ImageVerifierCode 换一换
格式:PDF , 页数:45 ,大小:407.20KB ,
资源ID:1021304      下载积分:10000 积分
快捷下载
登录下载
邮箱/手机:
温馨提示:
如需开发票,请勿充值!快捷下载时,用户名和密码都是您填写的邮箱或者手机号,方便查询和重复下载(系统自动生成)。
如填写123,账号就是123,密码也是123。
特别说明:
请自助下载,系统不会自动发送文件的哦; 如果您已付费,想二次下载,请登录后访问:我的下载记录
支付方式: 支付宝扫码支付 微信扫码支付   
注意:如需开发票,请勿充值!
验证码:   换一换

加入VIP,免费下载
 

温馨提示:由于个人手机设置不同,如果发现不能下载,请复制以下地址【http://www.mydoc123.com/d-1021304.html】到电脑端继续下载(重复下载不扣费)。

已注册用户请登录:
账号:
密码:
验证码:   换一换
  忘记密码?
三方登录: 微信登录  

下载须知

1: 本站所有资源如无特殊说明,都需要本地电脑安装OFFICE2007和PDF阅读器。
2: 试题试卷类文档,如果标题没有明确说明有答案则都视为没有答案,请知晓。
3: 文件的所有权益归上传用户所有。
4. 未经权益所有人同意不得将文件中的内容挪作商业或盈利用途。
5. 本站仅提供交流平台,并不能对任何下载内容负责。
6. 下载文件中如有侵权或不适当内容,请与我们联系,我们立即纠正。
7. 本站不保证下载资源的准确性、安全性和完整性, 同时也不承担用户因使用这些下载资源对自己和他人造成任何形式的伤害或损失。

版权提示 | 免责声明

本文(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)为本站会员(fuellot230)主动上传,麦多课文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文库(发送邮件至master@mydoc123.com或直接QQ联系客服),我们立即给予删除!

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

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

24、Prepreg, Film Adhesive and Non-Structural Glass Prepreg AMS3970/3 Carbon Fiber Fabric Repair Prepreg, 120 C (250 F) Vacuum Curing - Part 3 - Purchasing Specification for Carbon Prepreg AMS3970/4 Carbon Fiber Fabric Repair Prepreg, 120 C (250 F) Vacuum Curing - Part 4 - Purchasing Specification for F

25、ilm Adhesive AMS3970/5 Carbon Fiber Fabric Repair Prepreg, 120 C (250 F) Vacuum Curing - Part 5 - Purchasing Specification for Companion Non-Structural Glass Fiber Fabric Prepreg AMS3970/6 Carbon Fiber Fabric Repair Prepreg, 120 C (250 F) Vacuum Curing - Part 6 - Carbon Fiber Fabric Reinforced Epoxy

26、 Prepreg for Repair, Plain Weave, 193 gm/m2, Adhesive Film for Repair, Non-Structural Glass Fiber fabric Reinforced Epoxy Prepreg, 105 gm/m2AMS-C-9084 Cloth, Glass, Finished, For Resin Laminates AIR4844 Composites and Metal Bonding Glossary ARP4916 Masking and Cleaning of Epoxy and Polyester Matrix

27、Thermosetting Composite Materials 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org.ASTM C 297 Standard Test Method for Flatwise Tensile Strength of Sandwich Constructions ASTM C 393 Standa

28、rd Test Method for Flexural Properties of Sandwich Constructions ASTM D 740 Standard Specification for Methyl Ethyl Ketone ASTM D 1002 Standard Test Method for Apparent Strength of Single-Lap-Joint Adhesively Bonded Metal Specimens by Tension Loading (Metal-to-Metal) ASTM D 1655 Standard Specificati

29、on for Aviation Turbine Fuels SAE INTERNATIONAL AMS3970/1A 4 of 45_ASTM D 2344/D 2344M Standard Test Method for Short-Beam Strength of Polymer Matrix Composite Materials and Their Laminates ASTM D 3039/D 3039M Standard Test Method for Tensile Properties of Polymer Matrix Composite Materials ASTM D 3

30、171 Standard Test Methods for Constituient Content of Composite Materials ASTM D 3518/D 3518M Standard Practice for In-Plane Shear Response of Polymer Matrix Composite Materials by Tensile Test of a 45 Laminate ASTM D 3529/D 3529M Standard Test Method for Matrix Solids Content and Matrix Content of

31、Composite Prepreg ASTM D 3530/D 3530M Standard Test Method for Volitile Content of Composite Material Prepreg ASTM D 3531/D 3531M Standard Test Method for Resin Flow of Carbon Fiber-Epoxy Prepreg ASTM D 3532 Standard Test Method for Gel Time of Carbon Fiber-Epoxy Prepreg ASTM D 3776 Standard Test Me

32、thod for Mass per Unit Area (Weight) of Fabric ASTM D 3990 Standard Terminology Relating to Fabric Defects ASTM D 4440 Standard Practice for Rheological Measurement of Polymer Melts Using Dynamic Mechanical Procedures ASTM D 5229/D 5229M Standard Test Method for Moisture Absorption Properties and Eq

