ImageVerifierCode 换一换
格式:PDF , 页数:5 ,大小:198.86KB ,
资源ID:451391      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-451391.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(ASD-STAN PREN 2667-4-1996 Aerospace Series Non-Metallic Materials Foaming Structural Adhesive Films Test Methods Part 4 Vertical Slump (Edition P 1)《航空航天系列 非金属材料发泡结构粘合剂薄膜的试验方法 第4部分.pdf)为本站会员(bowdiet140)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!

ASD-STAN PREN 2667-4-1996 Aerospace Series Non-Metallic Materials Foaming Structural Adhesive Films Test Methods Part 4 Vertical Slump (Edition P 1)《航空航天系列 非金属材料发泡结构粘合剂薄膜的试验方法 第4部分.pdf

1、STD-AECMA PREN 2bb7-q-ENGL 399b 1032311 0032818 4T5 Edition approved for publication AECMA STANDARD NORME AECMA AECMA NORM C7 Chairman Comments should be sent within six months after the date of publication to prEN 2667-4 Edition P 1 November 1996 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE I

2、NDUSTRIES (AECMA) Gulledelle 94 - 8-1200 BRUXELLES - Tel. (32) 2 775 81 10 - Fax. (32) 2 775 81 11 ICs : Descriptors : ENGLISH VERSION Aerospace series Non-metallic materials Foaming structural adhesive films Test methods Part 4 : Vertical slump Srie arospatiale Matriaux non-mtalliques Adhsifs struc

3、turaux expansibles en film Mthodes dessai Partie 4 : Ecouiement vertical Luft- und Raumfahrt Nichtmetallische Werkstoffe Strukturelle Expansionsklebstoffe in Filmform Prfverfahren Teil 4 : Standvermgen in senkrechter Auftragslage This “Aerospace Series Prestandard has been drawn up under the respons

4、ibility of AECMA (The European Association of Aerospace Industries). It is published on green paper for the needs of AECMA-Members. It has been technically approved by the experts of the concerned Technical Committee following comment by the Member countries. Subsequent to the publication of this Pr

5、estandard, the technical content shall not be changed to an ex tent that interchangeability is affected, physically or functionall y, without re-iden tifica tion of the standard. After examination and signature of the AECMA Standard Checking Centre (NPSI and formal agreement of the Official Services

6、 of the Member countries it will be submitted as a draft European Standard to CEN (European Committee for Standardization) for formal vote. 1996-1 1-29 AECMA Gulledelle 94 6-1 200 BRUXELLES Mr Wright I I aecma 19s STD=AECMA PREN 2bb7-4-ENGL 377b 3032313 0032837 333 = Page 3 prEN 2667-4 : 1996 1 Scop

7、e This standard defines the test method for determining the extent of slump of a foaming adhesive film placed in a vertical position, after application of the specified cure cycle. 2 Normative references EN 2048 Aerospace series - L-section aluminium alloy extrusions - Dimensions 1) EN 2090 Aerospac

8、e series - Aluminium alloy 2024-T3 - Clad sheets and strips - 0,4 mrn I a I 6 rnm 1) EN 2321 Aerospace series - Aluminium alloy 2024-T3 - Bars and sections - a I 150 mm 1) EN 2334 Aerospace series - Acid chromate pickling of aluminium and aluminium alloys 1) 3 Apparatus and auxiliary equipment Air c

9、irculating oven, programmable or controllable when conducting the curing cycle, with an accuracy of f 2 oc. Micrometer, with an accuracy within 0,Ol mm. Desiccator. 4 Definition For the purposes of this standard, the following definition applies : Slump : Foaming adhesives when cured in a vertical p

10、osition may be of thicknesses appreciably different between the high and low parts. This thickness difference is called slump. 5 Principle The principle of the test is to reproduce curing in the vertical position, by bonding of the adhesive to a sheet maintained vertically by means of a reusable ang

11、le section. NOTE : This method is representative of the behaviour of foaming films, in the production of a sandwich panel including honeycomb to honeycomb and honeycomb to sheet vertical joints. 1) Published as AECMA Standard at the date of publication of this standard Previous page is blank STD*AEC

12、MA PREN 2bb7-q-ENGL 177b 1012311 0032820 053 W Page 4 prEN 2667-4 : 1996 6 Test assembly, test specimens 6.1 Test assembly The test assembly shall be prepared in conformity with figure 1. 6.1 .l Materials The backup sheet shall be made from aluminium alloy 2024-T3 in accordance with EN 2090, approxi

13、mately 1,6 mm thick. The piece of angle section shall be selected per EN 2048 - 40 mm x 40 mm x 4 mm, or machined in a bar per EN 2321, about 80 mm long. 6.1.2 Surface preparation The backup sheet before bonding shall be either degreased with an appropriate solvent in the vapour phase or pickled as

14、per EN 2334, unless otherwise specified in the material standard. A primer, if specified, shall be then applied on the backup sheet in accordance with the manufacturers instructions and the material standard. 6.1.3 Bonding The application of the foaming adhesive film and the curing shall be carried

15、out in accordance with the adhesive manufacturers instructions and the material standard. The backup sheet is temporarily clipped to the back of the reusable angle section support with a suitable clipping device and in conformity with figure 1. A sample of the adhesive film 35 mm x 60 mm shall then

16、be unrolled on the backup sheet as per figure 1, so as to avoid trapping air bubbles between the film and the backup sheet. Place the angle section/backup sheet/film unit on a flat surface coated with a suitable release agent and the assembly thus produced is placed in the air circulating oven. The

17、heat-up rate shall range from 1 OC/min to 6 OC/min and shall be monitored and recorded using a thermoelectric couple placed on the vertical flange of the angle section as per figure 1. At the end of the cure cycle, cool in a desiccator until it reaches ambient temperature. 6.2 Test specimens Remove

18、the clipping device and disassemble to obtain the test specimen as per figure 2. A minimum of three test specimens shall be made for each test. 7 Expression of results For each test specimen the thicknesses a and b are he mean of three measuremen s taken at the three points at lines A and B shown in

19、 figure 2 : a, and 6, (the line A being situated at 6 mm from the upper limit of the adhesive and B being the line of maximum thickness of the foamed adhesive after curing). All the thicknesses shall be expressed in millimetres. STD-AECMA PREN 2bb7-Y-ENGL 399b W 1UL23Ll 0032823 T9T M Page 5 prEN 266

20、7-4 : 1996 Calculate the slump for each test specimen as follows : S = b-a Calculate the average slump for the series of test specimens. 8 Designation EXAMPLE : Number of this standard 9 Test report It shall include the following : - reference to this standard ; - complete identification of the foam

21、ing adhesive and primer if any, including the type, name and address of the manufacturer, date of manufacture, batch number and material standard number ; - storage conditions of the foaming adhesive before curing (temperature, humidity) ; - information on the surface preparation of the backup sheet

22、 before bonding ; - processing and curing conditions (equipment, heat-up rate, curing temperature, duration and record of temperature) ; - number of test specimens ; - individual test results (thickness and Slump) ; - information on each test specimen : result S of the slump test ; - average slump o

23、f the series of test specimens ; - any deviation from this standard in detail ; - date of test and signature. STD-AECMA PREN 2bb7-4-ENGL L79b 9 LOL23LL 0032822 72b H Page 6 prEN 2667-4 : 1996 Dimensions in millimetres Backup sheet Thermoelectric couple I 60 Figure 1 : Test assembly before curing I I 6 rnm from top edge b, = max. thickness Figure 2 : Thickness measurement on test specimen

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