SAE AMS 4952F-2015 Titanium Alloy Welding Wire 6AI - 2Sn - 4Zr - 2Mo (UNS R54620).pdf
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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 there
2、from, 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 2015 SAE International All rights reserved. No part of this p
3、ublication 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: +1 724-776-497
4、0 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AMS4952F AEROSPACE MATERIAL SPECIFICATION AMS4952 REV. F Issued 1988-07 Revised 2
5、015-12 Superseding AMS4952E Titanium Alloy, Welding Wire 6AI - 2Sn - 4Zr - 2Mo (Composition similar to UNS R54620) RATIONALE AMS4952F results from a Five Year Review and update of this specification that includes the removal of sample size allowance for hydrogen of Table 1 (covered by ASTM E1447) an
6、d revises the report paragraph (4.4). 1. SCOPE 1.1 Form This specification covers a titanium alloy in the form of welding wire. 1.2 Application This wire has been used typically as filler metal for gas-metal-arc and gas-tungsten-arc welding, but usage is not limited to such applications. 2. APPLICAB
7、LE 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 document ha
8、s 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 +1 724-776-4970 (outside USA)
9、, www.sae.org. AMS2249 Chemical Check Analysis Limits, Titanium and Titanium Alloys AMS2813 Packaging and Marking of Packages of Welding Wire, Standard Method AMS2814 Packaging and Marking of Packages of Welding Wire, Premium Quality AMS2816 Identification Welding Wire, Tab Marking Method SAE INTERN
10、ATIONAL AMS4952F Page 2 of 7 AMS2819 Identification, Welding Wire Direct Color Code System ARP1876 Weldability Test for Weld Filler Metal Wire ARP4926 Alloy Verification and Chemical Composition Inspection of Welding Wire 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive
11、, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM E1409 Determination of Oxygen and Nitrogen in Titanium and Titanium Alloys by the Inert Gas Fusion Technique ASTM E1447 Determination of Hydrogen in Titanium and Titanium Alloys by the Inert Gas Fusion Thermal C
12、onductivity/Infrared Detection Method ASTM E1941 Determination of Carbon in Refractory and Reactive Metals and Their Alloys by Combustion Analysis ASTM E2371 Analysis of Titanium and Titanium Alloys by Direct Current Plasma and Inductively Coupled Plasma Atomic Emission Spectrometry 3. TECHNICAL REQ
13、UIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Table 1; carbon shall be determined in accordance with ASTM E1941, hydrogen in accordance with ASTM E1447, oxygen and nitrogen in accordance with ASTM E1409, and other elements in accordance with ASTM E2371. Other analytic
14、al methods may be used if acceptable to the purchaser. Table 1 - Composition Element min max Aluminum 5.50 6.50 Zirconium 3.60 4.40 Molybdenum 1.80 2.20 Tin 1.80 2.20 Oxygen (3.1.1.1) - 0.15 Silicon - 0.10 Iron - 0.10 Copper - 0.10 Carbon (3.1.1.1) - 0.04 Nitrogen (3.1.1.1) - 0.0400 (400 ppm) Hydrog
15、en (3.1.1.1) - 0.0125 (125 ppm) Yttrium (3.1.1.2) - 0.0050 (50 ppm) Boron - 0.0030 (30 ppm) Other Elements, each (3.1.1.2) - 0.10 Other Elements, total (3.1.1.2) - 0.40 Titanium remainder 3.1.1 Except for carbon, oxygen, nitrogen, and hydrogen, chemical analysis of initial bar or rod stock before dr
16、awing is acceptable provided the processes used for drawing or rolling, annealing, and cleaning are controlled to ensure conformance to composition requirements. 3.1.1.1 Carbon, oxygen, nitrogen, and hydrogen shall be determined on each lot of finished wire. 3.1.1.2 Determination not required for ro
17、utine acceptance. SAE INTERNATIONAL AMS4952F Page 3 of 7 3.1.2 Check Analysis Composition variations shall meet the applicable requirements of AMS2249. 3.2 Melting Practice Alloy shall be multiple melted. The first melt shall be made by vacuum consumable electrode, nonconsumable electrode, electron
18、beam cold hearth, or plasma arc cold hearth melting practice. The subsequent melt or melts shall be made under vacuum using vacuum arc remelting (VAR) practice. Alloy additions are not permitted in the final melt cycle. 3.2.1 The atmosphere for nonconsumable electrode melting shall be vacuum or shal
19、l be argon and/or helium at an absolute pressure not higher than 1000 mm of mercury. 3.2.2 The electrode tip for nonconsumable electrode melting shall be water-cooled copper. 3.3 Condition Cold drawn, bright finish, in a temper and with a surface finish that will provide proper feeding of the wire i
20、n machine-welding equipment. 3.4 Fabrication 3.4.1 Wire shall be formed from rod or bar descaled by a process that does not affect the composition of the wire. Surface irregularities inherent with a forming process that does not teat the wire surface are acceptable provided the wire conforms to the
21、tolerances of 3.7. 3.4.2 In-process annealing, if required between rolling or drawing operations, shall be performed in a vacuum or in a protective atmosphere to avoid surface oxidation and adsorption of other extraneous elements. Material shall have been chemically or mechanically cleaned prior to
22、annealing. 3.4.3 Butt welding is permissible only at diameters larger than final finished product size provided both ends to be joined are either alloy verified using a method or methods capable of distinguishing the alloy from all other alloys processed within the facility, or the repair is made at
23、 the wire processing station. The butt weld shall not interfere with the uniform, uninterrupted feeding of the wire in machine welding equipment. 3.4.4 Drawing compounds, oxides, dirt, oil, and other foreign materials shall be removed by cleaning processes that will neither result in pitting nor cau
24、se gas absorption by the wire or deposition of substances harmful to welding operations. 3.4.5 Surface contaminants or dissolved gasses picked up during wire processing that can adversely affect the welding characteristics, the operation of the equipment, or the properties of the weld material, shal
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