SAE AMS 4921N-2016 Titanium Bars Wire Forgings and Rings Commercially Pure 70 ksi (483 MPa) Yield Strength (UNS R50700).pdf
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1、_ 6$(7HFKQLFDO6WDQGDUGV%RDUG5XOHVSURYLGHWKDW7KLVUHSRUWLVSX EOLVKHGE6$(WRDGYDQFHWKHVWDWHRIWHFKQLFDODQGHQJL neering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any partLFXODUXVHLQFOXGLQJDQSDWHQWLQIULQJHPHQWDULVLQJWKHUHIURPLVWKHVROH UHVSRQVLELOLWRIW
2、KHXVHU 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 in
3、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 Email:
4、 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/AMS4921N AEROSPACE MATERIAL SPECIFICATION AMS4921 REV. N Issued 1952-11 Revised 2016-07 Superseding AMS4921M Titanium Bar
5、s, Wire, Forgings, and Rings Commercially Pure 70 ksi (483 MPa) Yield Strength (Composition similar to UNS R50700) RATIONALE AMS4921N results from a Five Year Review and update of this specification that removes of sample size allowance for hydrogen (covered by ASTM E1447), requires agreement on mec
6、hanical property values for material outside specification ranges (3.5.1.1.5), the addition of AS6279 (3.8), added AMS2368 to sampling (4.3) and revises reporting (4.4). 1. SCOPE 1.1 Form This specification covers one grade of commercially-pure titanium in the form of bars, wire, forgings, flash wel
7、ded rings, up to 4.000 inches (101.60 mm), inclusive, in nominal diameter or least distance between parallel sides, and stock for forging or flash welded rings. 1.2 Application These products have been used typically for parts requiring high corrosion resistance and moderate strength up to 400 F (20
8、4 C), and oxidation resistance up to 600 F (316 C), but usage is not limited to such applications. 1.3 Classification 1.3.1 Melting Practice Product covered by this specification is classified by melting practice as follows: Type 1 - Multiple melted with at least one of the melting cycles under vacu
9、um. Type 2 - Electron beam cold hearth or plasma arc cold heath melted. 1.3.1.1 Unless a specific type is ordered, either type may be supplied. SAE INTERNATIONAL AMS4921N Page 2 of 8 1.3.2 Ultrasonic Inspection Product covered by this specification is classified by test requirements as follows: Clas
10、s 1 - Ultrasonic inspection is not required. Class 2 - Product shall be ultrasonically inspected (see 3.6.2). 1.3.2.1 Class 1 may be provided unless Class 2 is specified. 2. APPLICABLE DOCUMENTS The issue of the following documents in effect on the date of the purchase order forms a part of this spe
11、cification 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 document has been specified, the last published issue of that document shall apply
12、. 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. AMS2241 Tolerances, Corrosion and Heat-Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Bars a
13、nd Wire AMS2249 Chemical Check Analysis Limits Titanium and Titanium Alloys AMS2368 Sampling and Testing of Wrought Titanium Raw Material Except Forgings and Forging Stock AMS2631 Ultrasonic Inspection Titanium and Titanium Alloy Bar, Billet and Plate AMS2750 Pyrometry AMS2808 Identification Forging
14、s AMS2809 Identification Titanium and Titanium Alloy Wrought Products AMS7498 Rings, Flash Welded Titanium and Titanium Alloys ARP1917 Clarification of Terms Used in Aerospace Metals Specifications AS6279 Standard Practice for Production, Distribution, and Procurement of Metal Stock 2.2 ASTM Publica
15、tions 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 E8/E8M Tension Testing of Metallic Materials ASTM E1409 Determination of Oxygen and Nitrogen in Titanium and Titanium Alloys by Inert Gas Fusion AST
16、M 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 Titanium and Titanium Alloys by
17、 Direct Current Plasma and Inductively Coupled Plasma Atomic Emission Spectrometry SAE INTERNATIONAL AMS4921N Page 3 of 8 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 accor
18、dance 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 acceptable to the purchaser. Table 1 - Composition Element min max Iron - 0.50 Oxygen - 0.40 Carbon - 0.08 Nitrogen - 0.05 (500 ppm) Hyd
19、rogen - 0.0125 (125 ppm) Other Elements, each (3.1.1) - 0.10 Other Elements, total (3.1.1) - 0.30 Titanium remainder 3.1.1 Determination not required for routine acceptance. 3.1.2 Check Analysis Composition variations shall meet the applicable requirements of AMS2249. 3.2 Melting Practice 3.2.1 Type
20、 1 Alloy shall be multiple melted. Melting cycle(s) prior to the 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 final melting cycle shall be made under vacuum using vacuum arc
21、 remelting (VAR) practice with no alloy additions. 3.2.1.1 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. 3.2.1.2 The electrode tip for nonconsumable electrode melting shall be water-coole
22、d copper. 3.2.2 Type 2 Alloy shall be single cold hearth melted. Either electron beam cold hearth or plasma arc cold hearth melting may be used. 3.3 Condition The product shall be supplied in the following condition: 3.3.1 Bars Hot finished with or without subsequent cold reduction, annealed, and de
23、scaled. A machined or ground surface is permitted unless prohibited by purchaser. The product shall be produced using standard industry practices for the production of bar to the procured thickness/diameter. Cut plate shall not be substituted for bar. 3.3.2 Wire Cold drawn, annealed, and descaled. S
24、AE INTERNATIONAL AMS4921N Page 4 of 8 3.3.3 Forgings and Flash Welded Rings Annealed and descaled. 3.3.4 Flash welded rings shall not be supplied unless specified or permitted on purchasers part drawing. When supplied, the rings shall be manufactured in accordance with AMS7498. 3.3.5 Stock for Forgi
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