SAE AMS 7857C-2013 Columbium (Niobium) Alloy Bars Rods and Extrusions 10Hf - 1 0Ti Recrystallization Annealed (UNS R04295)《再结晶退火的钶(铌)合金棒材、条材和挤压材10Hf-1 0Ti》.pdf
《SAE AMS 7857C-2013 Columbium (Niobium) Alloy Bars Rods and Extrusions 10Hf - 1 0Ti Recrystallization Annealed (UNS R04295)《再结晶退火的钶(铌)合金棒材、条材和挤压材10Hf-1 0Ti》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 7857C-2013 Columbium (Niobium) Alloy Bars Rods and Extrusions 10Hf - 1 0Ti Recrystallization Annealed (UNS R04295)《再结晶退火的钶(铌)合金棒材、条材和挤压材10Hf-1 0Ti》.pdf(7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/AMS7857CAEROSPACEMATERIAL SPECIFICATIONAMS7857REV. CIssued 1980-04Revised 2013-05Reaffirmed 2017-01Superseding AMS7857BColumbium (Niobium) Al
5、loy Bars, Rods, and Extrusions10Hf - 1.0Ti, Recrystallization Annealed(Composition similar to UNS R04295)RATIONALEAMS7857C 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 bars, rods, and extrusion
6、s.1.2 ApplicationThis material has 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 DOCUMENTSThe issue of the following documents in effect
7、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 and no superseding document has been specif
8、ied, the last published issue of 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.AMS2809 Identification, Titanium and Titanium Alloy
9、 Wrought Products2.2 ASTM PublicationsAvailable from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959Tel: 610-832-9585, www.astm.org.ASTM E 3 Preparation of Metallographic SpecimensASTM E 8 / E 8M Tension Testing of Metallic MaterialsASTM E 18 Rockwell Hardn
10、ess and Rockwell Superficial Hardness of Metallic MaterialsASTM E 112 Determining Average Grain SizeASTM E 384 Knoop and Vickers Hardness of MaterialsASTM E 2626 Spectrometric Analysis of Reactive and Refractory Metals3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the following percentages
11、 by weight shown in Table 1. Metallic elements shall be determined by spectrochemical methods in accordance with ASTM E 2626, carbon shall be determined by the combustion method using an infrared detection system; oxygen, nitrogen and hydrogen shall be determined by the inert gas fusion technique, a
12、ndcolumbium 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 - 0.50 0.03Tantalum - 0.50 0.05Carbon - 0.015 NoneOxygen - 0.0225 (225 ppm) NoneNitrogen - 0.015 (1
13、50 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 applicable only to purchaser verification testing; producers test results shall conform to min and
14、 max limits of Table 1.3.2 Melting PracticeAlloy shall be multiple melted under vacuum, using electron beam or consumable electrode practice.3.3 ConditionHot or cold finished, descaled, and recrystallization annealed.SAE INTERNATIONAL AMS7857C Page 2 of 7_3.4 PropertiesThe product shall conform to t
15、he following requirements:3.4.1 Average Grain SizeShall be as shown in Table 2, determined by comparison of a polished and etched specimen with the chart in ASTM E 112. TABLE 2 GRAIN SIZENominal Diameter or Least Distance Between Parallel Sides Average Grain SizeInches MillimetersUp to 2.0, incl Up
16、to 51, incl 5 or finerOver 2.0 to 4.0, incl Over 51 to 102, incl 4 or finerOver 4.0 Over 102 3 or finer3.4.2 Tensile PropertiesShall be as shown in Table 3, determined in accordance with ASTM E 8 / E 8M:TABLE 3 MINIMUM TENSILE PROPERTIESProperty ValueTensile Strength 54 ksi (372 MPa)Yield Strength a
17、t 0.2% Offset 35.0 ksi (241 MPa)Elongation in 4D 15%Reduction of Area 30%3.4.3 HardnessShall be not higher than 95 HRB, or equivalent (See 8.3), determined in accordance with ASTM E 18, but the product shall not be rejected on the basis of hardness if the tensile property requirements are met on a s
18、pecimen with similar nonconforming hardness.3.4.4 MicrostructureShall be as follows, determined at 100X magnification on specimens prepared in accordance with ASTM E 3:3.4.4.1 SegregationProduct shall be free from evidence of unalloyed elements and from segregation of alloying constituents.3.4.4.2 S
19、urface ContaminationProduct shall be free from surface contamination; a difference in hardness of 50 or more points HK100, determined in accordance with ASTM E 384, between the center of the specimen and a point 0.0015 inch (0.038 mm) from any as-supplied surface shall be construed as evidence of su
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