SAE AMS 4317A-2012 Aluminum Alloy Extruded Bar Rod and Shapes 5 6Zn - 2 5Mg - 1 6Cu - 0 23Cr 7075-T76(51X) Solution Heat Treated and Overaged (UNS R97075)《溶液热处理和老化的铝合金挤制棒材、杆材和型材5 6.pdf

《SAE AMS 4317A-2012 Aluminum Alloy Extruded Bar Rod and Shapes 5 6Zn - 2 5Mg - 1 6Cu - 0 23Cr 7075-T76(51X) Solution Heat Treated and Overaged (UNS R97075)《溶液热处理和老化的铝合金挤制棒材、杆材和型材5 6.pdf》由会员分享，可在线阅读，更多相关《SAE AMS 4317A-2012 Aluminum Alloy Extruded Bar Rod and Shapes 5 6Zn - 2 5Mg - 1 6Cu - 0 23Cr 7075-T76(51X) Solution Heat Treated and Overaged (UNS R97075)《溶液热处理和老化的铝合金挤制棒材、杆材和型材5 6.pdf（6页珍藏版）》请在麦多课文档分享上搜索。

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 2012 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/AMS4317AAEROSPACEMATERIALSPECIFICATIONAMS4317 REV. A Issued 2005-07 Revised 2012-

5、01Superseding AMS4317 Aluminum Alloy, Extruded Bar, Rod, and Shapes 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr 7075-T76(51X) Solution Heat Treated and Overaged (Composition similar to UNS R97075) RATIONALE AMS4317A revises condition (3.2), corrects an error in electrical conductivity (3.3.2.3) and results from

6、a Five Year Review and update of this specification. 1. SCOPE 1.1 Form This specification covers an aluminum alloy in the form of extruded bars, rods, and shapes. 1.2 Application This product has been used typically for structural applications requiring material with high strength and resistance to

7、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 practices to minimize such conditions. 2. APPLICABLE DOCUMENTS The issue of the followin

8、g 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 do

9、cument has been specified, the last published issue of that document shall apply. SAE AMS4317A Page 2 of 6 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.AM

10、S2355 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 Alloy Raw Materials ARP823 Minimizing Stress-Corrosion Cracking in Wrought Heat-Treatable Aluminum

11、 Alloy Products 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-Alloy Wrought Products for Aerospace Application

12、s ASTM B 660 Packaging/Packing of Aluminum and Magnesium Products ASTM B 666/B 666M Identification Marking of Aluminum and Magnesium Products ASTM G 47 Determining Susceptibility to Stress-Corrosion Cracking of High Strength Aluminum Alloy Products 2.3 ANSI Publications Available from American Natio

13、nal Standards Institute, 25 West 43rd Street, New York, NY 10036-8002, 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

14、percentages by weight shown in Table 1, determined in accordance with AMS2355. SAE AMS4317A Page 3 of 6 TABLE 1 - COMPOSITION Element min max Silicon - 0.40 Iron - 0.50 Copper 1.2 2.0 Manganese - 0.30Magnesium 2.1 2.9 Chromium 0.18 0.28 Zinc 5.1 6.1 Titanium - 0.20Other Elements, each - 0.05 Other E

15、lements, total - 0.15 Aluminum remainder 3.2 Condition Solution heat treated, stress-relieved by stretching to produce a nominal permanent set of 1.5%, but not less than 1% nor more than 3%, and precipitation heat treated to the T76511 or T76510 temper (See AS1900). Heat treatments shall be performe

16、d in accordance with AMS2772.3.2.1 The T76511 temper shall be supplied unless T76510 is specified. When T76 is specified, the stress relief by stretching may be omitted and the T76 temper supplied if the stretching is not practical due to the shape of the extrusion. 3.2.2 Extrusions supplied in the

17、T76 or T76511 temper may receive minor straightening, after stretching, of an amount necessary to meet the requirements of 3.5. 3.2.3 Extrusions supplied in the T76510 temper shall receive no straightening after stretching. 3.2.4 Extrusions shall be supplied with an as-extruded surface finish; light

18、 polishing to remove minor surface imperfections is acceptable provided such imperfections can be removed within specified dimensional tolerances. 3.3 Properties Extrusions shall conform to the following requirements, determined in accordance with AMS2355 on the mill produced size (See 8.2): 3.3.1 T

19、ensile Properties 3.3.1.1 Longitudinal Shall be as shown in Table 2 for all tempers. TABLE 2A - MINIMUM LONGITUDINAL TENSILE PROPERTIES, INCH/POUND UNITS (SEE 8.2) Nominal Diameter or Least Thickness Inches Nominal Cross- Sectional Area Square Inches Tensile Strength, ksi Yield Strength at 2% Offset

20、 ksi Elongation in 2 inches or 4D %Up to 0.049, incl All 73.0 63.0 7 Over 0.049 to 0.124, incl All 74.0 64.0 7 Over 0.124 to 0.249, incl Up to 20 74.0 64.0 7 Over 0.249 to 2.000, incl Up to 20 75.0 65.0 7 Over 2.000 to 3.000, incl Up to 20 74.0 64.0 7 Over 3.000 to 4.000, incl Up to 20 74.0 63.0 7 S

