SAE AMS 6907B-2015 Titanium Alloy Bars Forgings and Forging Stock 6 0Al - 2 0Sn - 4 0Zr - 6 0Mo Duplex Annealed (UNS R56260).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/AMS6907BAEROSPACEMATERIAL SPECIFICATIONAMS6907 REV. BIssued 2004-01Revised 2015-12Superseding
5、 AMS6907ATitanium Alloy Bars, Forgings and Forging Stock6.0Al - 2.0Sn - 4.0Zr - 6.0MoDuplex Annealed(Composition similar to UNS R56260)RATIONALEAMS6907B results from a Five Year Review and update of this specification that includes the removal of sample size allowance for hydrogen of Table 1 (covere
6、d by ASTM E1447), requires agreement on mechanical property values for material outside specification ranges (3.5.1.1.5 and 8.7), the addition of AS6279 (3.8) and revises the report paragraph (4.4).1. SCOPE1.1 FormThis specification covers a titanium alloy in the form of bars, forgings up through 4.
7、000 inches (101.60 mm), inclusive in nominal diameter or least distance between parallel sides and 32 in2(206.46 cm2) maximum cross sectional area, and stock for forging of any size.1.2 ApplicationThese products have been used typically for parts requiring high strength up to 1000 F (538 C), but usa
8、ge is not limited to such applications.1.2.1 Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking; ARP982 recommends practices to minimize such conditions.2. APPLICABLE DOCUMENTSThe issue of the following documents in effect on
9、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 document has been specified
10、, the last published 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 St
11、eel, Iron Alloy, Titanium, and Titanium Alloy Bars and WireSAE INTERNATIONAL AMS6907B Page 2 of 8AMS2249 Chemical Check Analysis Limits, Titanium and Titanium AlloysAMS2368 Sampling and Testing of Wrought Titanium Raw Material Except Forgings and Forging StockAMS2631 Ultrasonic Inspection, Titanium
12、and Titanium Alloy Bar, Billet and PlateAMS2643 Structural Examination of Titanium Alloys, Chemical Etch Inspection ProcedureAMS2750 PyrometryAMS2808 Identification ForgingsAMS2809 Identification, Titanium and Titanium Alloy Wrought ProductsARP982 Minimizing Stress-Corrosion Cracking in Wrought Tita
13、nium Alloy ProductsAS6279 Industry Standard Practices for 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, Tel: 610-832-9585, www.astm.org.ASTM E8/E8M Tension Testin
14、g 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 Conductivity/Infrared Detection MethodASTM E1941 Determination
15、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 REQUIREMENTS3.1 CompositionShall conform to the percentages by weight
16、 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 methods may be used if acceptable to the purchaser.Table 1 - Comp
17、ositionElement min maxAluminum 5.50 6.50Molybdenum 5.50 6.50Zirconium 3.60 4.40Tin 1.75 2.25Iron - 0.15Oxygen - 0.15Carbon - 0.04Nitrogen - 0.04 (400 ppm)Hydrogen - 0.0125 (125 ppm)Yttrium (3.1.1) - 0.005 ( 50 ppm)Other Elements each (3.1.1) - 0.10Other Elements, total (3.1.1) - 0.40Titanium remaind
18、erSAE INTERNATIONAL AMS6907B Page 3 of 83.1.1 Determination not required for routine acceptance.3.1.2 Check AnalysisComposition variations shall meet the applicable requirements of AMS2249.3.2 Melting PracticeAlloy shall be multiple melted. The first melt shall be made by vacuum consumable electrode
19、, 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 permitted in the final melt cycle.3.2.1 The atmosphere for nonconsumable electr
20、ode melting shall be vacuum or shall be argon or helium at an absolute 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 supplied in the following condition:3.3.1 BarsHot finished wit
21、h or without subsequent cold reduction, duplex annealed, and descaled. A machined or ground surface is permitted unless prohibited by the purchaser. The product shall be processed to the final thickness/diameter by metallurgical working operations prior to any straightening, dimensional sizing or su
22、rface finishing operations. Bar shall not be cut from plate.3.3.2 ForgingsDuplex annealed and descaled.3.3.3 Stock for ForgingAs ordered by the forging manufacturer.3.4 Heat TreatmentBars and forgings shall be duplex annealed as follows; pyrometry shall be in accordance with AMS2750:3.4.1 Solution H
23、eat TreatmentHeat to a temperature within the range 1500 to 1675 F (816 to 913 C), hold at the selected temperature within 25 F (14 C) for a time commensurate with section thickness and the heating equipment and procedure used, and cool at a rate equivalent to an air cool or faster.3.4.2 Stabilizati
24、on Heat TreatmentHeat to 1100 F 25 F (593 C 14 C), hold for 8 hours 0.25 hour, and cool at a rate equivalent to air cooling.SAE INTERNATIONAL AMS6907B Page 4 of 83.5 PropertiesThe product shall conform to the following requirements:3.5.1 Bars and Forgings3.5.1.1 Tensile PropertiesShall be as specifi
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