SAE AMS 7849E-2015 Tantalum Sheet Strip and Plate Annealed (UNS R05210).pdf
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1、AEROSPACE MATERIAL SPECIFICATION AMS7849 REV. E Issued 1960-06 Reaffirmed 2010-05 Revised 2015-01 Superseding AMS7849D Tantalum Sheet, Strip, and Plate Annealed (Composition similar to UNS R05210) RATIONALE AMS7849E is a Five Year Review and update of this specification. 1. SCOPE 1.1 Form This speci
2、fication covers tantalum in the form of sheet, strip, plate, and foil up through 0.1875 inch (4.75 mm), inclusive. 1.2 Application Primarily for parts requiring exposure to ultra-high temperatures. Applications in oxidizing atmospheres necessitate a protective coating. 2. APPLICABLE DOCUMENTS The is
3、sue 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 cancelled an
4、d 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, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA, www.sae.org. AMS2242
5、Tolerances, Corrosion and Heat-Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Sheet, Strip, and Plate AMS2350 Standards and Test Methods AMS2809 Identification, Titanium and Titanium Alloy Wrought Products _ SAE Technical Standards Board Rules provide that: “This report is published by SA
6、E 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 responsibility of the user.” SAE reviews each technical report at
7、 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 reproduced, stored in a retrieval system or transmitted, in any f
8、orm 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: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: ht
9、tp:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AMS7849E SAE INTERNATIONAL AMS7849E Page 2 of 6 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA
10、 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM E8 / E8M Tension Testing of Metallic Materials ASTM E112 Determining Average Grain Size ASTM E290 Bend Testing for Ductility of Materials ASTM E384 Knoop and Vickers Hardness of Materials 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to th
11、e following percentages by weight shown in Table 1, determined by analytical methods approved by purchaser (See 8.2): 3.1.1 Tantalum Shall be not less than 99.85%. 3.1.2 Other Elements Shall be not more than 0.15% (1500 ppm) total. Individual elements shall not exceed the following limits in parts p
12、er million (ppm): Table 1 - Composition Element Nominal Thickness Up to 0.010 Inch (0.25 mm), excl Nominal Thickness 0.010 Inch (0.25 mm) and Over Columbium 1000 1000 Tungsten 300 300 Oxygen 150 100 Iron 100 100 Zirconium 100 100 Molybdenum 100 100 Carbon 75 50 Nitrogen 75 50 Titanium 50 50 Silicon
13、50 50 Nickel 50 50 Cobalt 20 20 Hydrogen 10 10 3.2 Condition Cold rolled and annealed (See 8.3). SAE INTERNATIONAL AMS7849E Page 3 of 6 3.3 Annealing The product shall be annealed under vacuum (less than 0.1 micron (1 m) mercury) to produce a recrystallized microstructure, meeting the requirements o
14、f Table 2. Table 2 Nominal Thickness Inch Nominal Thickness Millimeters Percent Recrystallization Up to 0.060, excl Up to 1.52, excl 95 0.060 to 0.1875, excl 1.52 to 4.76, excl 90 0.1875 and over 4.76 and over 85 3.4 Properties The product shall conform to the following requirements (See 8.2 and 8.3
15、): 3.4.1 Tensile Properties Shall be as specified in Table 3, determined in accordance with ASTM E8 / E8M with the rate of strain set at 0.005 inch/inch/minute (0.005 mm/mm/minute) and maintained within a tolerance of 0.002 inch/inch/minute (0.002 mm/mm/minute) through the 0.2% offset yield strain a
16、nd 0.05 inch/inch/minute (0.05 mm/mm/minute) and maintained within a tolerance of 0.02 inch/inch/minute (0.02 mm/mm/minute) above the yield strain to fracture: Table 3A Inch/pound units Nominal Thickness Inch Tensile Strength ksi, min Yield Strength at 0.2% Offset ksi, min Elongation in 2 Inches or
17、4D %, min Up to 0.005, incl 30 20 15 Over 0.005 to 0.016, incl 30 20 20 Over 0.016 to 0.1875, incl 30 20 25 Table 3B SI units Nominal Thickness Millimeters Tensile Strength MPa, min Yield Strength at 0.2% Offset MPa, minimum Elongation in 50.8 mm or 4D %, minimum Up to 0.13, incl 207 138 15 Over 0.1
18、3 to 0.41, incl 207 138 20 Over 0.41 to 4.76, incl 207 138 25 3.4.1.1 Tensile properties of product over 0.1875 inch (4.76 mm) in nominal thickness shall be as agreed upon by purchaser and producer. 3.4.2 Hardness Should be not higher than 150 HV30, or equivalent, determined in accordance with ASTM
19、E384, but the product shall not be rejected on the basis of hardness if the tensile property requirements are met. 3.4.3 Bending The product 0.1875 inches (4.76 mm) and under shall withstand, without evidence of cracking when examined at 20X magnification, bending in accordance with ASTM E290 at roo
20、m temperature through an angle of 180 degrees around a diameter equal to the nominal thickness of the product with axis of bend parallel to the direction of rolling. In case of dispute, results of bend tests using the end supported guided bend test shall govern. SAE INTERNATIONAL AMS7849E Page 4 of
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