SAE AMS 4535D-2015 Copper-Beryllium Alloy Mechanical Tubing 98Cu - 1 9Be Solution and Precipitation Heat Treated (TF00 formerly AT) (UNS C17200).pdf
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1、AEROSPACE MATERIAL SPECIFICATION AMS4535 REV. D Issued 1991-07 Reaffirmed 2012-04 Revised 2015-01 Superseding AMS4535C Copper-Beryllium Alloy, Mechanical Tubing 98Cu - 1.9Be Solution and Precipitation Heat Treated (TF00, formerly AT) (Composition similar to UNS C17200) RATIONALE AMS4535D revises Con
2、dition (3.2) and Solution Annealing (3.3.1). 1. SCOPE 1.1 Form This specification covers a copper-beryllium alloy in the form of mechanical tubing. 1.2 Application This tubing has been used typically for parts requiring a combination of high strength, wear resistance, and corrosion resistance and wh
3、ere thermal conductivity, electrical conductivity, and low magnetic susceptibility may be important, but usage is not limited to such applications. 1.3 Safety - Hazardous Materials While the materials, methods, applications, and processes described or referenced in this specification may involve the
4、 use of hazardous materials, this specification does not address the hazards which may be involved in such use. It is the sole responsibility of the user to ensure familiarity with the safe and proper use of any hazardous materials and to take necessary precautionary measures to ensure the health an
5、d safety of all personnel involved. 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 issu
6、e 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. _ SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineerin
7、g sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be re
8、vised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions. Copyright 2015 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photo
9、copying, 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: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide
10、feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AMS4535D SAE INTERNATIONAL AMS4535D Page 2 of 5 2.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (o
11、utside USA), www.sae.org. AMS2223 Tolerances, Copper and Copper Alloy Seamless Tubing AMS2750 Pyrometry 2.2 ASTM Publications 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 B 251 General Requirements for
12、 Wrought Seamless Copper and Copper-Alloy Tube ASTM B 251M General Requirements for Wrought Seamless Copper and Copper-Alloy Tube (Metric) ASTM B 643 Copper-Beryllium Alloy Seamless Tube ASTM E 3 Preparation of Metallographic Specimens ASTM E 8/E 8M Tension Testing of Metallic Materials ASTM E 18 Ro
13、ckwell Hardness of Metallic Materials ASTM E 112 Determining Average Grain Size ASTM E 478 Chemical Analysis of Copper Alloys 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Table 1, determined by wet chemical methods in accordance with ASTM E 478, by sp
14、ectrochemical methods, or by other analytical methods acceptable to purchaser. TABLE 1 - Composition Element (3.1.1) min max Beryllium 1.80 2.00 Nickel + Cobalt 0.20 - Nickel + Cobalt + Iron - 0.6 Aluminum - 0.20 Silicon - 0.20 Copper (3.1.2) remainder Sum of Named Elements (3.1.3) 99.5 - 3.1.1 Thes
15、e composition limits do not preclude the presence of other elements. Limits may be established and analysis required for unnamed elements by agreement between the manufacturer or supplier and purchaser. 3.1.2 Copper may be reported as “remainder”, or as the difference between the sum of results for
16、all elements and 100%, or as the result of direct analysis. SAE INTERNATIONAL AMS4535D Page 3 of 5 3.1.3 When all the elements in the table are analyzed, the sum shall be 99.5% minimum, but such determination is not required for routine acceptance of each lot. 3.2 Condition Hot reduced or hot and co
17、ld reduced into a tube, solution and precipitation heat treated; TF00 Temper (See 8.2). Product shall not be produced from solid bar by machining methods. 3.3 Heat Treatment Tubing shall be heat treated as follows; pyrometry shall be in accordance with AMS2750. 3.3.1 Solution Annealing Heat within t
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