SAE AMS 2409G-2001 Plating Immersion Tin For Aluminum Alloys《铝合金用浸渍镀锡》.pdf
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1、AEROSPACE MATERIAL SPECIFICATIONAMS 2409GIssued 1948-05Revised 2001-02Superseding AMS 2409FPlating, Immersion TinFor Aluminum Alloys1. SCOPE:1.1 Purpose:This specification covers the engineering requirements for producing a thin tin coating on aluminum alloys by an immersion process.1.2 Application:
2、This process has been used typically to prevent scuffing and galling of aluminum alloy parts, 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 use of
3、 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 and safet
4、y 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 issue is sp
5、ecified. When the referenced document has been canceled and no superseding document has been specified, the last published issue of that document shall apply.Reaffirmed 2009-06 SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and en
6、gineering 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 m
7、ay be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2009 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, photocopy
8、ing, recording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: 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 feedbac
9、kon this Technical Report, please visit http:/www.sae.org/technical/standards/AMS2409G Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AMS 2409G SAE AMS 2409G- 2 -2.1 ASTM Publications: Available fro
10、m ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959.ASTM B 487 Measurement of Metal and Oxide Coating Thickness by Microscopical Examination of a Cross SectionASTM B 567 Measurement of Coating Thickness by the Beta Backscatter MethodASTM B 568 Measurement of Coating Thickness by X-Ray Sp
11、ectrometry3. TECHNICAL REQUIREMENTS: 3.1 Plating Bath: Shall consist of an aqueous solution of stannate salts.3.2 Operating Parameters: Temperature of bath, pH, solution concentration, and immersion time shall be controlled to provide a deposit meeting the requirements of 3.5.3.3 Preparation:Parts s
12、hall have clean surfaces free of waterbreak prior to immersion in the plating solution. Parts shall be transferred to plating solution without drying after rinsing.3.4 Procedure:3.4.1 Parts shall be immersed in the plating bath and shall remain in the bath until reaction is essentially complete, as
13、indicated by virtual cessation of evolution of hydrogen.3.4.1.1 Parts shall not be allowed to dry during the entire sequence of operations until completion of the final rinse.3.4.1.2 After plating, parts shall be thoroughly rinsed and dried.3.5 Properties:Plated tin shall conform to the following re
14、quirements:3.5.1 Thickness: The plate thickness shall be approximately 0.0001 inch (2.5 m), determined in accordance with ASTM B 487, ASTM B 567, ASTM B 568, or other method acceptable to purchaser.3.5.2 Adhesion: Plated parts shall show no blisters after being heated in a circulating-air oven to 30
15、0 F 15 (149 C 8) and held at heat for not less than three hours.Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AMS 2409G SAE AMS 2409G- 3 -3.5.2.1 When acceptable to purchaser, adhesion may be deter
16、mined by scratching the plated surface with a sharp point. When examined at 4 to 6X magnification, there shall be no evidence of flaking of the plating (See 4.3.3).3.6 Quality:Plated tin, as received by purchaser, shall be smooth, continuous, adherent to basis metal, uniform bright gray in appearanc
17、e, and free from blisters and other imperfections detrimental to usage of the plating. Slight staining or discoloration is permissible.4. QUALITY ASSURANCE PROVISIONS: 4.1 Responsibility for Inspection: The processor shall supply all samples for processors tests and shall be responsible for the perf
18、ormance of all required tests. Purchaser reserves the right to sample and to perform any confirmatory testing deemed necessary to ensure that processing conforms to the specified requirements.4.2 Classification of Tests: 4.2.1 Acceptance Tests: Adhesion (3.5.2 or 3.5.2.1, as applicable) and quality
19、(3.6) are acceptance tests and shall be performed to represent each lot.4.2.2 Periodic Tests: Thickness (3.5.1) and tests of cleaning and plating solutions (See 8.4) are periodic tests and shall be performed at a frequency selected by the vendor unless frequency of testing is specified by purchaser.
20、4.2.3 Preproduction Tests: All technical requirements are preproduction tests and shall be performed prior to or on the initial shipment of plated parts to a purchaser, when a change in material and/or processing requires approval by the cognizant engineering organization (See 4.4.2), and when purch
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