SAE AMS 4956G-2016 Titanium Alloy Welding Wire 6Al C 4V Extra Low Interstitial Environment Controlled Packaging (UNS R56408).pdf
《SAE AMS 4956G-2016 Titanium Alloy Welding Wire 6Al C 4V Extra Low Interstitial Environment Controlled Packaging (UNS R56408).pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4956G-2016 Titanium Alloy Welding Wire 6Al C 4V Extra Low Interstitial Environment Controlled Packaging (UNS R56408).pdf(7页珍藏版)》请在麦多课文档分享上搜索。
1、_ SAE Technical Standards Board RuleVSURYLGHWKDW7KLVUHSRUWLVSXEOLVKHGE6$(WRDGYDQFHWKH VWDWHRIWHFKQLFDODQGHQJLQHHULQJVFLHQFHV7KHXVHRIWKLV report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arisiQJWKHUHIURPLVWKHVROHUHVSRQVLELOL
2、WRIWKHXVHU 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, stored
3、 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: 724-776-0790 Em
4、ail: 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/AMS4956G AEROSPACE MATERIAL SPECIFICATION AMS4956 REV. G Issued 1969-05 Reaffirmed 2013-04 Revised 2016-06 Supersedin
5、g AMS4956F Titanium Alloy Welding Wire 6Al 4V, Extra Low Interstitial Environment Controlled Packaging (Composition similar to UNS R56408) RATIONALE AMS4956G removes allowance of larger size sample for hydrogen analysis (covered by ASTM E1447), adds continuous heat treating of smaller diameter wire
6、and allows vacuum degassing. 1. SCOPE 1.1 Form This specification covers a titanium alloy in the form of wire for welding filler metal. 1.2 Application This wire has been used typically as filler metal for gas-tungsten-arc welding with chemistry matched to weld low interstitial grade Ti 6Al-4V ELI (
7、UNS R56401) intended for cryogenic or elevated temperature applications, but usage is not limited to such applications. It is particularly intended for use with equipment providing continuous inert gas shielding of the wire as it passes from the dispenser to the welding arc, where high reliability o
8、f joints is required. 2. APPLICABLE 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
9、. 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 Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada)
10、 or +1 724-776-4970 (outside USA), www.sae.org. AMS2249 Chemical Check Analysis Limits Titanium and Titanium Alloys AMS2814 Packaging and Marking of Packages of Welding Wire Premium Quality SAE INTERNATIONAL AMS4956G Page 2 of 7 AMS2816 Identification Welding Wire, Tab Marking Method AMS2819 Identif
11、ication, 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 Chemical Composition Inspection of Welding Wire 2.2 ASTM Publications Available from ASTM Internati
12、onal, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM E539 Analysis of Titanium Alloys by X-Ray Fluorescence Spectrometry ASTM E1409 Determination of Oxygen and Nitrogen in Titanium and Titanium Alloys by the Inert Gas Fusion ASTM E1447 D
13、etermination 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 Titanium and Titanium Alloys by Direct C
14、urrent Plasma and Inductively Coupled Plasma Atomic Emission Spectrometry 3. TECHNICAL REQUIREMENTS 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 ac
15、cordance with ASTM E1409, and other elements in accordance with ASTM E539 or ASTM E2371. Other analytical methods may be used if acceptable to the purchaser. Table 1 - Composition Element min max Aluminum Vanadium Iron Oxygen (3.1.1.1) Carbon (3.1.1.1) Nitrogen (3.1.1.1) Hydrogen (3.1.1.1) Yttrium (
16、3.1.1.2) Other Elements, each (3.1.1.2) Other Elements, total (3.1.1.2) Titanium 5.50 3.50 - 0.03 - - - - - - remainder 6.75 4.50 0.15 0.11 0.03 0.012 (120 ppm) 0.005 ( 50 ppm) 0.005 ( 50 ppm) 0.03 0.10 SAE INTERNATIONAL AMS4956G Page 3 of 7 3.1.1 Except for carbon, oxygen, nitrogen, and hydrogen, c
17、hemical 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 composition requirements. 3.1.1.1 Carbon, oxygen, nitrogen, and hydrogen shall also be deter
18、mined 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 AMS2249. 3.2 Melting Practice Alloy shall be multiple melted. Melting cycle(s) prior to final melting cycle shall be ma
19、de using vacuum consumable electrode, nonconsumable electrode, electron beam cold hearth, or plasma arc cold hearth melting practice(s). The final melting cycle shall be made under vacuum using vacuum arc (VAR) practice with no alloy additions permitted. 3.2.1 The atmosphere for nonconsumable electr
20、ode 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 electrode melting shall be water-cooled copper. 3.3 Condition Except as specified in 3.3.1, vacuum annealed. 3.3.1 Continuous Heat Treatment Wire 0.125 inch (
21、3.18 mm) and under in diameter may be continuously heat treated provided that process parameters (e.g., furnace temperature set points, heat input, travel rate, etc.) for continuous heat treating lines shall be established by the material producer and validated by testing of product to requirements
22、of 3.5. 3.4 Fabrication 3.4.1 Wire shall be rolled or drawn 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 tear the wire surface are acceptable provided the wire conforms to the tolerances o
23、f 3.7. 3.4.2 In-process annealing, if required between rolling or drawing operations, shall be performed after cleaning the material and in a vacuum or in protective inert atmosphere to avoid surface oxidation and adsorption of other extraneous elements unless the contaminated surface is removed mec
24、hanically or chemically. 3.4.3 Butt welding is permissible 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 of a wire break is made at the wire processing station
- 1.请仔细阅读文档,确保文档完整性,对于不预览、不比对内容而直接下载带来的问题本站不予受理。
- 2.下载的文档,不会出现我们的网址水印。
- 3、该文档所得收入(下载+内容+预览)归上传者、原创作者;如果您是本文档原作者,请点此认领!既往收益都归您。
下载文档到电脑,查找使用更方便
10000 积分 0人已下载
下载 | 加入VIP,交流精品资源 |
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- SAEAMS4956G2016TITANIUMALLOYWELDINGWIRE6ALC4VEXTRALOWINTERSTITIALENVIRONMENTCONTROLLEDPACKAGINGUNSR56408PDF

链接地址:http://www.mydoc123.com/p-1021832.html