SAE-AMS-4133D-2000-R2006.pdf
《SAE-AMS-4133D-2000-R2006.pdf》由会员分享,可在线阅读,更多相关《SAE-AMS-4133D-2000-R2006.pdf(11页珍藏版)》请在三一文库上搜索。
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 therefr
2、om, 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. All rights reserved.Printed in U.S.A. QUESTIONS REGARDING THIS DOCUMENT:(724) 772-716
3、1FAX: (724) 776-0243 TO PLACE A DOCUMENT ORDER:(724) 776-4970FAX: (724) 776-0790 SAE WEB ADDRESS:http:/www.sae.org 400 Commonwealth Drive, Warrendale, PA 15096-0001 AEROSPACE MATERIAL SPECIFICATION AMS 4133D IssuedMAY 1972 RevisedSEP 2000 Superseding AMS 4133C Aluminum Alloy Forgings and Rolled Ring
4、s 4.4Cu - 0.85Si - 0.80Mn - 0.50Mg (2014-T6) Solution and Precipitation Heat Treated UNS A92014 1.SCOPE: 1.1Form: This specification covers an aluminum alloy in the form of die forgings, hand forgings, rolled rings, and forging stock. 1.2Application: These products have been used typically for aircr
5、aft structural members requiring moderately high strength. Certain design and processing procedures may cause these forgings and rolled rings to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions. 2.APPLICABLE DOCUMENTS: The issue of the followin
6、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 canceled and no superseding doc
7、ument has been specified, the last published issue of that document shall apply. 2.1SAE Publications: Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001. AMS 2355Quality Assurance Sampling and Testing, Aluminum Alloys and Magnesium Alloys, Wrought Products, Except Forging Stock, a
8、nd Rolled, Forged, or Flash Welded Rings MAM 2355 Quality Assurance Sampling and Testing, Aluminum Alloys and Magnesium Alloys, Wrought Products, Except Forging Stock, and Rolled, Forged, or Flash Welded Rings, Metric (SI) Units AMS 2772Heat Treatment of Aluminum Alloy Raw Materials AMS 2808Identifi
9、cation, Forgings Copyright 2006 SAE International Reaffirmed APR 2006 AMS 4133DSAEAMS 4133D - 2 - 2.1 (Continued): ARP823Minimizing Stress-Corrosion Cracking in Wrought Heat-Treatable Aluminum Alloy Products 2.2ASTM Publications: Available from ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 1942
10、8-2959. ASTM B 594Ultrasonic Inspection of Aluminum-Alloy Products for Aerospace Applications ASTM B 660Packaging/Packing of Aluminum and Magnesium Products ASTM E 1417 Liquid Penetrant Examination 2.3ANSI Publications: Available from ANSI, 11 West 42nd Street, New York, NY 10036-8002. ANSI H35.2Dim
11、ensional Tolerances for Aluminum Mill Products ANSI H35.2M Dimensional Tolerances for Aluminum Mill Products (Metric) 3.TECHNICAL REQUIREMENTS: 3.1Composition: Shall conform to the percentages by weight shown in Table 1, determined in accordance with AMS 2355 or MAM 2355. TABLE 1 - Composition Eleme
12、ntminmax Silicon0.501.2 Iron-0.7 Copper3.95.0 Manganese0.401.2 Magnesium0.200.8 Chromium-0.10 Zinc-0.25 Titanium-0.15 Other Elements, each-0.05 Other Elements, total-0.15 Aluminumremainder -,-,- AMS 4133DSAEAMS 4133D - 3 - 3.2Condition: The product shall be supplied in the following condition: 3.2.1
13、Die Forgings, Hand Forgings, and Rolled Rings: Solution and precipitation heat treated in accordance with AMS 2772. 3.2.2Forging Stock: As ordered by the forging manufacturer. 3.3Properties: The product shall conform to the following requirements, determined in accordance with AMS 2355 or MAM 2355 o
14、n the mill produced size. 3.3.1Die Forgings, Hand Forgings, and Rolled Rings: 3.3.1.1Tensile Properties: Shall be as follows: 3.3.1.1.1Die Forgings: 3.3.1.1.1.1With Grain Flow: Specimens, machined from heat treated forgings 4 inches (102 mm) and under in nominal thickness at time of heat treatment o
15、r from prolongations on such forgings, with axis of specimen in the 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 not more than twice the heat treated thickness. TABLE 2A -
16、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 4D % Up to 2, incl65.056.06 Over 2 to 3, incl65.055.06 Over 3 to 4, incl63.055.06 TABLE 2B - Minimum Tensile Properties, SI Units Nomin
17、al Thickness at Time of Heat Treatment Millimeters Tensile Strength MPa Yield Strength at 0.2% Offset MPa Elongation in 4D % Up to 51, incl4483866 Over 51 to 76, incl4483796 Over 76 to 102, incl4343796 AMS 4133DSAEAMS 4133D - 4 - 3.3.1.1.1.2Across Grain Flow: Specimens, machined from heat treated fo
18、rgings 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 the area of gage length varying not more than 15 degrees from perpendicular to the forging flow lines, shall have the properties shown in Table 3 provide
19、d 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 based on testing as in 3.3.1.1.1.3. 3.3.1.1.1.2.1Elongation requirements shall not app
20、ly to specimens having a gage length diameter less than 0.250 inch (6.35 mm) or to specimens machined from locations in immediate proximity to an abrupt change in thickness or from locations such that any part of the specimen gage length is located within 1/8 inch (3.2 mm) of the trimmed flash line.
21、 3.3.1.1.1.3At 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 the axis of specimen in the area of gage length varying more than 15 degrees from parallel and also more than
22、 15 degrees from perpendicular 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. Such test results shall be identified as neither longitudinal nor transverse tensile properties. 3.3.1.1.2Hand Forg
23、ings: Specimens, machined from forgings 8 inches (203 mm) and under in nominal thickness at time of heat treatment and having an essentially square or rectangular cross- section, shall have the properties shown in Table 4 provided the as-forged thickness does not exceed 8 inches (203 mm). TABLE 3A -
24、 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 4D % Up to 1, incl64.055.03 Over 1 to 2, incl64.055.02 Over 2 to 4, incl63.054.02 TABLE 3B - Minimum Tensile Properties, SI Units Nomi
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- SAE AMS 4133 2000 R2006
链接地址:https://www.31doc.com/p-3792939.html