SAE AMS 4126C-2005 Aluminum Alloy Die and Hand Forgings and Rolled Rings 5 6Zn - 2 5Mg - 1 6Cu - 0 23Cr (7075-T6) Solution and Precipitation Heat Treated (UNS A97075)《铝合金模件和手工锻件和轧制.pdf
《SAE AMS 4126C-2005 Aluminum Alloy Die and Hand Forgings and Rolled Rings 5 6Zn - 2 5Mg - 1 6Cu - 0 23Cr (7075-T6) Solution and Precipitation Heat Treated (UNS A97075)《铝合金模件和手工锻件和轧制.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4126C-2005 Aluminum Alloy Die and Hand Forgings and Rolled Rings 5 6Zn - 2 5Mg - 1 6Cu - 0 23Cr (7075-T6) Solution and Precipitation Heat Treated (UNS A97075)《铝合金模件和手工锻件和轧制.pdf(9页珍藏版)》请在麦多课文档分享上搜索。
1、 AEROSPACE MATERIAL SPECIFICATION Aluminum Alloy, Die and Hand Forgings and Rolled Rings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T6) Solution and Precipitation Heat Treated (Composition similar to UNS A97075) AMS 4126C Superseding AMS 4126B 1. SCOPE: 1.1 Form: This specification covers an aluminum allo
2、y in the form of die forgings, hand forgings, rolled rings, and stock for forging or rolled rings. 1.2 Application: These products have been used typically for applications requiring high strength in light-to-medium sections, but usage is not limited to such applications. 1.2.1 Certain design and pr
3、ocessing 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 following documents in effect on the date of the purchase order forms a part of this specification to th
4、e 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 document has been specified, the last published issue of that document shall apply. Issued 1973-05
5、 Revised 2005-08 Reaffirmed 2010-10 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
6、 patent 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 reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2010 SAE International All rights reser
7、ved. 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 and Canad
8、a) 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/AMS4126C SAE - 2 - AMS 4126C AMS 4126C 2.1 SAE Publications
9、: Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001 or www.sae.org. AMS 2355 Quality Assurance Sampling and Testing, Aluminum Alloys and Magnesium Alloys, Wrought Products, Except Forging Stock, and Rolled, Forged, or Flash Welded Rings AMS 2772 Heat Treatment of Aluminum Alloy R
10、aw Materials AMS 2808 Identification, Forgings ARP823 Minimizing Stress-Corrosion Cracking in Wrought Heat-Treatable Aluminum Alloy Products AS1990 Aluminum Alloy Tempers 2.2 ASTM Publications: Available from ASTM, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428- 2959 or www.astm.o
11、rg. ASTM B 594 Ultrasonic Inspection of Aluminum Alloy-Wrought Products for Aerospace Applications ASTM B 660 Packaging/Packing of Aluminum and Magnesium Products ASTM E 1417 Liquid Penetrant Examination 2.3 ANSI Publications: Available from American National Standards Institute, Inc., 23 West 43rd
12、Street, New York, NY 10036-8002. ANSI H35.2 Dimensional Tolerances for Aluminum Mill Products ANSI H35.2M Dimensional Tolerances for Aluminum Mill Products (Metric) SAE - 3 - AMS 4126C AMS 4126C 3. TECHNICAL REQUIREMENTS: 3.1 Composition: Shall conform to the percentages by weight shown in Table 1,
13、determined in accordance with AMS 2355. TABLE 1 - Composition Element min max Silicon Iron Copper Manganese Magnesium Chromium Zinc Titanium Other Elements, each Other Elements, total Aluminum - - 1.2 - 2.1 0.18 5.1 - - - remainder 0.40 0.50 2.0 0.30 2.9 0.28 6.1 0.20 0.05 0.15 3.2 Condition: Shall
14、be as follows: 3.2.1 Die Forgings, Hand Forgings, and Rolled Rings: Solution and precipitation heat treated in accordance with AMS 2772 to the -T6 temper (See AS1990). 3.2.2 Stock for Forging or Rolled Rings: As ordered by the forging or rolled ring manufacturer. 3.3 Properties: The product shall co
15、nform to the following requirements, determined on the mill product in accordance with AMS 2355: 3.3.1 Die Forgings, Hand Forgings, and Rolled Rings: 3.3.1.1 Tensile Properties: Shall be as follows: 3.3.1.1.1 Die Forgings: 3.3.1.1.1.1 With Grain Flow: Specimens, machined from forgings 4 inches (102
16、mm) and under in nominal thickness at time of heat treatment or from prolongations on such forgings, with axis of specimen in area of gage length varying not more than 15 degrees from parallel to the forging flow lines, shall have the properties shown in Table 2 provided the as-forged thickness is n
17、ot more than twice the heat treated thickness. SAE - 4 - AMS 4126C AMS 4126C TABLE 2A - Minimum Tensile Properties, Inch/Pound Units Nominal Thickness at Time of Heat Treatment Inches Tensile Strength ksi Yield Strength at 0.2% Offset ksi Elongation in 2 Inches or 4D % Up to 1, incl Over 1 to 3, inc
18、l Over 3 to 4, incl 75.0 74.0 73.0 64.0 63.0 62.0 7 7 7 TABLE 2B - Minimum Tensile Properties, SI Units Nominal Thickness at Time of Heat Treatment Millimeters Tensile Strength MPa Yield Strength at 0.2% Offset MPa Elongation in 50.8 mm or 4D % Up to 25, incl Over 25 to 76, incl Over 76 to 102, incl
19、 517 510 503 441 434 427 7 7 7 3.3.1.1.1.2 Across Grain Flow: Specimens, machined from forgings 4 inches (102 mm) and under in nominal thickness at time of heat treatment or from prolongations on such forgings, with axis of specimen in area of gage length varying not more than 15 degrees from perpen
20、dicular to the forging flow lines, shall have the properties shown in Table 3 provided the as-forged thickness is not more than twice the heat treated thickness. If configuration of the forging or prolongation cannot accommodate the transverse specimen described, acceptance of the forging shall be b
21、ased on testing as in 3.3.1.1.1.3. TABLE 3A - Minimum Tensile Properties, Inch/Pound Units Nominal Thickness at Time of Heat Treatment Inches Tensile Strength ksi Yield Strength at 0.2% Offset ksi Elongation in 2 Inches or 4D % Up to 2, incl Over 2 to 3, incl Over 3 to 4, incl 71.0 70.0 70.0 61.0 60
22、.0 60.0 3 3 2 TABLE 3B - Minimum Tensile Properties, SI Units Nominal Thickness at Time of Heat Treatment Millimeters Tensile Strength MPa Yield Strength at 0.2% Offset MPa Elongation in 50.8 mm or 4D % Up to 51, incl Over 51 to 76, incl Over 76 to 102, incl 490 483 483 421 414 414 3 3 2 3.3.1.1.1.2
23、.1 Elongation requirements shall not apply to specimens having a gage length diameter less than 0.250 inch (6.35 mm) or located in immediate proximity to an abrupt change in thickness or located so that any part of the specimen gage length is located within 1/8 inch (3.2 mm) of the trimmed flash lin
24、e. SAE - 5 - AMS 4126C AMS 4126C 3.3.1.1.1.3 At Angle to Grain Flow: Specimens, machined from forgings 4 inches (102 mm) and under in nominal thickness at time of heat treatment or from prolongations on such forgings, with axis of specimen in area of gage length varying more than 15 degrees from par
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