SAE AMS 4955H-2016 Titanium Alloy Welding Wire 8Al - 1Mo - 1V (UNS R54810).pdf
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1、_ 6$(7HFKQLFDO6WDQGDUGV%RDUG5XOHVSURYLGHWKDW7KLVUHSRUWLVSX EOLVKHGE6$(WRDGYDQFHWKHVWDWHRIWHFKQLFDO 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 therefrom, LVWKHVROHUHVSR
2、QVLELOLWRIWKHXVHU 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 2016 SAE International All rights reserved. No part of this publication may be reproduced,
3、 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 (outside USA) Fax: 724-776-
4、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/AMS4955H AEROSPACE MATERIAL SPECIFICATION AMS4955 REV. H Issued 1965-11 Revised 2016-06 Superseding AMS4955G T
5、itanium Alloy, Welding Wire 8Al - 1Mo - 1V (Composition similar to UNS R54810) RATIONALE AMS4955H is a Five Year Review and update of this specification that removes allowance of larger sample size for hydrogen (included in E1447), adds AMS2368 for sampling and revises reporting. 1. SCOPE 1.1 Form T
6、his 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 of titanium alloys, but usage is not limited to such applications. 2. APPLICABLE DOCUMENTS The issue of the followin
7、g 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 superseding do
8、cument 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 Chemical Check
9、Analysis Limits Titanium and Titanium Alloys AMS2368 Sampling and Testing of Wrought Titanium Raw Material Except Forgings and Forging Stock AMS2813 Packaging and Marking of Packages of Welding Wire Standard Method AMS2814 Packaging and Marking of Packages of Welding Wire Premium Quality AMS2816 Ide
10、ntification Welding Wire, Tab Marking Method SAE INTERNATIONAL AMS4955H Page 2 of 7 AMS2819 Identification, Welding Wire Direct Color Code System ARP1876 Weldability Test for Weld Filler Metal Wire ARP1917 Clarification of Terms Used in Aerospace Metals Specifications ARP4926 Alloy Verification and
11、Chemical Composition Inspection of Welding Wire 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, 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 Ine
12、rt Gas Fusion Technique ASTM E1447 Determination of Hydrogen in Titanium and Titanium Alloys by the Inert Gas Fusion Thermal Conductivity/Infrared Detection Method ASTM E1941 Determination of Carbon in Refractory and Reactive Metals and Their Alloys by Combustion Analysis ASTM E2371 Analysis of Tita
13、nium and Titanium Alloys by Direct Current Plasma and Inductively Coupled Plasma Atomic Emission Spectrometry 3. TECHNICAL REQUIREMENTS 3.1 Wire Composition Shall conform to the percentages by weight shown in Table 1; carbon shall be determined in accordance with ASTM E1941, hydrogen in accordance w
14、ith 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 acceptable to the purchaser. Table 1 - Composition Element min max Aluminum 7.35 8.35 Molybdenum 0.75 1.25 Vanadium 0.75 1.25 Iron - 0.30 Oxyge
15、n (3.1.1.1, 3.1.3) - 0.12 Carbon (3.1.1.1) - 0.08 Nitrogen (3.1.1.1) - 0.05 (500 ppm) Hydrogen (3.1.1.1) - 0.01 (100 ppm) Yttrium (3.1.1.2) - 0.005 ( 50 ppm) Residual Elements, each (3.1.1.2) - 0.10 Residual Elements, total (3.1.1.2) - 0.40 Titanium remainder 3.1.1 Except for carbon, hydrogen, nitro
16、gen, and oxygen, 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 continued conformance to chemical composition requirements. 3.1.1.1 Carbon, hydrogen, nitrogen, and
17、 oxygen shall be determined on each lot of finished wire (see 4.2.1). 3.1.1.2 Determination not required for routine acceptance. SAE INTERNATIONAL AMS4955H Page 3 of 7 3.1.2 Check Analysis Composition variations shall meet the applicable requirements of AMS2249. 3.1.3 When ASTM E1409 is used, sample
18、 sizes larger than those recommended may be used. 3.2 Melting Practice Alloy shall be multiple melted. Melting cycle(s) prior to final melting cycle shall be made using vacuum consumable electrode, nonconsumable electrode, electron beam cold hearth, or plasma arc cold hearth melting practice(s). The
19、 final melting cycle shall be made under vacuum using vacuum arc remelting (VAR) practice with no alloy additions permitted. 3.2.1 The atmosphere for nonconsumable electrode melting shall be vacuum or shall be argon and/or helium at an absolute pressure not higher than 1000 mm of mercury. 3.2.2 The
20、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 in machine welding equipment. 3.4 Fabrication 3.4.1 Wire shall be formed from rod or bar descale
21、d by a process that does not affect 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 Unless the contaminated surface is subsequently removed mechanically o
22、r chemically, any in-process annealing between cold rolling or drawing operations shall be performed after cleaning the material. Annealing shall be performed in a protective atmosphere to avoid surface oxidation and adsorption of other extraneous material. 3.4.3 Butt welding is permissible provided
23、 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 the wire processing station. The butt weld shall not interfere with uniform, uninterrupted feeding of the wire
24、 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 cause gas absorption by the wire or deposition of substances harmful to welding operations. 3.4.5 Surface contaminants
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