SAE AMS 4985E-2014 Titanium Alloy Investment Castings 6Al - 4V 130 UTS 120 YS 6% EL Hot Isostatically Pressed Anneal Optional or When Specified (UNS R56401)《可选型热均衡加压退火或指定的6Al-4V 13.pdf
《SAE AMS 4985E-2014 Titanium Alloy Investment Castings 6Al - 4V 130 UTS 120 YS 6% EL Hot Isostatically Pressed Anneal Optional or When Specified (UNS R56401)《可选型热均衡加压退火或指定的6Al-4V 13.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4985E-2014 Titanium Alloy Investment Castings 6Al - 4V 130 UTS 120 YS 6% EL Hot Isostatically Pressed Anneal Optional or When Specified (UNS R56401)《可选型热均衡加压退火或指定的6Al-4V 13.pdf(11页珍藏版)》请在麦多课文档分享上搜索。
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 theref
2、rom, is the sole responsibility of the user.”SAE 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 2014 SAE InternationalAll rights reserved. No part of this publi
3、cation may be reproduced, stored in 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 (out
4、side USA)Fax: 724-776-0790Email: CustomerServicesae.orgSAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedbackon this Technical Report, please visithttp:/www.sae.org/technical/standards/AMS4985EAEROSPACE MATERIAL SPECIFICATIONAMS4985 REV. EIssued 1983-07Revised 2014-04Supersedin
5、g AMS4985DTitanium Alloy, Investment Castings6Al - 4V130 UTS, 120 YS, 6% ELHot Isostatically PressedAnneal Optional or When Specified(Composition similar to UNS R56401)RATIONALEAMS4985E results from a Five Year Review and update of this specification that aligns hydrogen sample mass with ASTM E 1447
6、 and standardizes reporting requirements.1. SCOPE1.1 FormThis specification covers a titanium alloy in the form of investment castings.1.2 ApplicationThese castings have been used typically for parts of intricate design requiring a combination of good strength-to-weight rate and corrosion resistance
7、, but usage is not limited to such applications.2. APPLICABLE DOCUMENTSThe 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 do
8、cument issue is specified. When the referenced document has been cancelled and no superseding document has been specified, 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
9、(inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org.AMS2175 Castings, Classification and Inspection ofAMS2249 Chemical Check Analysis Limits, Titanium and Titanium AlloysAMS2694 Repair Welding of Aerospace CastingsSAE INTERNATIONAL AMS4985E Page 2 of 11AMS2750 PyrometryAMS2804 Identif
10、ication, Castings2.2 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 B 600 Descaling and Cleaning Titanium and Titanium Alloy SurfacesASTM E 8 / E 8M Tension Testing of Metallic Materials
11、ASTM E 539 Analysis of Titanium Alloys by X-Ray Fluorescence SpectrometryASTM E 1320 Standard Reference Radiographs for Titanium CastingsASTM E 1409 Determination of Oxygen and Nitrogen in Titanium and Titanium Alloys by the Inert Gas Fusion TechniqueASTM E 1417 Liquid Penetrant TestingASTM E 1447 D
12、etermination of Hydrogen in Titanium and Titanium Alloys by the Inert Gas Fusion Thermal Conductivity/Infrared Detection MethodASTM E 1742 Radiographic ExaminationASTM E 1941 Determination of Carbon in Refractory and Reactive Metals and Their Alloys by Combustion AnalysisASTM E 2371 Analysis of Tita
13、nium and Titanium Alloys by Direct Current Plasma and Inductively Coupled Atomic Emission Spectrometry3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the percentages by weight shown in Table 1; carbon shall be determined in accordance with ASTM E 1941, hydrogen in accordance with ASTM E 144
14、7, oxygen and nitrogen in accordance with ASTM E 1409, and other elements in accordance with ASTM E 539 and ASTM E 2371. Other analytical methods may be used if acceptable to the purchaser (See 8.2.1 and 8.2.2).TABLE 1 - COMPOSITIONElement min maxAluminum 5.50 6.75Vanadium 3.50 4.50Iron - 0.30Oxygen
15、 - 0.20Carbon - 0.10Nitrogen - 0.05 (500 ppm)Hydrogen - 0.015 (150 ppm)Yttrium (3.1.1) - 0.005 ( 50 ppm)Other Elements, each (3.1.1) - 0.10Other Elements, total (3.1.1) - 0.40Titanium remainderSAE INTERNATIONAL AMS4985E Page 3 of 113.1.1 Determination not required for routine acceptance.3.1.2 Check
16、AnalysisComposition variations shall meet the applicable requirements of AMS2249.3.2 Melting Practice3.2.1 Castings and specimens shall be poured at casting vendors facility either from a melt (See 8.2.3) of a master heat, or directly from a master heat (See 3.2.3).3.2.1.1 Remelt for CastingCastings
17、 and specimens shall be remelted and poured under inert gas pressure in accordance with 3.2.2.1, or under vacuum without loss of vacuum between melting and pouring.3.2.1.2 If authorized by purchaser (See 8.2.4), portions of two or more qualified master heats of 3.2.3 may be remelted together and pou
18、red into castings using a procedure acceptable to purchaser.3.2.1.3 Remelt for casting shall be performed using consumable electrode-practice or other method authorized by purchaser.3.2.2 Master Heat PreparationA master heat shall be prepared from any combination of elemental and revert materials th
19、at are melted and refined as necessary in a single furnace charge. Single or multiple melting shall be accomplished using consumable electrode, nonconsumable electrode, electron beam cold hearth, or plasma cold hearth practice(s).3.2.2.1 The atmosphere for melting shall be vacuum or shall be argon a
20、nd/or helium at an absolute pressure not higher than 1000 millimeters of mercury.3.2.2.2 Revert (gates, sprues, risers, and rejected castings) may be used in the preparation of master heats.3.2.2.3 Solidification of the master heat into pigs or ingots before remelting and pouring of castings is perm
21、itted.3.2.2.4 The master heat source shall establish effective control procedures, including parameters for the critical variables that will consistently produce material suitable for remelting of castings meeting the requirements of this specification. Control procedures shall be acceptable to purc
22、haser and casting vendor.3.2.3 Master Heat QualificationEach master heat shall be qualified by evaluation of chemical and tensile specimens.3.2.3.1 Specimens shall be either separately-cast, integrally-cast (See 8.2.5), or machined-from-casting, and shall conform to 3.2.1.3.2.3.2 If specimens are se
23、parately-cast, vendor shall have a written procedure acceptable to purchaser. Control factors of 4.4.2.2 shall apply.3.2.3.3 Specimens used for master heat tensile qualification tests shall be hot isostatically pressed, and annealed (See 3.3.2), as specified in the written procedure of 3.2.3.2.3.2.3
24、.4 Specimens used for master heat tensile qualification test may be hot isostatically pressed and annealed separately from castings.3.2.3.5 The acceptance tests of 4.2.1 may be used to satisfy the qualification requirements of 3.2.3.SAE INTERNATIONAL AMS4985E Page 4 of 113.3 Condition3.3.1 Castings
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