SAE AMS 4146G-2008 Aluminum Alloy Forgings and Rolled or Forged Rings 1 0Mg - 0 60Si - 0 28Cu - 0 20Cr (6061 - T4) Solution Heat Treated and Naturally Aged (UNS A96061)《1 0Mg 0 60S.pdf
《SAE AMS 4146G-2008 Aluminum Alloy Forgings and Rolled or Forged Rings 1 0Mg - 0 60Si - 0 28Cu - 0 20Cr (6061 - T4) Solution Heat Treated and Naturally Aged (UNS A96061)《1 0Mg 0 60S.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4146G-2008 Aluminum Alloy Forgings and Rolled or Forged Rings 1 0Mg - 0 60Si - 0 28Cu - 0 20Cr (6061 - T4) Solution Heat Treated and Naturally Aged (UNS A96061)《1 0Mg 0 60S.pdf(7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 2014 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/AMS4146G AEROSPACE MATERIAL SPECIFICATION AMS4146 REV. G Issued 1960-06 Noncurren
5、t 2005-02 Revised 2008-05 Reaffirmed 2014-05 Superseding AMS4146F Aluminum Alloy Forgings and Rolled or Forged Rings 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061 - T4) Solution Heat Treated and Naturally Aged (Composition similar to UNS A96061) RATIONALE This document has been reaffirmed to comply with th
6、e SAE five-year review policy. 1. SCOPE 1.1 Form This specification covers an aluminum alloy in the form of die forgings, hand forgings, rolled or forged rings, and forging stock. 1.2 Application These products have been used typically for parts which will be welded or brazed to assemblies and then
7、given further heat treatment to develop the full strength of which the alloy is capable, but usage is not limited to such applications. 1.2.1 Corrosion resistance of this alloy is generally superior to that of aluminum alloys containing copper as a principle alloying element. 2. APPLICABLE DOCUMENTS
8、 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 is specified. When the referenced document has been cance
9、lled and no superseding document has been specified, the last published issue of that document shall apply. SAE INTERNATIONAL AMS4146G Page 2 of 7 2.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 72
10、4-776-4970 (outside USA), www.sae.org. AMS2201 Tolerances, Aluminum and Aluminum Alloy Bar, Rod, Wire, and Forging Stock, Rolled or Cold Finished AMS2355 Quality Assurance, Sampling and Testing, Aluminum Alloys and Magnesium Alloy, Wrought Products, Except Forging Stock, and Rolled, Forged, or Flash
11、 Welded Rings AMS2645 Fluorescent Penetrant Inspection AMS2770 Heat Treatment of Wrought Aluminum Alloy Parts AMS2808 Identification, Forgings AMS-H-6088 Heat Treatment of Aluminum Alloys 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken
12、, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM B 594 Ultrasonic Inspection of Aluminum-Alloy Products for Aerospace Applications ASTM B 660 Packing/Packaging of Aluminum and Magnesium Products 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight as shown in Ta
13、ble 1, determined in accordance with AMS2355. TABLE 1 - COMPOSITION Element min max Magnesium Silicon Copper Chromium Iron Zinc Manganese Titanium Other Impurities, each Other Impurities, total 0.8 0.40 0.15 0.04 - - - - - - -1.2 0.8 0.40 0.35 0.7 0.25 0.15 0.15 0.05 0.15 Aluminum Remainder 3.2 Cond
14、ition The product shall be supplied in the following condition: 3.2.1 Die Forgings, Hand Forgings, and Rolled Rings Solution heat treated in accordance with AMS-H-6088 and naturally aged. 3.2.2 Forging Stock As ordered by the forging manufacturer. 3.3 Properties The product shall conform to the foll
15、owing requirements, determined in accordance with AMS2355. SAE INTERNATIONAL AMS4146G Page 3 of 7 3.3.1 Die Forgings, Hand Forgings, and Rolled Rings 3.3.1.1 As Solution Heat Treated and Naturally Aged 3.3.1.1.1 Hardness Shall be 50 - 80 HB/10/500 or 55 - 85 HB/10/1000 but product shall not be rejec
16、ted on the basis of hardness if tensile properties after precipitation heat treatment meet all requirements of 3.3.1.2.1. 3.3.1.2 After Precipitation Heat Treatment Shall be as follows after being precipitation heat treated to T62 temper in accordance with AMS2770: 3.3.1.2.1 Tensile Properties Shall
17、 be as follows: 3.3.1.2.1.1 Test Specimens Specimens machined from separately forged coupons or from stock representing the forgings and, in either case, heat treated with the forgings, shall have the properties in Table 2: TABLE 2 - TENSILE PROPERTIES Property Minimum Tensile Strength Yield Strengt
18、h at 0.2% Offset Elongation in 4D 38.0 ksi (262 MPa) 35.0 ksi (241 MPa) 10% 3.3.1.2.1.2 Die Forgings 3.3.1.2.1.2.1 With Grain Fl ow Specimens, machined from forgings 4 inches (102 mm) and under in nominal thickness with axis of specimen in area of gage length varying not more than 15 degrees from pa
19、rallel to forging flow lines, shall have properties specified in Table 2 except that elongation may be as low as 7%. 3.3.1.2.1.2.2 Across Grain Flow Specimens, machined from forgings 4 inches (102 mm) and under in nominal thickness with axis of specimen area of gage length varying not more than 15 d
20、egrees from perpendicular to forging flow lines, shall have properties specified in Table 2 except that elongation may be as low as 5%. SAE INTERNATIONAL AMS4146G Page 4 of 7 3.3.1.2.1.3 Hand Forgings Specimens, machined from forgings 8 inches (203 mm) and under in nominal thickness shall have prope
21、rties specified in Table 3; tests need not be made in the longitudinal direction unless specifically required by purchaser. TABLE 3A - TENSILE PROPERTIES Nominal Thickness Inches Specimen Orientation Tensile Strengthksi, min Yield Strength at 0.2% Offset ksi, min Elongation in 4D %, min Up to 4, inc
22、l Over 4 to 8, incl Longitudinal Long Trans. Short Trans. Longitudinal Long Trans. Short Trans. 38.0 38.0 37.0 37.0 37.0 35.0 35.0 35.0 33.0 34.0 34.0 32.0 10 8 5 8 6 4 TABLE 3B - TENSILE PROPERTIES (SI) Nominal Thickness Millimeters Specimen Orientation Tensile Strength MPa, min Yield Strength at 0
23、.2% Offset MPa, min Elongation in 5D %, min Up to 102, incl Over 102 to 203, incl Longitudinal Long Trans. Short Trans. Longitudinal Long Trans. Short Trans. 262 262 255 255 255 241 241 241 228 234 234 221 9 7 4 7 5 3 3.3.1.2.1.4 Rolled Rings 3.3.1.2.1.4.1 Tangential Specimens, machined from rings 2
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