21、AE AMS4317A Page 4 of 6 TABLE 2B - MINIMUM LONGITUDINAL TENSILE PROPERTIES, SI UNITS (SEE 8.2) Nominal Diameter or Least Thickness MillimetersNominal Cross- Sectional Area Square Centimeters Tensile Strength MPaYield Strength at 2% Offset MPaElongation in 50.8 mm or 4D %Up to 1.24, incl All 503 434

22、7 Over 1.24 to 3.15, incl All 510 441 7 Over 3.15 to 6.32, incl Up to 129 510 441 7 Over 6.32 to 50.80, incl Up to 129 517 448 7 Over 50.80 to 76.20, incl Up to 129 510 441 7 Over 76.20 to 101.60, incl Up to 129 510 434 7 3.3.2 Electrical Conductivity Conductivity shall be measured on the same speci

23、mens used for mechanical property tests and shall be measured prior to testing for mechanical properties. 3.3.2.1 If the conductivity is 38% IACS (22 MS/m) 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 le

24、ast 36% IACS (20.9 MS/m) but less than 38% IACS (22 MS/m), the material may be tested as specified in 3.3.3 and 3.3.4 and accepted if 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 conductiv

25、ity is lower than 36.0% IACS (20.9 MS/m), the product is not acceptable and may be given an additional precipitation heat treatment, or entirely reheat treated, and retested. 3.3.3 Exfoliation Resistance Product shall not exhibit exfoliation corrosion at the T/10 plane greater than that illustrated

26、by Photo EB, Figure 2 of ASTM G 34. 3.3.4 Stress-Corrosion Test Specimens, cut from material 0.750 inch (19.05 mm) and over in nominal thickness, shall show no evidence of stress-corrosion cracking when tested in accordance with ASTM G 47 and stressed in the short-transverse direction to 25.0 ksi (1

27、72 MPa). 3.4 Quality 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, rod, bar, and shapes shall be ultrasonically inspected in accordance with

28、ASTM B 594 to the acceptance limits specified in Table 3. All extrusions in the inspection lot shall be inspected. TABLE 3 - ULTRASONIC ACCEPTANCE LIMITS Nominal Diameter or Least Thickness Inches (mm) Maximum Weight of Piece pounds (kg) Maximum Thickness to Width Ratio Discontinuity Class 0.500 (12

29、.7) to 1.499 (38.1) incl 600 (272) 10 to 1 B Over 1.499 (38.1) 600 (272) 10 to 1 A SAE AMS4317A Page 5 of 6 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 extrusions shall suppl

30、y 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 extrusions conform to specified requirements. 4.2 Classification of Tests 4.2.1 Accep

31、tance Tests Composition (3.1), longitudinal tensile properties (3.3.1.1), electrical conductivity (3.3.2), quality (3.4), tolerances (3.5) and, when specified, ultrasonic testing (3.4.1) are acceptance tests and, except for composition, shall be performed on each inspection lot. 4.2.2 Periodic Tests

32、 Exfoliation resistance (3.3.3) and stress-corrosion resistance (3.3.4) are periodic tests and shall be performed on at least one sample per month of the applicable tempers for each thickness or diameter range listed in the table of minimum mechanical properties in the detailed specification produce

33、d during the month, and for shapes with width to thickness ratios of up through 6 and over 6 within the thickness ranges produced during the month, 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 produ

34、ct shall furnish with each shipment a report stating that the product conforms to the chemical composition, tolerances, 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

35、that the product conforms to the other specified requirements. This report shall include the purchase order number, inspection lot number, AMS4317A, size, and quantity. The report shall also identify the producer, the mill product form, and the mill produced size. 4.5 Resampling and Retesting Shall

36、be in accordance with AMS2355. 5. PREPARATION FOR DELIVERY 5.1 Identification Shall be in accordance with ASTM B 666/B 666M. 5.2 Protective Treatment Product shall be protected from damage during storage and shipment by a method determined by vendor unless specified by purchaser. An example of typic

37、al protective method includes but is not limited to oiling of the surface. SAE AMS4317A Page 6 of 6 5.3 Packaging 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

38、 of the product to ensure carrier acceptance and safe delivery.6. ACKNOWLEDGMENT A vendor shall mention this specification number in all quotations and when acknowledging purchase orders. 7. REJECTIONS Extrusions not conforming to this specification, or to modifications authorized by purchaser, will

39、 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 previous issue of this document. An (R) symbol to the left of the document title indicates a

40、 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 These mechanical properties have been taken from QQ-A-200/15 and have not been substantiated by AMS statistical proc

41、edures. 8.3 Terms used in AMS are clarified in ARP1917. 8.4 Dimensions and properties 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 on

42、ly for information. 8.5 Purchase documents should specify not less than the following: AMS4317A Form and size or section identification number of extrusions desired Quantity of extrusions desired Ultrasonic testing, when required (See 3.4.1). 8.6 Similar Specifications AMS-QQ-A-200/15, Temper T76(51X), is listed for information only and shall not be construed as an acceptable alternate unless all requirements of this AMS are met. PREPARED BY AMS COMMITTEE “D”