1、AEROSPACE MATERIAL SPECIFICATION AMS4154 REV. R Issued 1945-10 Reaffirmed 2008-05 Revised 2015-01 Superseding AMS4154P Aluminum Alloy, Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T6, 7075-T6510, 7075-T6511) Solution Heat Treated, Stress Relieved by Stretching when Required and Precipitation Heat
2、 Treated (Composition similar to UNS A97075) RATIONALE AMS4154R revises tensile properties (Table 2, 3.3.2.2) and introduces General Agreement wording related to properties outside the applicable size range (3.3.1, 4.4.1). 1. SCOPE 1.1 Form This specification covers an aluminum alloy in the form of
3、extruded bars, rods, wire, profiles, and tubing. 1.1.1 This specification covers products up to 5.000 inches (127.00 mm) in nominal diameter or thickness, or wall thickness (See 8.5). 1.2 Application These extrusions have been used typically for parts requiring high strength and whose fabrication do
4、es not usually involve welding or forming, but usage is not limited to such applications. 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 supplied herein. The supplier may work to a subsequent r
5、evision of a document unless a specific document issue is specified. When the referenced document has been cancelled and no superseding document has been specified, the last published issue of that document shall apply. 2.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, W
6、arrendale, 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, Aluminum Alloys and Magnesium Alloy, Wrought Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings _ SAE Technical Sta
7、ndards 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 therefrom, is the sole r
8、esponsibility 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 2015 SAE International All rights reserved. No part of this publication may be r
9、eproduced, 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 USA) Fax
10、: 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/AMS4154R SAE INTERNATIONAL AMS4154R Page 2 of 6 AMS2772 Heat Treatment of Aluminum Alloy Raw Materia
11、ls 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 ASTM B 660 Packaging/Packing of Alumi
12、num and Magnesium Products ASTM B 666/B 666M Identification Marking of Aluminum and Magnesium Products 2.3 ANSI Publications Available from American National 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 Alu
13、minum Mill Products ANSI H 35.2M Dimensional Tolerances for Aluminum Mill Products (Metric) 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 Silicon - 0.40 Iron - 0.50 C
14、opper 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 Aluminium remainder 3.2 Condition Solution heat treated, stress-relieved by stretching to produce a nominal permanent set of 1.5%, but not less th
15、an 1% nor more than 3%, and precipitation heat treated to the T6511 or T6510 temper (See AS1900). Heat treatments shall be performed in accordance with AMS2772. 3.2.1 The T6511 temper shall be supplied unless T6510 is specified. When T6 is specified, the stress relief by stretching may be omitted an
16、d the T6 temper supplied if the stretching is not practical due to the shape of the extrusion. SAE INTERNATIONAL AMS4154R Page 3 of 6 3.2.2 Extrusions supplied in the T6 or T6511 temper may receive minor straightening, after stretching, of an amount necessary to meet the requirements of 3.5. 3.2.3 E
17、xtrusions supplied in the T6510 temper shall receive no straightening after stretching. 3.2.4 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
18、tolerances. 3.3 Properties Extrusions shall conform to the following requirements, determined in accordance with AMS2355 on the mill product. 3.3.1 Mechanical properties requirements for product outside of the range covered by Tables 2 and 3 shall be agreed upon between purchaser and producer. 3.3.2
19、 Tensile Properties Shall be as shown in 3.3.2.1 (Table 2) and 3.3.2.2 (Table 3). 3.3.2.1 Longitudinal TABLE 2A - Minimum Longitudinal Tensile Properties, Inch/Pound Units Nominal Dimensions Diameter or Thickness (rods, bars, wire, profiles) or Nominal Wall Thickness (tubing) Inches Nominal Dimensio
20、ns Cross-Sectional Area Square Inches Tensile Strength ksi Yield Strength at 0.2% Offset ksi Elongation in 2 inches or 4D % Up to 0.249, incl All areas 78.0 70.0 7 Over 0.249 to 0.499, incl All areas 81.0 73.0 7 Over 0.499 to 2.999, incl All areas 81.0 72.0 7 Over 2.999 to 4.499, incl Up to 20, incl
21、 81.0 71.0 7 Over 2.999 to 4.499, incl Over 20 to 32, incl 78.0 70.0 6 Over 4.499 to 5.000, incl Up to 32, incl 78.0 68.0 6 TABLE 2B - Minimum Longitudinal Tensile Properties, SI Units Nominal Dimensions Diameter or Thickness (rods, bars, wire, profiles) or Nominal Wall Thickness (tubing) Millimeter
22、s Nominal Dimensions Cross-Sectional Area Square Centimeters Tensile Strength MPa Yield Strength at 0.2% Offset MPa Elongation in 50.8 mm or 4D % Up to 6.32, incl All areas 538 483 7 Over 6.32 to 12.67, incl All areas 558 503 7 Over 12.67 to 76.17, incl All areas 558 496 7 Over 76.17 to 114.27, incl
