SAE AMS 3109-1991 Primer Adhesive Electrodeposited -55 to +82 (-67 o +180 《电解镀层粘胶底漆-55至+82C(-67至+180F)》.pdf
《SAE AMS 3109-1991 Primer Adhesive Electrodeposited -55 to +82 (-67 o +180 《电解镀层粘胶底漆-55至+82C(-67至+180F)》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 3109-1991 Primer Adhesive Electrodeposited -55 to +82 (-67 o +180 《电解镀层粘胶底漆-55至+82C(-67至+180F)》.pdf(13页珍藏版)》请在麦多课文档分享上搜索。
1、AEROSPACE MATERIAL SPECIFICATIONAMS3109Issued 1991-04Reaffirmed 2014-08Primer, Adhesive, Electrodeposited-55 to +82 C (-67 to +180 F)RATIONALEAMS3109 has been reaffirmed to comply with the SAE five year review policy._SAE Technical Standards Board Rules provide that: “This report is published by SAE
2、 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 therefrom, is the sole responsibility of the user.”SAE reviews each technical report at l
3、east every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions.Copyright 2014 SAE InternationalAll rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any form
4、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 USA)Fax: 724-776-0790Email: CustomerServicesae.orgSAE WEB ADDRESS: http:/www.s
5、ae.orgSAE values your input. To provide feedbackon this Technical Report, please visithttp:/www.sae.org/technical/standards/AMS31091. SCOPE:1.1 Form: This specification covers a corrosion-inhibiting, water soluble,modified epoxy primer in liquid form.1.2Application:Primarily for use as a primer with
6、 structural adhesive bondingof metal-to-metal attachments and honeycomb panels.1.3 Safety - Hazardous Materials: While the materials, methods, applications,and processes described or referenced in this specification may involve theuse of hazardous materials, this specification does not address the h
7、azardswhich may be involved in such use. It is the sole responsibility of theuser to ensure familiarity with the safe and proper use of any hazardousmaterials and to take necessary precautionary measures to ensure the healthand safety of all personnel involved.2 APPLICABLE DOCUMENTS: The following p
8、ublications form a art of thisspecification to the extent specified herein. The latest issue of SAEpublications shall apply. The applicable issue of other publications shallbe the issue in effect on the date of the purchase order.2.1 SAE Publications: Available from SAE, 400 Commonwealth Drive, Warr
9、endale,PA 15096-0001.2.1.1 Aerospace Material Specifications:AMS 2825 - Material Safety Data SheetsAMS 4004 - Aluminum Alloy Foil, 2.5Mg - 0.25Cr (5052 - H191, StrainHardenedAMS 4045 - Aluminum Alloy Sheet and Plate, 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr,(7075; -T6 Sheet, -T651 Plate), Solution and Precipi
10、tationHeat TreatedSAE INTERNATIONAL AMS3109 Page 2 of 132.2 ASTM Publications: Available from ASTM, 1916 Race Street, Philadelphia, PA19103-1187.ASTM D 1475 - Density of Paint, Varnish, Lacquer, and Related ProductsASTM D 2369 - Volatile Content of Coatings2.3 U.S. Government Publications: Available
11、 from Standardization DocumentsOrder Desk, Building 4D, 700 Robbins Avenue, Philadelphia, PA 19111-5094.2.3.1 Federal Specifications:MMM-A-132 - Adhesive, Heat Resistant, Airframe Structural, Metal to MetalPPP-P-1892 - Paint, Varnish, Lacquer, ovendrying after processing, however, is optional if spe
12、cimens are placedin the electrodeposition tank immediately. Specimens shall be primedwithin 72 hours following the final drying operation.4.5.2.1.2 Primer shall be applied by electrodeposition to a uniform, dry filmthickness of 0.0001 to 0.0004 inch (0.003 to 0.010 mm). Primer shallhave been under a
13、gitation for not less than 4 hours prior toapplication to specimens.4.5.2.1.3 The primed specimens shall be cured in a constant temperature oven at143C 3 (290F 5) for 40 minutes 5 before assembly.4.5.2.2 Curing of Bonded Specimens:4.5.2.2.1 Specimens shall be cured at a pressure of 40 ksi 5 (276 kPa
14、 34).4.5.2.2.2 Curing temperature shall be 107 - 121C (225 - 250F) for 90 minutes 3 with a rise from ambient to 107C (225F) in 50 to 85 minutes;i.e., a rise of 1 - 1.7C (1.75 - 3F) per minute.4.5.2.2.3 Specimens shall be cooled to 66C (151F) or lower under pressure.4.5.2.2.4 Completeness of Cure: Sh
15、all be tested by saturating a 4 x 4 inch(102 x 102 mm) piece of cheesecloth with methyl ethyl ketone (MEK),flooding the area to be tested with MEK, and rubbing the test area,using considerable pressure, 200 times counting the strokes in onedirection. Exposure of any metal constitutes a noncured film
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