Strength at 0.2% Offset ksi Elongation in 2 Inches or 4D % T76 0.063 to 0.249, incl 73.0 62.0 8 Over 0.249 to 0.499, incl 72.0 61.0 8 T7651 Over 0.499 to

20、1.000, incl 71.0 60.0 6 Over 1.000 to 2.000, incl 71.0 60.0 5 SAE INTERNATIONAL AMS4315A Page 4 of 6 Table - 2B Minimum tensile strength properties, SI units (see 8.2) Temper Thickness Millimeters Tensile Strength MPa Yield Strength at 0.2% Offset MPa Elongation in 2 Inches or 4D % T76 1.60 to 6.32,

21、 incl 503 428 8 Over 6.32 to 12.67, incl 497 421 8 T7651 Over 12.67 to 25.40, incl 490 414 6 Over 25.40 to 50.80, incl 490 414 5 3.3.1.1 Mechanical property requirements for product outside of the range covered by Table 2 shall be agreed upon between purchaser and producer. 3.3.2 Electrical Conducti

22、vity 3.3.2.1 If the conductivity is 38% IACS or higher, and the tensile properties meet the minimum limits specified herein, the material is acceptable. 3.3.2.2 If the conductivity is at least 36% IACS but less than 38% IACS, the material may be tested as specified in 3.3.3 and 3.3.4 and accepted if

23、 it passes these tests. As alternatives, the product may be given an additional precipitation heat treatment, or reheat treated, and retested. 3.3.2.3 If the conductivity is lower than 36.0% IACS (22.0 MS/m), the product is not acceptable and may be given an additional precipitation heat treatment,

24、or entirely reheat treated, and retested. 3.3.3 Exfoliation Resistance Plate shall not exhibit exfoliation corrosion at the T/10 plane greater than that illustrated by Photo B, Figure 2 of ASTM G34. 3.3.4 Stress-Corrosion Test Specimens, cut from plate 0.750 inch (19.05 mm) and over in nominal thick

25、ness, shall show no evidence of stress-corrosion cracking when tested in accordance with ASTM G47 and stressed in the short-transverse direction to 25.0 ksi (172 MPa). 3.4 Quality Product, as received by purchaser, shall be uniform in quality and condition, sound, and free from foreign materials and

26、 from imperfections detrimental to usage of the material. 3.4.1 When specified, each plate, 0.500 inch (12.70 mm) to 2.000 inch (50.8 mm) in nominal thickness, shall be ultrasonically inspected in accordance with ASTM B594 and shall meet ultrasonic Class A. 3.5 Tolerances Shall conform to all applic

27、able requirements of ANSI H35.2 or ANSI H35.2M. SAE INTERNATIONAL AMS4315A Page 5 of 6 4. QUALITY ASSURANCE PROVISIONS 4.1 Responsibility for Inspection The vendor shall supply all samples for vendors tests and shall be responsible for the performance of all required tests. Purchaser reserves the ri

28、ght 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 properties (3.3.1), electrical conductivity (3.3.2), quality (3.4), and tolerances (3.5)

29、 are acceptance tests and, except for composition, shall be performed on each lot. 4.2.2 Periodic Tests Exfoliation resistance (3.3.3) and stress-corrosion resistance (3.3.4) are periodic tests and shall be performed at a frequency of at least one sample per month for each size range of sheet and pl

30、ate produced during that month unless frequency of testing is specified by purchaser. 4.3 Sampling and Testing Shall be in accordance with AMS2355 and the following: 4.3.1 Specimens for conductivity testing shall be the tensile specimens. 4.3.2 One or more samples shall be taken from each inspection

31、 lot for exfoliation-resistance testing and for stress-corrosion resistance testing, when the conductivity is between 36.0% and 38.0% IACS (see 3.3.2.2). 4.4 Reports The vendor of the product shall furnish with each shipment a report stating that the product conforms to the composition, tolerances,

32、and ultrasonic testing when specified showing the numerical results of tests on each inspection lot to determine conformance to the other acceptance test requirements and stating that the product conforms to the other specified requirements. This report shall include the purchase order number, inspe

33、ction lot number(s), AMS4315A, size, and quantity. The report shall also identify the producer, the mill product form, and the mill produced size. 4.4.1 When the product size is outside the range covered by Table 2, the report shall contain a statement to that effect. 4.4.2 When material produced to

34、 this specification is beyond the sizes allowed in the scope or tables, or other exceptions are taken to the technical requirements listed in Section 3, (see 5.1.1), the report shall contain a statement “This material is certified as AMS4315A(EXC) because of the following exceptions.” and the specif

35、ic exceptions shall be listed. 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. SAE INTERNATIONAL AMS4315A Page 6 of 6 5.1.1 When technical exceptions are taken (see 4.4.2), the material shal

36、l be marked with AMS4315A(EXC). 5.2 Protective Treatment Product shall be protected from damage during storage and shipment by a method determined by vendor unless specified by purchaser. Examples of typical protective methods include but are not limited to interleaving with paper or oiling of the s

37、urface. 5.3 Packaging The product shall be prepared for shipment in accordance with ASTM B660 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 sh

38、all mention this specification number in all quotations and when acknowledging purchase orders. 7. REJECTIONS Plate 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 (I) located in the left ma

39、rgin 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 revision of the document, including technical revisions. Change bars

40、 and (R) are not used in original publications, nor in documents that contain editorial changes only. 8.2 These mechanical properties have been taken from QQ-A-250/24 and have not been substantiated by AMS statistical procedures. 8.3 Terms used in AMS are clarified in ARP1917. 8.4 Dimensions and pro

41、perties in inch/pound units and the Fahrenheit temperatures are primary; dimensions and properties in SI units and the 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: AMS4315A Ultrasonic Testing when desired (see 3.4.1) Size of product desired Property and acceptance requirements from the cognizant engineering organization applicable to sizes outside the range listed in 1.1 Quantity of product desired. PREPARED BY AMS COMMITTEE “D”