SAE AMS 3894E-1990 Carbon Fiber Tape and Sheet Epoxy Resin Impregnated《环氧树脂浸渍的碳纤维带和薄板》.pdf
《SAE AMS 3894E-1990 Carbon Fiber Tape and Sheet Epoxy Resin Impregnated《环氧树脂浸渍的碳纤维带和薄板》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 3894E-1990 Carbon Fiber Tape and Sheet Epoxy Resin Impregnated《环氧树脂浸渍的碳纤维带和薄板》.pdf(14页珍藏版)》请在麦多课文档分享上搜索。
1、 AEROSPACE MATERIAL SPECIFICATION Carbon Fiber Tape and Sheet Epoxy Resin Impregnated 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
2、 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 your written comments and suggestions.
3、 Copyright 2005 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 permission of SAE. TO PLACE A DOCUM
4、ENT 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 3894EIssued NOV 1972 Revised JAN 1990 Superseding AMS 3894D 1. SCOPE:1.1 Form: This specification and its supplementary detail specifica
5、tions covertape and sheet fabricated using carbon fibers impregnated with epoxy resin.1.2 Application: Primarily for fabricating high-strength and high-moduluscomposite parts, using either hand-layup or a machine for automated-tape-layup.Classification: The tapes and sheets shall be as specified in
6、theapplicable detail specifications, wherein each product is defined byproperty characteristics and continuous service temperature. An example isshown in 8.2. The product covered by each detail specification appears aspart of the title.Safety - Hazardous Materials: While the materials, methods, appl
7、ications,and processes described or referenced in this specification may involve theuse of hazardous materials, this specification does not address the hazardswhich may be involved in such use. It is the sole responsibility of theuser to ensure familiarity with the safe and proper use of any hazardo
8、usmaterials and to take necessary precautionary measures to ensure the healthand safety of all personnel involved.1.31.4Reaffirmed JUN 2005 Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE - 2 - A
9、MS 3894E AMS 36894E2. APPLICABLE DOCUMENTS: The following publications form a part of thisspecification to the extent specified herein. The latest issue of SAEpublications shall apply. The applicable issue of other publications shallbe as specified in AMS 2350.2.1 SAE Publications: Available from SA
10、E, 400 Commonwealth Drive, Warrendale,PA 15096.2.1.1 Aerospace Material Specifications:AMS 2350 - Standards and Test MethodsAMS 2825 - Material Safety Data SheetsAMS 3892 - Fibers, Carbon, Tow and Yarn, for Structural Composites- Interleaf Carrier Material, Composite Tape2.2 ASTM Publications: Avail
11、able from ASTM, 1916 Race Street, Philadelphia, PA19103.- Specific Gravity (Relative Density) and Density ofPlastics by DisplacementASTM D 1505 - Density of Plastics by the Density-Gradient TechniqueASTM D 2344 - Apparent Interlaminar Shear Strength of Parallel FiberComposites by Short Beam MethodAS
12、TM D 2734 - Void Content of Reinforced PlasticsTensile Properties of Fiber-Resin Composites- Fiber Content of Resin-Matrix Composites by MatrixDigestionASTM D 3410 - Compressive Properties of Unidirectional or Crossply Fiber-Resin CompositesASTM D 3529 - Resin Solids Content of Carbon Fiber-Epoxy Pr
13、epregVolatiles Content of Carbon Fiber-Epoxy PrepregASTM D 3531 - Resin Flow of Carbon Fiber-Epoxy PrepregASTM D 3532 - Gel Time of Carbon Fiber-Epoxy PrepregU.S. Government Publications: Available from Commanding Officer, NavalPublications and Forms Center, 5801 Tabor Avenue, Philadelphia, PA 19120
14、.2.3.1 Military Standards:MIL-STD-794 - Parts and Equipment, Procedures for Packaging and Packing of2.4 AIA Publications: Available from National Standards Association, Inc.,1321 14th Street, N.W., Washington, DC 20005.NAS 992 - Reel, Composite Filament Tape, Automated Machine LayupAMS 3898ASTM D 79
15、2ASTM D 3171ASTM D 3039-ASTM D 3530-2.3Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE - 3 - AMS 3894E AMS 36894E3. TECHNICAL REQUIREMENTS:3.1 Detail Specifications: The requirements for a specif
16、ic product shallconsist of all the requirements specified herein in addition to requirementsspecified in the applicable detail specification. In case of conflictbetween requirements of this basic specification and an applicable detailspecification, requirements of the detail specification shall gove
17、rn.3.2 Material:3.2.1 Construction: The product shall consist of parallel, unidirectionalcarbon fibers meeting the requirements of AMS 3892 and its applicabledetail specification, impregnated with an epoxy resin meeting therequirements of the applicable detail specification, and arranged in asingle
18、in-plane layer.3.2.2 Ends: The product shall contain no unspliced yarn or tow ends. Splicesin the same yarn or tow shall be not less than 10 feet (3 m) apart.Splices in adjacent yarns or tows shall be not less than 12 inches(305 mm) apart.3.2.3 Storage Life: The product, when packaged in water resis
19、tant, heat-sealedbags, shall meet the requirements of the applicable detail specificationafter storage at standard conditions as specified therein.3.2.4 Working Life: The product shall meet the requirements of the applicabledetail specification after exposure for a continuous period at therelative h
20、umidity and temperature specified therein.3.2.5 Bending: The product shall withstand, without visible material damage,bending through an angle of 180 degrees around a 1.0 inch (25 mm) diametermandrel with the fiber direction perpendicular to the axis of bend; 10Xmagnification shall be used in examin
21、ation for damage.3.3 Properties of Uncured Impregnated Material: The as-received product shallconform to the requirements of this specification and the applicable detailspecification, determined on the product as-supplied in accordance with testprocedures specified herein.3.4 Properties of Cured Lam
22、inate: Test laminates shall conform to therequirements of this specification and the applicable detail specification,determined on specimens cut from laminates prepared in accordance with 4.5.3.5 Quality: The product, as received by purchaser, shall be uniform in qualityand condition, free from fore
23、ign material and, except as specified in 3.5.1,free from imperfections detrimental to usage of the product.Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE - 4 - AMS 3894E AMS 36894E3.5.1 Visual I
24、mperfection Criteria: Visible indications of dry spots, voids,crimps, crossed or broken fibers, twisted fibers, irregular carrier,over-impregnation or incomplete impregnation areas are not acceptable ifthe total length of each area exceeds limits indicated below for the totaltape length of the roll:
- 1.请仔细阅读文档,确保文档完整性,对于不预览、不比对内容而直接下载带来的问题本站不予受理。
- 2.下载的文档,不会出现我们的网址水印。
- 3、该文档所得收入(下载+内容+预览)归上传者、原创作者;如果您是本文档原作者,请点此认领!既往收益都归您。
下载文档到电脑,查找使用更方便
10000 积分 0人已下载
下载 | 加入VIP,交流精品资源 |
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- SAEAMS3894E1990CARBONFIBERTAPEANDSHEETEPOXYRESINIMPREGNATED 环氧树脂 浸渍 碳纤维 薄板 PDF

链接地址:http://www.mydoc123.com/p-1021235.html