SAE AMS 7847D-2015 Tantalum Alloy Sheet Strip and Plate 90Ta - 10W (UNS R05255).pdf
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1、AEROSPACE MATERIAL SPECIFICATION AMS7847 REV. D Issued 1965-09 Reaffirmed 2010-05 Revised 2015-01 Superseding AMS7847C Tantalum Alloy Sheet, Strip, and Plate 90Ta - 10W (Composition similar to UNS R05255) RATIONALE AMS7847D is a Five Year Review and update of this specification. 1. SCOPE 1.1 Form Th
2、is specification covers a tantalum alloy in the form of sheet, strip, and plate from 0.010 through 0.250 inch (0.25 through 6.35 mm), inclusive. 1.2 Application Primarily for parts requiring exposure to ultra-high temperatures. Applications in oxidizing atmospheres necessitate a protective coating.
3、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 a specific document issue is specified. When the referenced
4、document has been cancelled and 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 (outs
5、ide USA, www.sae.org. AMS2242 Tolerances, Corrosion and Heat-Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Sheet, Strip, and Plate AMS2809 Identification, Titanium and Titanium Alloy Wrought Products _ SAE Technical Standards Board Rules provide that: “This report is published by SAE to
6、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 leas
7、t 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 form o
8、r 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: http:/w
9、ww.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AMS7847D SAE INTERNATIONAL AMS7847D Page 2 of 5 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 1942
10、8-2959, Tel: 610-832-9585, www.astm.org. ASTM E8 / E8M Tension Testing of Metallic Materials ASTM E290 Bend Testing Materials for Ductility ASTM E384 Knoop and Vickers Hardness of Materials 3. TECHNICAL REOUIREMENTS 3.1 Composition Shall conform to the following percentages by weight shown in Table
11、1; carbon shall be determined conductometrically, oxygen by the inert gas or vacuum fusion method, nitrogen by the Kjeldahl method or by vacuum fusion, hydrogen by the vacuum fusion or vacuum extraction method, and metallic elements by spectrochemical methods or by other analytical methods acceptabl
12、e to purchaser. Table 1 - Composition Element min max Tungsten 8.50 11.00 Columbium - 0.10 Molybdenum - 0.030 Nickel - 0.010 Iron - 0.010 Carbon - 0.010 Oxygen - 0.010 (100 ppm) Nitrogen - 0.005 ( 50 ppm) Hydrogen - 0.001 ( 10 ppm) Tantalum remainder 3.2 Condition Cold rolled and fully annealed, hav
13、ing a surface appearance comparable to a commercial corrosion-resistant steel No. 2D finish (See 8.2). 3.3 Properties The product shall conform to the following requirements: 3.3.1 Tensile Properties Shall be as follows for product 0.010 to 0.250 inch (0.25 to 6.35 mm), incl, in nominal thickness, d
14、etermined 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 and 0.05 inch/inch/minute (0.05 mm/mm/minute) and maintained wit
15、hin a tolerance of 0.02 inch/inch/minute (0.02 mm/mm/minute) above the yield strain to fracture: Table 2 Tensile properties Property Value Tensile Strength, minimum 70 ksi (483 MPa) Yield Strength at 0.2% Offset, minimum 60 ksi (414 MPa) Elongation in 1 Inch (25.4 mm), minimum 15% SAE INTERNATIONAL
16、AMS7847D Page 3 of 5 3.3.1.1 Tensile property requirements for product under 0.010 inch (0.25 mm) or over 0.250 inch (6.35 mm) in nominal thickness shall be as agreed upon by purchaser and producer. 3.3.2 Hardness Not higher than 260 HV10, or equivalent, determined in accordance with ASTM E384. 3.3.
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