SAE AMS 3970 1A-2011 Carbon Fiber Fabric Repair Prepreg 120 (250 Vacuum Curing Part 1 - General Requirements《120℃(250℉)真空固化碳纤维织物修补预浸材料 第1部分 一般要求》.pdf
《SAE AMS 3970 1A-2011 Carbon Fiber Fabric Repair Prepreg 120 (250 Vacuum Curing Part 1 - General Requirements《120℃(250℉)真空固化碳纤维织物修补预浸材料 第1部分 一般要求》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 3970 1A-2011 Carbon Fiber Fabric Repair Prepreg 120 (250 Vacuum Curing Part 1 - General Requirements《120℃(250℉)真空固化碳纤维织物修补预浸材料 第1部分 一般要求》.pdf(45页珍藏版)》请在麦多课文档分享上搜索。
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:/standards.sae.org/AMS3970/1A AEROSPACE MATERIAL SPECIFICATION AMS3970/1 REV. A Issued 1999-12 Revised 2011-04 Rea
5、ffirmed 2016-12 Superseding AMS3970/1 Carbon Fiber Fabric Repair Prepreg, 120 C (250 F) Vacuum Curing Part 1 - General Requirements RATIONALE AMS3970/1A has been reaffirmed to comply with the SAE five-year review policy. FOREWORD AMS3970/1 belongs to the Technical Specification system explained in A
6、MS3970. TABLE OF CONTENTS 1. SCOPE 4 2. APPLICABLE DOCUMENTS 4 2.1 SAE Publications . 4 2.2 ASTM Publications 4 2.3 EN Publications . 6 2.4 ISO Publications 7 2.5 SACMA Publications . 8 2.6 Military Specifications 8 2.7 PRI Publications 8 3. DEFINITIONS . 8 3.1 General . 8 3.2 Specific for Carbon Fi
7、ber Prepreg and Film Adhesive 8 4. REQUIREMENTS . 10 4.1 General Requirements: . 10 4.1.1 Qualification 10 4.1.2 Process Control Document . 10 4.1.3 Traceability 10 4.1.4 Health and Safety Requirements 10 4.1.5 Manufacturers Responsibility . 10 4.1.6 Quality Assurance . 10 4.2 Technical Requirements
8、 . 11 4.2.1 Technical Requirements for Carbon Fibers 11 4.2.2 Technical Requirements for Fabric . 11 4.2.3 Technical Requirements for Resin 13 4.2.4 Technical Requirements for Carbon and Glass Prepreg 13 4.2.5 Technical Requirements for Film Adhesive 134.2.6 Common Technical Requirements for Prepreg
9、 and Film Adhesive 144.3 Requirements for Composite Materials . 154.4 Test Methods 154.4.1 Required Number of Specimens . 164.4.2 Test Methods for Fiber 164.4.3 Test Methods for Fabric 164.4.4 Test Methods for Resin . 164.4.5 Test Methods for Composites . 165. QUALIFICATION. 175.1 Introduction . 175
10、.2 Material Qualification . 175.2.1 General . 175.2.2 Screening of the Prepreg System . 175.2.3 Qualification of Material . 175.2.4 Audit of a Manufacturer . 185.2.5 Establishment of an Appendix of PRI QPL AMS3970 185.3 Material Qualification Program 185.3.1 Qualification Retests . 185.3.2 Qualifica
11、tion Test Report. 195.4 Side Qualification and Requalification 195.5 Material Safety Data Sheet . 205.6 Evaluation of Test Data . 206. COMPOSITE TEST METHODS AND SPECIMEN MANUFACTURING 206.1 Specimen Manufacturing and Storage 206.1.1 Specimen Definition 206.1.2 Panel Size . 206.1.3 Panel Manufacturi
12、ng . 216.1.4 Tabs 216.1.5 Specimen Machining . 216.1.6 Specimen Selection 216.1.7 Storage of Panels and Specimens 216.1.8 Drying of Specimens . 216.1.9 Strain Gauge Bonding . 236.2 Fluid Immersion and Humidity Aging 236.2.1 Wet Conditioning Procedures . 236.2.2 Traveler Specimens 236.2.3 Selected Fl
