ImageVerifierCode 换一换
格式:PDF , 页数:7 ,大小:181.05KB ,
资源ID:419799      下载积分:5000 积分
快捷下载
登录下载
邮箱/手机:
温馨提示:
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   
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-419799.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(AECMA PREN 2904-1998 Aerospace Series Clamps - Saddle in Aluminium Alloy Dimensions - Masses Issue P 2 [Refer To ASD-STAN PREN 3730]《航空航天系列夹子螺纹驱动尺寸--鞍状铝合金尺寸--质量 P 2版》.pdf)为本站会员(cleanass300)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!

AECMA PREN 2904-1998 Aerospace Series Clamps - Saddle in Aluminium Alloy Dimensions - Masses Issue P 2 [Refer To ASD-STAN PREN 3730]《航空航天系列夹子螺纹驱动尺寸--鞍状铝合金尺寸--质量 P 2版》.pdf

1、STD-AECMA PREN 2904-ENGL L998 LOL23Ll DOL5080 TqZ I AECMA STANDARD prEN 2904 NORME AECMA Edition P 2 AECMA NORM September 1998 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - B-1200 BRUXELLES - Tel. (+32) 2 775 81 10 - Fax. (+32) 2 775 81 11 ICs: Supersedes issu

2、e P 1 Descriptors: April 1989 Replace page 1 of the previous issue by this page for aluminium and alutniniuni alloys 1) EN 2900 -Aerospace series - Clamps - Technical specification 2) EN 2905 -Aerospace series - Rubtaer cushioninys for clamps - Dimensions - Masses 2j 3 R eq u ired cli a ra c t e r i

3、 s t ic s 3.1 Material EN 2091 Top half : Bottom half : Rubber cushionitigs for clamps : EN 2905 3 2 Surface treatment EN 2437 Top fialf : Bottom half : 3.3 Configuration - Dimensions - Tolerances The corifiguratiorr sliail correspond with the figures, Dimensions shall correspond with the figures an

4、d tables. 1.l in preparation 2) Published as AECMA prestandard 3) Published as AECMA standard Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,- AECMAAPR

5、EN2404 67 W LOL23LL O004376 T r Issue P 1 prEN 2904 Page 4 F H1 L R Mass 2) 63,O 70,O 2,O 2,8 78,O 8S,O 2,8 2,8 I Figure 1 - Configuration, complete clamp Table 1 - Dimensions I DN 1) c max . 7J-G- ky/1000 pcs 5,76 -.- Tolerances I 32,O +0,4 -0 6,93 7,82 11,6 13,6 9,65 12,7 16,l 21,o 1 6485 16,4 25,

6、O 15,20 +O, 8 -0 30,O I 74,5 to- 106,O 36,5 45, o 22,50 28,SO I- Untolerenced dimensions + - 0,4 mm 1) as per IS0 2964 2) Data referring to the elastomer specific mass of 1,2 y/cm3 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot f

7、or ResaleNo reproduction or networking permitted without license from IHS-,-,-4i,o I 32 I 56,5 AECMA PREN2704 87 m LOL23LL 0004377 L m Issue P 1 prEN 29G9 Paye 5 Identification mark Figure 2 - Configuration, form “All, clamp top half Edges to be rounded - “I 9 $6 11,6 13,6 16,l 21 ,o 25,O 30,O 36,5

8、45,O - Figure 3 - Configuration, form tstj;ti, bottom half Table 2 - Dimensions I l 8,4 I 50,9 I 20 17,h I 70,O I 36 26,4 Dimensions in millimetres 3,6 1,6 20,04 3 16,30 6,20 3,6 1,6 0,04 3 20,60 7,90 Untoleranced dimensions 2 0,4 1) Data referring to the elastomer specific mass of 1,2 g/cm3 Copyrig

9、ht Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Issue P 1 prEN 2904 Page 6 Description block CLAhlP, SADDLE, TOP HALF 4 -Designation Each clamp shall only be

10、designated as in the following exainpies : I denti ty block 1 Descript ion block Identity block EN2904C201 EN2904G1 I CLAMP, SADDLE Number of EN standard C; = Code letter for material I (see EN 2905) DN = Nominal diameter (see table) A = Code letter for form (see figure 2) Form B Description block C

11、LAMP, SADDLE, STTM HALF -Identity block EN2904G; Number of EN standard I C = Code letter for material 1 DN = Nominal diameter (see table) B = Code letter for form (see figure 33 Note : if necessary the originator code 14005 may be ii-itroduced between the description block and the identity block. Co

12、pyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AECMA PREN2704 87 m 1012311 0004377 5 W, _ issue P 1 prEN 2904 Page 7 5 In addition to the manufacturers

13、own rnarlting each clamp shall be msrked in the position inclicatecl using the identity block as defined in clause 4 of tllis standard. A4arking nietliod is at the manufacturers option. h4a r I: i I ig 6 Technical specification As per EN 2900. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-

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