23、 Up to 129, incl 558 490 7 Over 76.17 to 114.27, incl Over 129 to 206, incl 538 483 6 Over 114.27 to 127.00, incl Up to 206, incl 538 469 6 3.3.2.2 Long-Transverse; Rods, Bars, and Profiles Long-transverse tensile requirements apply only to extrusions from which a test specimen not less than 2.50 in
24、ches (63.5 mm) in length can be taken. SAE INTERNATIONAL AMS4154R Page 4 of 6 Table 3A - Minimum Long Transverse Tensile Properties, Inch/Pound Units Nominal Dimensions Diameter or Thickness Inches Nominal Dimensions Cross-Sectional Area Square Inches Tensile Strength ksi Yield Strength at 0.2% Offs
25、et ksi Elongation in 2 inches or 4D % Up to 0.249, incl Up to 20, incl 76.0 66.0 5 Over 0.249 to 0.499, incl Up to 20, incl 78.0 68.0 5 Over 0.499 to 0.749, incl Up to 20, incl 76.0 66.0 4 Over 0.749 to 1.499, incl Up to 20, incl 74.0 65.0 3 Over 1.499 to 2.999, incl Up to 20, incl 70.0 61.0 1 Over
26、2.999 to 4.499, incl Up to 20, incl 67.0 56.0 1 Over 2.999 to 4.499, incl Over 20 to 32, incl 65.0 55.0 1 Table 3B - Minimum Long Transverse Tensile Properties, SI Units Nominal Dimensions Diameter or Thickness Millimeters Nominal Dimensions Cross-Sectional Area Square Centimeters Tensile Strength M
27、Pa Yield Strength at 0.2% Offset MPa Elongation in 50.8 mm or 4D % Up to 6.32, incl Up to 129, incl 524 455 5 Over 6.32 to 12.67, incl Up to 129, incl 538 469 5 Over 12.67 to 19.02, incl Up to 129, incl 524 455 4 Over 19.02 to 38.07, incl Up to 129, incl 510 448 3 Over 38.07 to 76.17, incl Up to 129
28、, incl 483 421 1 Over 76.17 to 114.27, incl Up to 129, incl 462 386 1 Over 76.17 to 114.27, incl Over 129 to 206, incl 448 379 1 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 u
29、sage of the extrusions. 3.4.1 When specified, extrusions shall be subjected to ultrasonic inspection in accordance with ASTM B 594. Extrusions 0.500 to 1.499 inches (12.70 to 38.07 mm), inclusive, in nominal thickness, not exceeding 600 pounds (272 kg) per piece, or a 10 to 1 width-to-thickness rati
30、o shall meet ultrasonic class B. Extrusions 1.500 inches (38.10 mm) and over in nominal thickness, not exceeding 600 pounds (272 kg) per piece, or a 10 to 1 width-to-thickness ratio shall meet ultrasonic class A. 3.5 Tolerances Shall conform to all applicable requirements of ANSI H35.2 or ANSI H35.2
31、M. 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 confirmatory testing deemed necessary
32、 to ensure that the extrusions conform to specified requirements. SAE INTERNATIONAL AMS4154R Page 5 of 6 4.2 Classification of Tests 4.2.1 Acceptance Tests Composition (3.1), longitudinal tensile properties (3.3.2.1), ultrasonic inspection when specified (3.4.1), and tolerances (3.5) are acceptance
33、tests and, except for composition, shall be performed on each inspection lot. 4.2.2 Periodic Tests Long-transverse tensile properties (3.3.2.2) are periodic tests and shall be performed at a frequency selected by the vendor unless frequency of testing is specified by purchaser. 4.3 Sampling and Test
34、ing Shall be in accordance with AMS2355. 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 specified, and tolerances and showing the numerical results of tests on each inspection
35、lot to determine conformance to the other acceptance test requirements. This report shall include the purchase order number, inspection lot number, AMS4154R, size or section identification number, and quantity. The report shall also identify the producer, product form, producer lot number, and the s
36、ize of the mill product. 4.4.1 When the product size is outside the range covered by 1.1.1, the report shall contain a statement to that effect. 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 6
37、66M. 5.2 Packaging Extrusions 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 extrusions to ensure carrier acceptance and safe delivery. 6. ACKNOWLEDGMENT A vendor sh
38、all mention this 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 t
39、he 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 complete revision of the document, including technical revisions. C
40、hange bars and (R) are not used in original publications, nor in documents that contain editorial changes only. SAE INTERNATIONAL AMS4154R Page 6 of 6 8.2 Hardness should be not lower than 135HB/10/500 or 140HB/10/1000, determined in accordance with ASTM E 10. Hardness has been used to verify that e
41、xtrusions have been properly processed, but an 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
42、extrusions with out-of-range hardness, may be 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 infor
43、mation. 8.5 Purchase documents should specify not less than the following: AMS4154R Form and size or section identification of extrusions desired Quantity of extrusions desired Property and acceptance requirements from the cognizant engineering organization applicable to sizes outside the range listed in 1.1.1. Ultrasonic inspection report when specified (See 3.4.1). 8.6 Similar Specifications AMS-QQ-A-200/11, Temper T6, 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”
