SAE AMS 2728C-2012 Heat Treatment of Wrought Copper Beryllium Alloy Parts《熟铜铍合金零件热处理》.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 reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2012 SAE International All rights reserved. No part of this publication m
3、ay 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 (outside U
4、SA) 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:/www.sae.org/technical/standards/AMS2728C AEROSPACE MATERIAL SPECIFICATION AMS2728 REV. C Issued 1988-01 Revised 2012-09 Super
5、seding AMS2728B Heat Treatment of Wrought Copper Beryllium Alloy Parts RATIONALE AMS2728C results from a Limited Scope Ballot to correct errors present in revision B (3.1.2.2, 3.1.5.1, 3.3.6, 3.3.7, 4.2.2). 1. SCOPE 1.1 Purpose This specification establishes the requirements for heat treatment of wr
6、ought copper beryllium parts (See 1.2.2 and 8.2.1) by users or by their vendors or subcontractors. 1.2 Application This specification is applicable to parts made from the following alloys: UNS C17000, UNS C17200, UNS C17300, UNS C17500, and UNS C17510 (See 8.4). 1.2.1 The heat treat parameters (temp
7、eratures, soaking times, cooling rates, etc.) used by material producers and forge shops for qualification of response to heat treatment of their products shall conform to the requirements of this specification. 1.2.2 Heat treatment of raw material by producers or forge shops shall be in accordance
8、with the material procurement specification. 1.3 While the materials, methods, applications, and processes described or referenced in this specification may involve the use of hazardous materials, this specification does not address the hazards which may be involved in such use. It is the sole respo
9、nsibility 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 and safety of all personnel involved. 2. APPLICABLE DOCUMENTS The issue of the following documents in effect on the date of the purcha
10、se order forms a part of this specification to the extent specified herein. The vendor 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 iss
11、ue of that document shall apply. SAE AMS2728C Page 2 of 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 724-776-4970 (outside USA), www.sae.org. AMS2750 Pyrometry AMS2769 Heat Treatment of Parts
12、 in Vacuum ARP1917 Clarification of Terms Used in Aerospace Metals Specifications ARP1962 Training and Approval of Heat-Treating Personnel 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.
13、 ASTM E 3 Preparation of Metallographic Specimens ASTM E 8/E 8M Tension Testing of Metallic Materials ASTM E 10 Brinell Hardness of Metallic Materials ASTM E 18 Rockwell Hardness of Metallic Materials ASTM E 384 Knoop and Vickers Hardness of Materials 3. TECHNICAL REQUIREMENTS 3.1 Equipment 3.1.1 Py
14、rometry Shall conform to AMS2750. 3.1.2 Furnaces 3.1.2.1 Solution heat treating furnaces shall be a minimum of Class 2 (10 F or 6 C) 3.1.2.2 Precipitation hardening furnaces shall be a minimum of Class 2 ( 10 F or 6 C) 3.1.2.3 Stress Relieving furnaces shall be a minimum of Class 5 (25 F or 14 C) 3.
15、1.2.4 Vacuum furnaces used to perform processes in this specification shall be in accordance with AMS2769. 3.1.3 Heating Media High temperature furnaces with or without controlled atmosphere are acceptable for solution heat treating. Salt baths shall not be used for solution treatments. A muffle fur
16、nace shall be used for solution treating in fuel fired furnaces with an air atmosphere. Circulating atmosphere type furnaces, with or without controlled atmospheres, and salt bath type furnaces are acceptable for precipitation hardening. Still air oven type furnaces are not permitted for age hardeni
17、ng. SAE AMS2728C Page 3 of 12 3.1.4 Racks and Fixtures Shall not cause contamination of product and shall not reduce the heating, cooling, or quenching rates to less than required for correct heat treating. Design and construction shall preclude entrapment of quenchant and minimize deformation or ot
18、her damage to product. 3.1.5 Quenching Equipment 3.1.5.1 Equipment shall be provided for quenching in water and for measuring and recording water temperature. Provisions shall be made for mechanical or hydraulic agitation of the quenching medium and/or agitation of the product and for cooling of the
19、 water as necessary to conform with 3.1.5.3. 3.1.5.2 Air agitation shall not be used. 3.1.5.3 Quench tanks shall be located in proximity to solution heat treating furnaces so that the quench delay times listed in Table 2 can be achieved. The delay time is measured from the time the furnace door star
20、ts to open until complete immersion of the load in quenchant. 3.1.5.4 The quenchant volume shall be sufficient to prevent the quench tank temperature from rising to a temperature greater than the limit established in 3.2.2. 3.1.6 Cleaning Equipment Equipment shall be provided to clean parts before h
21、eat treatment and to remove salt from parts heated in salt baths. 3.2 Heating and Cooling Environment 3.2.1 Atmospheres Shall be controlled so as not to react with the parts being heat treated. Materials that could attack or contaminate shall not contact parts. 3.2.1.1 Solution Treating Atmosphere P
22、arts shall be solution treated in either air or protective atmospheres. Acceptable protective atmospheres are exothermic, argon, helium, nitrogen, hydrogen, blends of these gases, and vacuum (See 3.2.1.1.2). Endothermic atmosphere is not acceptable. To minimize discoloration an air atmosphere should
23、 be avoided. 3.2.1.1.1 Unless specifically informed that the part will be machined all over, the heat treating processor shall heat treat the parts as if some surfaces will not have subsequent metal removal and, therefore, when solution heat treating, shall heat treat using protective atmosphere. 3.
24、2.1.1.2 Vacuum Is permitted for UNS C17000, UNS C17200, and UNS C17300 at 1450 F (790 C), but is not permitted for UNS C17500 and UNS C17510 at 1700 F (925 C). 3.2.1.2 Age Hardening Atmosphere Parts shall be aged in air or protective atmospheres. Acceptable protective atmospheres for age hardening a
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