SAE AMS 7498R-2016 Rings Flash Welded Titanium and Titanium Alloys.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 2016 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:/standards.sae.org/AMS7498R AEROSPACE MATERIAL SPECIFICATION AMS7498 REV. R Issued 1955-03 Revised 2016-12Supersed
5、ing AMS7498P Rings, Flash Welded Titanium and Titanium Alloys RATIONALE AMS7498R results from a Five-Year Review and update of this specification that revises proof testing (3.2.5). 1. SCOPE 1.1 Form This specification covers flash welded rings made of titanium and titanium alloys. 1.2 Application T
6、hese rings have been used typically for parts such as flanges, but usage is not limited to such applications. 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 w
7、ork to a subsequent revision of a document unless a specific document 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 Publications Available from SAE International, 400
8、Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or +1 724-776-4970 (outside USA), www.sae.org. AMS2750 Pyrometry ARP1917 Clarification of Terms Used in Aerospace Metals Specifications SAE INTERNATIONAL AMS7498R Page 2 of 6 2.2 ASTM Publications Available from
9、 ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM E8/E8M Tension Testing of Metallic Materials 3. TECHNICAL REQUIREMENTS 3.1 Material Shall be as specified on the part drawing. 3.2 Fabrication 3.2.1 Forming Rings shall
10、be formed from rolled, extruded, or forged shapes. Grain flow in the formed rings shall be substantially circumferential. 3.2.2 Preparation for Welding 3.2.2.1 Formed rings shall be clean and free from foreign materials in the area of electrode contact and at the surfaces to be welded. 3.2.2.2 Forme
11、d rings may be preheated, before welding, as agreed upon by purchaser and producer. 3.2.3 Welding 3.2.3.1 The ends of the formed rings shall be flash butt-welded together with only one weld per ring. Welding shall be performed on a machine provided with control of the following: Feed of joint during
12、 flashing Rate and distance of travel of the sections to be welded Secondary voltage and current magnitude Timing and current cut off. 3.2.3.2 The flash shall be maintained during the flashing interval of the welding operation. The amount of manual flashing used for preheating shall be limited to 10
13、% of the total flashing distance. The machine shall be capable of repeating the sequence of operations independently of the skill of the machine operator. A record of all machine settings and sequence of operations for each lot shall be maintained in accordance with purchasers requirements. 3.2.4 He
14、at Treatment Welded rings shall be annealed as in 3.2.4.1 or solution heat treated as in 3.2.4.2, as applicable. 3.2.4.1 Annealing Rings, except as specified in 3.2.4.1.1 and 3.2.4.1.2, shall be annealed by heating to 1300 F 25 F (704 C 14 C), holding at heat for not less than 2 hours, and cooling i
15、n air to room temperature. Pyrometry shall be in accordance with AMS2750. 3.2.4.1.1 If the drawing or material specification specifies the annealing cycle, the rings shall be annealed as specified. 3.2.4.1.2 If neither the drawing nor the material specification specifies a required annealing cycle a
16、nd the producer of the material reports use of an annealing temperature higher than 1300 F (704 C), rings may be annealed by heating to a temperature as high as the reported annealing temperature. SAE INTERNATIONAL AMS7498R Page 3 of 6 3.2.4.2 Solution Heat Treatment The rings shall be solution heat
17、 treated when specified in the applicable material specification or drawing. 3.2.5 Proof Testing of Welds (Sizing) Each ring shall be proof tested to determine the quality of the weld. The flash and excess metal at the weld shall be removed to within +0.031 inch (+0.8 mm) of the parent metal and ble
18、nded smoothly before sizing. The stress applied for sizing shall be sufficient to provide a permanent expansion of not less than 1% across a 2 inch (50.8 mm) gage length centered on the weld. The 1% minimum permanent expansion shall be verified by measurement on at least one ring from each welding l
19、ot. Sizing shall be performed to provide a uniform stress distribution throughout the ring. 3.2.5.1 Rings may be heated to a temperature not exceeding 50 F (28 C) below the annealing or solution temperature as specified in 3.2.4 or 50 F (28 C) below producers material certification reported annealin
20、g or solution temperature given to the material. 3.2.5.2 Rings may be sized on cooling from the annealing or solution temperature. 3.2.5.3 For rings less than 0.188 inch (4.78 mm) nominal thickness, flash removal may reduce thickness below parent material provided the thickness is not reduced below
21、the minimum specified. Proof testing shall be waived if the welding precedes a final forming operation that expands the weld equivalent to 3.2.5. 3.2.5.4 When permitted by purchaser, statistical data developed for each part/process combination may be used to substantiate proof testing in lieu of act
22、ual measurements taken on the weld. 3.2.6 When the drawing or applicable material specification requires additional heat treatment, rings shall be so heat treated after sizing. 3.2.7 Restoration to Shape When necessary to restore the shape of rings following annealing or solution heat treatment, suc
23、h operation shall be done on suitable presses and not by localized blows as from a hammer. Except as specified in 3.2.7.1, rings may be heated to not higher than 1250 F (677 C) for such operations. Where rings receive a final heat treatment below 1250 F (677 C), they may be heated to not higher than
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