SAE AMS 7264A-1988 RINGS SEALING SILICONE RUBBER High Temperature Resistant Low Compression Set 65 - 75《耐高温65-75低压缩硅酮橡胶密封环》.pdf
《SAE AMS 7264A-1988 RINGS SEALING SILICONE RUBBER High Temperature Resistant Low Compression Set 65 - 75《耐高温65-75低压缩硅酮橡胶密封环》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 7264A-1988 RINGS SEALING SILICONE RUBBER High Temperature Resistant Low Compression Set 65 - 75《耐高温65-75低压缩硅酮橡胶密封环》.pdf(7页珍藏版)》请在麦多课文档分享上搜索。
1、 AEROSPACE MATERIAL SPECIFICATION RINGS, SEALING, SILICONE RUBBER High Temperature Resistant, Low Compression Set 65 - 75 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
2、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 reaffirmed, revised, or cancelled. SAE invites yo
3、ur written comments and suggestions. Copyright 2007 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, photocopying, recording, or otherwise, without the prior written
4、 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: custsvcsae.org SAE WEB ADDRESS: http:/www.sae.org AMS 7264A Issued OCT 1982 Revised APR 1988 Reaffirmed JUN 2007 Superseding AMS 7264 RATIONALE This docum
5、ent has been reaffirmed to comply with the SAE 5-year Review policy. THIS REVISION CONTAINS ONLY EDITORIAL CHANGES 1. SCOPE: 1.1 Form: This specification covers a silicone rubber in the form of molded rings. 1.2 Application: Sealing rings for use from -55 to +205 C (-65 to +400 F) in dynamic applica
6、tions and from -60 to +260 C (-80 to +500 F) in static applications. 2. APPLICABLE DOCUMENTS: The following publications form a part of this specification to the extent specified herein. The latest issue of Aerospace Material Specifications, Aerospace Standards, and Aerospace Information Reports sha
7、ll apply. The applicable issue of other documents shall be as specified in AMS 2350. 2.1 SAE Publications: Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096. AMS 7264A SAE AMS 7264A - 2 - 2.1.1 Aerospace Material Specifications: AMS 2350 Standards and Test Methods AMS 2817 Packaging a
8、nd Identification, Preformed Packings 2.1.2 Aerospace Standards: AS 568 Aerospace Size Standard for O-Rings AS 871 Manufacturing and Inspection Standards for Preformed Packings (O-Rings) 2.1.3 Aerospace Information Reports: AIR 851 O-Ring Tension Testing Calculations 2.2 ASTM Publications: Available
9、 from American Society for Testing and Materials, 1916 Race Street, Philadelphia, PA 19103. ASTM D1414 Testing Rubber O-Rings 3. TECHNICAL REQUIREMENTS: 3.1 Material: Shall be a compound, based on a silicone elastomer, suitably cured to produce sealing rings meeting the requirements of 3.2. 3.2 Prop
10、erties: Rings shall conform to the following requirements; tests shall be performed on the rings supplied in accordance with ASTM D1414, insofar as practicable. Tensile strength testing is not required on rings which are too small to permit assembly on rollers and are, after cutting, too short to pe
11、rmit testing as a single strand. Eliminating testing for tensile strength does not eliminate testing for elongation; elongation test can be made by stretching a ring over a mandrel of a size which will stretch the ring sufficiently to produce the required elongation when figured on the ID of the rin
12、g. Calculations of tensile strength and elongation may be made in accordance with AIR 851. AMS 7264A SAE AMS 7264A - 3 - 3.2.1 As Received: 3.2.1.1 Hardness, Durometer “A“ or equiv. 70 5 3.2.1.2 Tensile Strength, minimum 750 psi (5.15 MPa)3.2.1.3 Elongation, minimum 110% 3.2.1.4 Corrosion Nil 3.2.1.
13、5 Specific Gravity Preproduction Value 0.02 3.2.2 Dry Heat Resistance: Temperature: 260C 3 (500F 5)3.2.2.1 Tensile Strength Change, -20% Time: 168 hr 1.0 maximum 3.2.2.2 Elongation Change, maximum -40% 3.2.2.3 Hardness Change, Durometer “A“ or equiv. 0 to +10 3.2.3 Compression Set: Temperature: 260C
14、 3 Percent of Original Deflection, (500F 5) maximum 50 Time: 22 hr 0.25 3.2.4 Low-Temperature Resistance: Temperature Retraction TR10point, maximum -55C (-65F) 3.3 Quality: Rings, as received by purchaser, shall be uniform in quality and condition, smooth, as free from foreign material as commercial
15、ly practicable, and free from internal imperfections detrimental to their performance. Surface imperfections shall be no greater than permitted by AS 871 for minor defects. 3.4 Sizes and Tolerances: Shall be as specified on the drawing. Inspection for conformance to dimensional requirements shall be
16、 made in accordance with AS 871. AMS 7264A SAE AMS 7264A - 4 - 4. QUALITY ASSURANCE PROVISIONS: 4.1 Responsibility for Inspection: The vendor of rings shall supply all samples for vendors tests and shall be responsible for performing all required tests. Results of such tests shall be reported to the
17、 purchaser as required by 4.5. Purchaser reserves the right to sample and to perform any confirmatory testing deemed necessary to ensure that the rings conform to the requirements of this specification. 4.2 Classification of Tests: 4.2.1 Acceptance Tests: Tests to determine conformance to the follow
18、ing requirements are classified as acceptance tests and shall be performed on each lot: Requirements Paragraph Reference Hardness, as received Tensile Strength, as received Elongation, as received Specific Gravity, as received Compression Set 3.2.1.1 3.2.1.2 3.2.1.3 3.2.1.5 3.2.3 4.2.2 Periodic Test
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