13、uids 236.2.4 Fluid Immersion Procedure . 246.3 Report on Specimen Manufacturing, Conditioning and Storage 256.3.1 Panel Manufacturing . 256.3.2 Specimen Manufacturing 256.3.3 Fluid Immersion . 256.3.4 Humidity Aging 266.4 Test Procedure for Testing at Nonambient Conditions . 266.4.1 Temperature Cham
14、ber 266.4.2 Testing at Elevated Temperatures 266.4.3 Testing at Sub-Zero Temperatures . 266.5 Additions and Changes to Standard Test Methods 276.5.1 General . 276.5.2 Tensile Weft / Warp . 286.5.3 Compressive Weft / Warp . 296.5.4 Tensile In-Plane Shear (45) . 296.5.5 Interlaminar Shear Warp . 306.5
15、.6 DMA Composite 306.5.7 Tensile QI 31SAE INTERNATIONAL AMS3970/1A 2 of 45_6.5.8 Tensile QI Open-Hole . 316.5.9 Compressive QI 326.5.10 Compressive QI Open Hole 326.5.11 Double Shear Bearing QI 336.5.12 Compression After Impact 346.5.13 Flatwise Tensile 356.5.14 Long Beam Sandwich Flexure 356.5.15 T
16、ensile Tapered Joint 366.5.16 Tensile Stepped Joint 366.5.17 Tensile Single Lap Shear 366.5.18 Thick Adherent Shear . 366.5.19 Moisture Uptake 366.5.20 Fracture Toughness Energy - G1c 376.5.21 Fracture Toughness Energy - G2c 376.6 Determination of Laminate Quality 376.6.1 C-Scan 376.6.2 Void Content
17、 (Porosity) . 386.6.3 Fiber Volume . 396.7 Specimen Manufacturing 396.7.1 General . 396.7.2 Equipment . 396.7.3 Essential Expendable Materials 406.7.4 Other Expendable Materials . 406.7.5 Manufacturing of Laminates 416.7.6 Manufacturing of Sandwich Panels . 416.7.7 Manufacturing of Tapered and Stepp
18、ed Joint Specimens 436.7.8 Manufacturing of Tensile Single Lap Shear Specimens . 437. NOTES 44APPENDIX A AUTHORIZED ANCILLARY MATERIALS 45FIGURE 1 SETUP FOR LAMINATE CURING . 42FIGURE 2 SETUP FOR SANDWICH CURING 42TABLE 1 SIDE QUALIFICATION PROGRAM . 19TABLE 2 FLUID TYPES FOR IMMERSION TESTING 22TAB
19、LE 3 STORAGE CONDITIONS AND TIMES FOR LAMINATE PANELS AND LAMINATE SPECIMENS . 22TABLE 4 STORAGE CONDITIONS AND TIMES FOR SANDWICH PANELS AND SANDWICH SPECIMENS 24SAE INTERNATIONAL AMS3970/1A 3 of 45_1. SCOPE AMS3970/1 gives information about the technical requirements and qualification procedure fo
20、r carbon fiber fabric epoxy prepreg and a companion non-structural glass prepreg used for repair of carbon fiber reinforced epoxy structures. The prepreg system may include a film adhesive to be applied in a co-curing process with the prepreg for joint and sandwich bonding. The need for a film adhes
21、ive shall be established during screening tests. 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
22、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 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7
23、323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org.AMS3970 Carbon Fiber Fabric Repair Prepreg, 120 C (250 F) Vacuum Curing - Part 0 - Introduction AMS3970/2 Carbon Fiber Fabric Repair Prepreg, 120 C (250 F) Vacuum Curing - Part 2 - Qualification Program for Fiber, Fabric, Carbon
- 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:
- SAEAMS39701A2011CARBONFIBERFABRICREPAIRPREPREG120250VACUUMCURINGPART1GENERALREQUIREMENTS120 250 真空 固化

链接地址:http://www.mydoc123.com/p-1021304.html