SAE AMS 7852C-2013 Columbium (Niobium) Alloy Sheet Strip and Plate 10Hf - 1 0Ti (UNS R04295)《钶(铌)合金片材、带材和板材 10Hf 1 0Ti》.pdf
《SAE AMS 7852C-2013 Columbium (Niobium) Alloy Sheet Strip and Plate 10Hf - 1 0Ti (UNS R04295)《钶(铌)合金片材、带材和板材 10Hf 1 0Ti》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 7852C-2013 Columbium (Niobium) Alloy Sheet Strip and Plate 10Hf - 1 0Ti (UNS R04295)《钶(铌)合金片材、带材和板材 10Hf 1 0Ti》.pdf(6页珍藏版)》请在麦多课文档分享上搜索。
1、_SAE Technical Standards Board Rules SURYLGHWKDW7KLVUHSRUWLVSXEOLVKHGE6$(WRDGYDQFHWKHVWDWHRI WHFKQLFDODQGHQJLQHHULQJVFLHQFHV7KHXVHRIWKLVUH port is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising WKHUHIURPLVWKHVROHUHVSRQVLELO
2、LWRIWKHXVHUSAE 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 2017 SAE InternationalAll rights reserved. No part of this publication may be reproduced, stored i
3、n 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: +1 724-776-4970 (outside USA)Fax: 724-776-0790Email: C
4、ustomerServicesae.orgSAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedback on thisTechnical Report, please visithttp:/standards.sae.org/AMS7852CAEROSPACEMATERIAL SPECIFICATIONAMS7852REV. CIssued 1980-04Revised 2013-05Reaffirmed 2017-01Superseding AMS7852BColumbium (Niobium) Al
5、loy Sheet, Strip, and Plate,10Hf - 1.0Ti(Composition Similar to UNS R04295)RATIONALEAMS7852C has been reaffirmed to comply with the SAE five-year review policy.1. SCOPE1.1 FormThis specification covers a columbium (niobium) alloy in the form of sheet, strip, and plate.1.2 ApplicationThis material ha
6、s been used typically for parts requiring exposure at ultra-high temperatures, but usage is not limited to such applications. Applications in oxidizing atmospheres necessitate a protective coating.2. APPLICABLE DOCUMENTS: The issue of the following documents in effect on the date of the purchase ord
7、er 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 and no superseding document has been specified, the last published issue o
8、f that document shall apply.2.1 SAE PublicationsAvailable 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 Tolerances, Corrosion and Heat Resistant Steel, Iron Alloy, Titanium, and
9、 Titanium Alloy Sheet, Strip, and PlateAMS2809 Identification, Titanium and Titanium Alloy Wrought Products2.2 ASTM PublicationsAvailable from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org.ASTM E 3 Preparation of Metallogr
10、aphic SpecimensASTM E 8 / E 8M Tension Testing of Metallic MaterialsASTM E 112 Determining Average Grain SizeASTM E 290 Bend Testing Material for DuctilityASTM E 384 Knoop and Vickers Hardness of MaterialsASTM E 2626 Spectrometric Analysis of Reactive and Refractory Metals 3. TECHNICAL REQUIREMENTS3
11、.1 CompositionShall conform to the percentages by weight shown in Table 1. Metallic elements shall be determined by spectrochemical methods in accordance with ASTM E 2626 or by other analytical methods acceptable to purchaser, carbon shall be determined by the combustion method using an infrared det
12、ection system; oxygen, nitrogen and hydrogen shall be determined by the inert gas fusion technique and columbium shall be determined by difference.TABLE 1 COMPOSITIONElement min maxCheck Analysis (3.1.2)Under min or over maxHafnium 9.00 11.00 0.15Titanium 0.70 1.30 0.07Zirconium - 0.70 0.05Tungsten
13、- 0.50 0.03Tantalum - 0.50 0.05Carbon - 0.015 NoneOxygen - 0.0225 (225 ppm) NoneNitrogen - 0.015 (150 ppm) NoneHydrogen - 0.0015 ( 15 ppm) NoneOther Elements, total (3.1.1) - 0.30 NoneColumbium (Niobium) remainder3.1.1 Determination not required for routine acceptance.3.1.2 Check analysis limits are
14、 applicable only to purchaser verification testing; producers test results shall conform to min and max limits of Table 1.3.2 Melting PracticeAlloy shall be multiple vacuum melted using electron beam or consumable electrode practice.3.3 ConditionCold rolled or hot-cold rolled, descaled, and recrysta
15、llized.SAE INTERNATIONAL AMS7852C Page 2 of 6_3.4 PropertiesThe product shall conform to the following requirements:3.4.1 Average Grain SizeShall be as follows, determined by comparison of a polished and etched specimen with the chart in ASTM E 112:3.4.1.1 Sheet and Strip Under 0.160 Inch (4.06 mm)
16、in Nominal ThicknessPredominantly 5 or finer .3.4.1.2 Product 0.160 to 0.750 Inch (4.06 to 19.05 mm) Inclusive in Nominal ThicknessPredominantly 3 or finer .3.4.2 Tensile Properties: Shall be as shown in Table 2, determined in accordance with ASTM E 8 / E 8M.TABLE 2A MINIMUM TENSILE PROPERTIES, INCH
17、/POUND UNITSNominal Thickness, InchesTensile Strength, ksiYield Strength at 0.2% Offset, ksiElongation in 1 inch, %Up to 0.125, incl 54 40.0 20Over 0.125 54 38.0 20TABLE 2B - MINIMUM TENSILE PROPERTIES, SI UNITSNominal Thickness, MillimetersTensile Strength, MPaYield Strength at 0.2% Offset, MPaElon
18、gation in 25.4 mm, %Up to 3.18, incl 372 276 20Over 3.18 372 262 203.4.3 BendingProduct shall have a test sample prepared nominally 0.750 inch (19.06 mm) in width with axis of bending parallel to the direction of rolling. The sample shall be bend tested in conformance with the guided bend test defin
19、ed in ASTM E 290 at 64 to 84 F (18 to 29 C) through an angle of 105 degrees with the speed of bending not less than 1.0 inch (25 mm) per minute. The test fixture supports shall have a minimum contact radius of 0.010 inch (0.25 mm) and the plunger shall have a radius equal to the bend factor shown in
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