SAE AMS 2485L-2016 Coating Black Oxide.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 revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions. Copyright 2016 SAE International All rights reserved. No part of this p
3、ublication 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: +1 724-776-497
4、0 (outside USA) 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/AMS2485L AEROSPACE MATERIAL SPECIFICATION AMS2485 REV. L Issued 1948-05 Revised 2
5、016-02 Superseding AMS2485K Coating, Black Oxide RATIONALE AMS2485L results from a five year review and update of this specification. NOTICE ORDERING INFORMATION: The following information shall be provided to the plating processor by the purchaser. Purchase order shall specify not less than the fol
6、lowing: AMS2485L Basis metal to be treated Tensile strength or hardness of the basis metal Pretreatment stress relief to be performed by processor (time and temperature) if different from 3.1.2 Special features, geometry, or processing present on parts that requires special attention by the processo
7、r Optional: Periodic testing frequency (4.2.2) and sample quantity (4.3.2) Quantity of pieces to be coated 1. SCOPE 1.1 Purpose This specification covers the requirements for black oxide coatings on parts. 1.2 Application This coating has been used typically to improve the anti-chafing and anti-fric
8、tion properties of carbon and low-alloy steel parts, particularly for sliding or bearing surfaces, by providing a finish coating that retains an oil film, but usage is not limited to such applications. SAE INTERNATIONAL AMS2485L Page 2 of 6 1.3 Safety - Hazardous Materials While the materials, metho
9、ds, 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 responsibility of the user to ensure familiarity with the safe and proper use of
10、 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 purchase order forms a part of this specification to the extent specified herein.
11、 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 published issue of that document shall apply. 2.1 ASTM Publications Available from AST
12、M International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM G46 Examination and Evaluation of Pitting Corrosion 3. TECHNICAL REQUIREMENTS 3.1 Preparation 3.1.1 The coating shall be applied to part surfaces free from water-breaks. The
13、 cleaning procedure shall not produce pitting or intergranular attack of the basis metal and shall preserve dimensional requirements 3.1.2 Steel parts having a hardness of 36 HRC and higher and that are machined, ground, cold worked or straightened shall be cleaned to remove surface contamination an
14、d thermally stress relieved before coating. Temperatures to which parts are heated shall be such that maximum stress relief is obtained while still maintaining hardness of parts within drawing limits. Unless otherwise specified, the following treatment temperatures and times shall be used: 3.1.2.1 F
15、or parts, excluding nitrided parts, having a hardness of 55 HRC and above, including carburized and induction hardened parts, stress relieve at 275 F 25 F (135 C 14 C) for a minimum of 4 hours. 3.1.2.2 For parts having a hardness less than 55 HRC, stress relieve at 375 F 25 F (191 C 14 C) for a mini
16、mum of 4 hours. Nitrided parts fall into this category. Higher temperatures shall be used only when specified or approved by the cognizant engineering organization. 3.2 Procedure 3.2.1 The cleaned parts, while still wet, shall be immersed in one or more boiling aqueous alkali oxidizing baths for tim
17、es and at temperatures which will produce coatings meeting the requirements of 3.3 and 3.4 (see 8.3). 3.2.2 Coated parts shall be washed thoroughly in running water to remove all traces of processing solution and salts. Parts shall not be allowed to dry during the entire sequence of operations until
18、 completion of this rinse. 3.2.3 Parts shall be thoroughly dried unless a water-displacing oil is used in 3.2.4, in which case complete drying may be omitted. 3.2.4 Parts shall be dipped in a suitable corrosion-preventative oil. SAE INTERNATIONAL AMS2485L Page 3 of 6 3.3 Properties Coated parts shal
19、l conform to the following requirements: 3.3.1 Smut Test Coatings on parts before oiling as in 3.2.4, or on oiled parts after degreasing, shall show no indications of reddish-brown or green smut when wiped with a clean, white cloth. 3.3.2 Dimensional Change When determined using a micrometer accurat
20、e to 0.0001 inch (2.5 mm), no dimensional change shall result from processing. 3.3.3 Oxalic Acid Spot Test The coating, prior to application of corrosion preventative oil, shall be tested as follows. Clean, dry coated parts or specimens of the same composition and heat treat condition as the parts a
21、nd processed with the parts represented shall be handled with clean gloves. Each sample shall have deposited three drops of a 5% (approximately) solution of oxalic acid on a flat surface. Permit the accompanying reaction to continue for not less than eight minutes, followed by rinsing in cool water
22、and drying. When examined, the area which was directly under the acid test solution drops shall exhibit a black or dark brown center with a light border. Areas under the drop, which exhibit a gray center and lighter border are marginal coatings and are not acceptable. 3.3.4 Surface and Intergranular
23、 Attack The cleaning and coating process shall not result in any surface pitting, as determined by ASTM G46 and intergranular attack, determined on metallographically-prepared cross-sections examined unetched at 400X to 500X magnification. 3.4 Quality Except as otherwise specified herein, the coatin
24、g on polished surfaces shall be a uniformly lustrous black. Coating on other surfaces shall be black or dark gray in color, uniform on areas of equivalent surface roughness. Coating on all types of surfaces shall be free of spots of red oxide or an overall reddish-brown color but an overall reddish-
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