33、uilibrium Conditioning of Polymer Matrix Composite Materials ASTM D 5528/D 5528M Standard Test Method for Mode I Interlaminar Fracture Toughness of Unidirectional Fiber-Reinforced Polymer Matrix Composites ASTM D 5656 Standard Test Method for Thick-Adherend Metal Lap-Shear Joints for Determination o

34、f Stress-Strain Behavior of Adhesives in Shear by Tension Loading ASTM D 5766/D 5766M Standard Test Method for Open Hole Tensile Strength of Polymer Matrix Composite Laminates ASTM D 5961/D 5961M Standard Test Method for Bearing Response of Polymer Matrix Composite Laminates ASTM D 6484/D 6484M Stan

35、dard Test Method for Open Hole Compressive Strength of Polymer Matrix Composite Laminates ASTM D 7137/D 7137M Standard Test Method for Compressive Residual Strength Properties of Damaged Polymer Matrix Composite Plates ASTM E 4 Standard Practices for Force Verification of Testing Machines. ASTM E 12

36、52 Standard Practice for General Techniques for Qualitative Infrared Analysis ASTM E 1640 Standard Test Method for Assignment of the Glass Transition Temperature By Dynamic Mechanical Analysis SAE INTERNATIONAL AMS3970/1A 5 of 45_2.3 EN Publications Available from CEN-comite, European de Normalisati

37、on, Secretatiat Central, Rue de Stassart 36, B-1050 Bruxelles, Belgium or www.cenorm.be.EN 2243-7 Aerospace Series: Structural Adhesives Test Methods. Part 7: Determination of the Flow Characteristics of a Film Adhesive EN 2329 Aerospace Series: Textile Glass Fibre Preimpregnates, Test Method for th

38、e Determination of Mass per Unit Area EN 2330 Aerospace Series: Textile Glass Fibre Preimpregnates, Test Method for the Determination of the Content of Volatile Matter EN 2331 Aerospace Series: Textile Glass Fibre Preimpregnates, Test Method for the Determination of the Resin and Fibre Content and t

39、he Mass of Fibre per Unit Area EN 2379 Aerospace Series: Test Fluids for Non Metallic Materials EN 2489 Aerospace Series: Fiber Reinforced Plastics - Determination of the Action of Liquid Chemicals EN 2557 Aerospace Series: Carbon Fibre Preimpregnates, Test Method for the Determination of Mass per U

40、nit AreaEN 2558 Aerospace Series: Carbon Fibre Preimpregnates, Test Method for the Determination of the Percentage of Volatile Matter EN 2559 Aerospace Series: Carbon Fibre Preimpregnates, Test Method for the Determination of the Resin and Fibre Content and the Mass of Fibre per Unit Area EN 2560 Ae

41、rospace Series: Carbon Fibre Preimpregnates, Test Method for the Determination of the Resin Flow EN 2561 Aerospace Series: Unidirectional Laminates - Carbon Thermosetting Resin, Tensile Test Parallel to the Fiber Direction EN 2563 Aerospace Series: Carbon Fibre Reinforced Plastics - Unidirectional L

42、aminates - Determination of Apparent Interlaminar Shear Strength EN 2564 Aerospace Series: Carbon Fiber Laminates - Test Method for the Determination of the Fiber and Resin Fraction and Porosity Content EN 2565 Aerospace Series: Preparation of Carbon Fiber Reinforced Resin Panels for Test Purposes E

43、N 2823 Aerospace Series: Fiber Reinforced Plastic, Test Method for the Determination of the Effect of Exposure to Humid Atmospheres on Physical and Mechanical Characteristics EN 2850 Aerospace Series: Fiber Reinforced Plastics, Testing Unidirectional Laminates and Woven Fabric Laminates - Compressio

44、n Test EN 3003 Aerospace Series: Test Method - Determination of Mass per Unit Area of Film Adhesives EN 3615 Aerospace Series: Fiber Reinforced Plastics, Procedure for the Determination of the Conditions of Exposure to Humid Atmosphere and the Determination of Moisture Absorption EN 6031 Aerospace S

45、eries: Fiber Reinforced Plastic, Determination of In-Plane Shear Properties (45 Tensile Test)SAE INTERNATIONAL AMS3970/1A 6 of 45_EN 6032 Aerospace Series: Determination of Glass Transition Temperature (DMA). EN 6033 Aerospace Series: Carbon Fiber Reinforced Plastics, Determination of the Interlamin

46、ar Fracture Toughness Energy - Mode I - G1c Test EN 6034 Aerospace Series: Carbon Fiber Reinforced Plastics, Determination of the Interlaminar Fracture Toughness Energy - Mode II - G2c Test EN 6035 Aerospace Series: Fiber Reinforced Plastics, Determination of Notched and Unnotched Tensile Strength E

47、N 6036 Aerospace Series: Fiber Reinforced Plastics, Test Method, Determination of Notched, Unnotched and Filled Hole Compression Strength EN 6037 Aerospace Series: Fiber Reinforced Plastics - Test Method - Determination of Bearing Strength EN 6038 Aerospace Series: Fiber Reinforced Plastic, Determination of Compression Strength After Impact EN 6040 Aerospace Series: Analysis of Non-Metallic Materials (Uncured) by High Performance Liquid Chromatography (HPLC) EN 6041 Aerospace Series: Analysis of Non-Metallic Materials (Uncured) by Dif

copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
备案/许可证编号:苏ICP备17064731号-1