SAE AMS 4924H-2015 Titanium Alloy Bars Forgings and Rings-15 5Al - 2 5Sn Extra Low Interstitial Annealed (UNS R54521).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 theref
2、rom, 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 InternationalAll rights reserved. No part of this publi
3、cation 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: +1 724-776-4970 (out
4、side USA)Fax: 724-776-0790Email: CustomerServicesae.orgSAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedbackon this Technical Report, please visithttp:/www.sae.org/technical/standards/AMS4924HAEROSPACEMATERIAL SPECIFICATIONAMS4924 REV. HIssued 1965-09Revised 2015-08Superseding
5、 AMS4924GTitanium Alloy Bars, Forgings, and Rings-155Al - 2.5Sn, Extra Low InterstitialAnnealed(Composition similar to UNS R54521)RATIONALEAMS4924H 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
6、ASTM E1447), requires agreement on mechanical property values for material outside specification ranges (3.5.1.3 and 8.5), the addition of AS6279 (3.8), adds AMS2368 (4.3 and 4.5) and revises the report paragraph (4.5).1. SCOPE1.1 FormThis specification covers a titanium alloy in the form of bars, w
7、ire, forgings, flash welded rings 4.000 inches (101.60 mm) and under in nominal diameter or least distance between parallel sides, and stock for forging and flash welded rings of any size.1.2 ApplicationThese products have been used typically for parts requiring good weldability and high strength-to
8、-weight ratio operating from -250 to -423 F (-155 to -255 C), but usage is not limited to such applications. The room and elevated temperature strengths of this alloy are lower than those of AMS4926 and AMS4966.2. APPLICABLE DOCUMENTSThe issue of the following documents in effect on the date of the
9、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 document has been specified, the last publi
10、shed issue of that document shall apply.2.1 SAE PublicationsAvailable 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,
11、 Titanium, and Titanium Alloy Bars and WireAMS2249 Chemical Check Analysis Limits, Titanium and Titanium AlloysSAE INTERNATIONAL AMS4924H Page 2 of 9AMS2368 Sampling and Testing of Wrought Titanium Raw Material, Except Forgings and Forging StockAMS2375 Control of Forgings Requiring First Article App
12、rovalAMS2750 PyrometryAMS2808 Identification ForgingsAMS7498 Rings, Flash Welded, Titanium and Titanium AlloysAS6279 Production, Distribution, and Procurement of Metal Stock2.2 ASTM PublicationsAvailable from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959,
13、 Tel: 610-832-9585, www.astm.org.ASTM E8/E8M Tension Testing of Metallic MaterialsASTM E1409 Determination of Oxygen and Nitrogen in Titanium and Titanium Alloys by the Inert Gas Fusion TechniqueASTM E1447 Determination of Hydrogen in Titanium and Titanium Alloys by the Inert Gas Fusion Thermal Cond
14、uctivity/Infrared Detection MethodASTM E1941 Determination of Carbon in Refractory and Reactive Metals and Their Alloys by Combustion AnalysisASTM E2371 Analysis of Titanium and Titanium Alloys by Direct Current Plasma and Inductively Coupled PlasmaAtomic Emission Spectrometry3. TECHNICAL REQUIREMEN
15、TS3.1 CompositionShall 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 method
16、s may be used if acceptable to the purchaser.Table 1 - CompositionElement min maxAluminumTinIronOxygenOxygen + IronCarbonNitrogenHydrogen Yttrium (3.1.1)Other Elements, each (3.1.1)Other Elements, total (3.1.1)Titanium4.702.00-remainder5.60 3.00 0.25 0.120.320.05 0.0350.01250.0050.050.40 (350 ppm)(1
17、25 ppm)( 50 ppm)SAE INTERNATIONAL AMS4924H Page 3 of 93.1.1 Determination not required for routine acceptance.3.1.2 Check AnalysisComposition variations shall meet the requirements of AMS2249 except that the check analysis limit for iron shall be 0.05 over maximum.3.2 Melting PracticeAlloy shall be
18、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 vacuum using vacuum arc remelting (VAR) practice. Alloy additions are not per
19、mitted 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 electrode melting shall be water-cooled copper.3.3 ConditionThe product shall be su
20、pplied in the following condition:3.3.1 BarsHot finished with or without subsequent cold reduction, annealed, and descaled. Bar shall be processed to the final thickness/diameter by metallurgical working operations prior to any straightening, dimensional sizing or surface finishing operations. Bar s
21、hall not be cut from plate.3.3.2 WireCold drawn, annealed, and descaled.3.3.3 Forgings and Flash Welded RingsAnnealed and descaled.3.3.3.1 Flash welded rings shall not be supplied unless specified or permitted on purchasers part drawing. Whensupplied, they shall be manufactured in accordance with AM
22、S7498.3.3.4 Stock for Forging or Flash Welded RingsAs ordered by the forging or flash welded ring manufacturer.3.4 AnnealingBars, wire, forgings, and flash welded rings shall be annealed by heating to a temperature within the range 1400 to 1500 F (760 to 815 C), holding at the selected temperature w
23、ithin 25 F (15 C) for not less than 1 hour, and cooling at a rate which will produce product meeting the requirements of 3.5. Pyrometry shall be in accordance with AMS2750.3.5 PropertiesThe product shall conform to the following requirements and shall also meet the requirements of 3.5.1.1 and 3.5.1.
24、2 after being heated to any temperature up to 1200 F (650 C) (See 4.2.2.1), held at heat for 30 minutes 3, cooled in air, and descaled.3.5.1 Bars, Wire, Forgings, and Flash Welded RingsSAE INTERNATIONAL AMS4924H Page 4 of 93.5.1.1 Tensile PropertiesShall be as specified in Table 2 and 3.5.1.2, deter
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