SAE AMS 4953G-2015 Titanium Alloy Welding Wire 5Al - 2 5Sn (UNS R54520).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/AMS4953G AEROSPACE MATERIAL SPECIFICATION AMS4953 REV. G Issued 1958-03 Revised 2
5、015-12 Superseding AMS4953F Titanium Alloy Welding Wire 5Al - 2.5Sn (Composition similar to UNS R54520) RATIONALE AMS4953G 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) and revises t
6、he 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 for gas-metal-arc and gas-tungsten-arc welding, but usage is not limited to such applications. 2. APPLICABLE DOCUMENTS The issue of t
7、he 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 has been cancelled and no sup
8、erseding 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), www.sae.org. AMS2249 Chem
9、ical 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 INTERNATIONAL AMS4953G Page 2 of
10、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, P.O. Box C700, West Consh
11、ohocken, 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 Conductivity/Infrared Detect
12、ion 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 REQUIREMENTS 3.1 Composition S
13、hall 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 analytical methods may be used if a
14、cceptable to the purchaser. Table 1 - Composition Element min max Aluminum 4.50 5.75 Tin 2.00 3.00 Iron - 0.50 Oxygen (3.1.1.1) - 0.175 Carbon (3.1.1.1) - 0.08 Nitrogen (3.1.1.1) - 0.05 Hydrogen (3.1.1.1) - 0.015 (150 ppm) Yttrium (3.1.1.2) - 0.005 ( 50 ppm) Other Elements, each (3.1.1.2) - 0.10 Oth
15、er Elements, total (3.1.1.2) - 0.40 Titanium remainder 3.1.1 Except for carbon, oxygen, nitrogen, and hydrogen, chemical analysis of initial ingot, bar, or rod stock before drawing is acceptable provided the processes used for drawing or rolling, annealing, and cleaning are controlled to ensure cont
16、inued conformance to composition requirements. 3.1.1.1 Carbon, oxygen, nitrogen, and hydrogen shall also be determined on each lot of finished wire. 3.1.1.2 Determination not required for routine acceptance. 3.1.2 Check Analysis Composition variations shall meet the applicable requirements of AMS224
17、9. SAE INTERNATIONAL AMS4953G Page 3 of 7 3.2 Melting Practice Alloy shall be multiple melted. The first melt shall be made by vacuum consumable electrode, nonconsumable electrode, electron beam cold hearth, or plasma arc cold hearth melting practice. The subsequent melt or melts shall be made under
18、 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 shall be inert gas at a pressure not higher than 1000 mm of mercury. 3.2.2 The electrode tip for nonconsumable ele
19、ctrode 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 in 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
20、 the composition of the wire. Surface irregularities inherent with a forming process that does not tear the wire surface are acceptable provided the wire conforms to the tolerances of 3.7. 3.4.2 In-process annealing, if required between rolling or drawing operations, shall be performed in a vacuum o
21、r in a protective atmosphere to avoid surface oxidation and adsorption of other extraneous elements. Material shall have been chemically or mechanically cleaned prior to annealing. 3.4.3 Butt welding is permissible only at diameters larger than final finished product size provided both ends to be jo
22、ined 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 the wire processing station. The butt weld shall not interfere with the uniform, uninterrupted feeding of the wire in machine wel
23、ding equipment. 3.4.4 Drawing compounds, oxides, dirt, oil, and other foreign materials shall be removed by cleaning processes which will neither result in pitting, nor cause gas absorption by the wire or deposition of substances harmful to welding operations. 3.4.5 Surface contaminants or dissolved
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