SAE AMS 4156K-2003 Aluminum Alloy Extrusions 0 68Mg - 0 40Si (6063-T6) Solution and Precipitation Heat Treated (UNS A96063)《0 68Mg 0 40Si(6063-T6)溶解热处理和沉淀热处理的铝合金挤压制品》.pdf

《SAE AMS 4156K-2003 Aluminum Alloy Extrusions 0 68Mg - 0 40Si (6063-T6) Solution and Precipitation Heat Treated (UNS A96063)《0 68Mg 0 40Si(6063-T6)溶解热处理和沉淀热处理的铝合金挤压制品》.pdf》由会员分享，可在线阅读，更多相关《SAE AMS 4156K-2003 Aluminum Alloy Extrusions 0 68Mg - 0 40Si (6063-T6) Solution and Precipitation Heat Treated (UNS A96063)《0 68Mg 0 40Si(6063-T6)溶解热处理和沉淀热处理的铝合金挤压制品》.pdf（5页珍藏版）》请在麦多课文档分享上搜索。

1、AEROSPACE MATERIAL SPECIFICATION AMS4156 REV. K Issued 1949-11 Revised 2003-07 Reaffirmed 2015-05 Superseding AMS4156J Aluminum Alloy, Extrusions 0.68Mg - 0.40Si (6063-T6) Solution and Precipitation Heat Treated (Composition similar to A96063) RATIONALE AMS4156K has been reaffirmed to comply with th

2、e SAE five-year review policy. _ 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 pa

3、tent infringement arising therefrom, 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 2015 SAE International All rig

4、hts reserved. No part of this 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

5、and Canada) Tel: +1 724-776-4970 (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/AMS4156K 1. SCOPE:1.1 Form: This specification cov

6、ers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing.1.2 Application: These extrusions have been used typically for parts requiring good surface finish and for hollow, partially enclosed, and intricate profiles for which an alloy having good extruding characteristics

7、is required, 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 specified herein. The supplier may work to a subsequent revision of a document unless

8、a specific document issue is specified. When the referenced document has been canceled and no superseding document has been specified, the last published issue of that document shall apply.2.1 SAE Publications: Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001 or www.sae.org.AMS

9、2355 Quality Assurance Sampling and Testing, Aluminum Alloys and Magnesium Alloys, Wrought Products, Except Forging Stock, and Rolled, Forged or Flash Welded RingsAMS 2772 Heat Treatment of Aluminum Alloy Raw MaterialsAS1990 Aluminum Alloy Tempers2.2 ASTM Publications: Available from ASTM, 100 Barr

10、Harbor Drive, West Conshohocken, PA 19428-2959 or www.astm.org.ASTM B 594 Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace ApplicationsASTM B 660 Packaging/Packing of Aluminum and Magnesium ProductsASTM B 666/B 666M Identification Marking of Aluminum and Magnesium Products2.3 A

11、NSI Publications: Available from ANSI, 25 West 43rd Street, New York, NY 10036 or www.ansi.org.ANSI H35.2 Dimensional Tolerances for Aluminum Mill ProductsANSI H35.2M Dimensional Tolerances for Aluminum Mill Products (Metric)3. TECHNICAL REQUIREMENTS: 3.1 Composition: Shall conform to the percentage

12、s by weight shown in Table 1, determined in accordance with AMS 2355.3.2 Condition: Solution and precipitation heat treated to the T6 temper (see AS1990) in accordance with AMS 2772.3.2.1 Extrusions shall be supplied with an as-extruded surface finish; light polishing to remove minor surface imperfe

13、ctions is permissible provided such imperfections can be removed within specified dimensional tolerances.TABLE 1 - CompositionElement min maxSilicon 0.20 0.6Iron - 0.35Copper - 0.10Manganese - 0.10Magnesium 0.45 0.9Chromium - 0.10Zinc - 0.10Titanium - 0.10Other Elements, each - 0.05Other Elements, t

14、otal - 0.15Aluminum remainderSAE INTERNATIONAL AMS4156K Page 2 of 5_ 3.3 Properties: Extrusions shall conform to the following requirements, determined on the mill size in accordance with AMS 2355:3.3.1 Tensile Properties: Shall be as shown in Table 2.3.4 Quality: Extrusions, as received by purchase

15、r, 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 by purchaser, extrusions shall be subjected to ultrasonic inspection in accordance with ASTM B 594. Standards for acceptance shall b

16、e as agreed upon by purchaser and vendor. 3.5 Tolerances: Shall conform to all applicable requirements of ANSI H35.2 or ANSI H35.2M.TABLE 2A - Minimum Tensile Properties, Inch/Pound UnitsNominal Diameteror Least Thickness(rods, bars, wire, profiles) orNominal Wall Thickness(tubing)InchesTensileStren

17、gthksiYield Strengthat 0.2% OffsetksiElongation in2 Inches or 4D% Up to 0.125, excl 30.0 25.0 80.125 to 1.000, incl 30.0 25.0 10TABLE 2B - Minimum Tensile Properties, SI UnitsNominal Diameteror Least Thickness(rods, bars, wire, profiles) orNominal Wall Thickness(tubing)MillimetersTensileStrengthMPaY

18、ield Strengthat 0.2% OffsetMPaElongation in50.8 mm or 4D% Up to 3.18, excl 207 172 83.18 to 25.40, incl 207 172 10SAE INTERNATIONAL AMS4156K Page 3 of 5_ 4. QUALITY ASSURANCE PROVISIONS: 4.1 Responsibility for Inspection: The vendor of extrusions shall supply all samples for vendors tests and shall

19、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: Composition (3.1), tensile properties (3.3.1), ultras

20、onic inspection when specified (3.4.1), and tolerances (3.5) are acceptance tests and, except for composition, shall be performed on each inspection lot.4.3 Sampling and Testing: Shall be in accordance with AMS 2355.4.4 Reports: The vendor of product shall furnish with each shipment a report stating

21、 that the product conforms to the chemical composition, ultrasonic inspection when specified, and tolerances and 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, insp

22、ection lot number(s), AMS 4156K, size, and quantity. This 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

23、 666/B 666M.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 v

24、endor shall mention this specification number and its revision letter in all quotations and when SAE INTERNATIONAL AMS4156K Page 4 of 5_ acknowledging purchase orders.7. REJECTIONS: Extrusions not conforming to this specification, or to modifications authorized by purchaser, will be subject to rejec

25、tion.8. NOTES:8.1 A change bar (|) 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 specification. An (R) symbol to the left of the document title indicates a complete revisi

26、on of the specification, including technical revisions. Change bars and (R) are not used in original publications, nor in specifications that contain editorial changes only.8.2 Hardness should be not lower than 60HB/10/500 or 66HB/10/1000, determined in accordance with ASTM E 10. Hardness has been u

27、sed to verify that product is properly processed, but an out-of-range hardness number is not always indicative of product with out-of-specification tensile properties. Further analysis, including material composition verification, heat treat process parameter review, and/or tensile property measurem

28、ent on product 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 inf

29、ormation.8.5 Purchase documents should specify not less than the following: AMS 4156KForm and size or section identification of extrusions desiredQuantity of extrusions desiredUltrasonic inspection standards when required (See 3.4.1).8.6 Similar Specifications: AMS QQ-A-200/9, 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 UNDER THE JURISDICTION OF AMS COMMITTEE “D”SAE INTERNATIONAL AMS4156K Page 5 of 5_