ImageVerifierCode 换一换
格式:PDF , 页数:9 ,大小:66.09KB ,
资源ID:453686      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-453686.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 6069-2008 Aerospace series Rivet 100 Degrees reduced flush head close tolerance Inch series (Edition P 3)《航空航天系列 紧公差100°小埋头铆钉 英制系列 第P3版》.pdf)为本站会员(livefirmly316)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 6069-2008 Aerospace series Rivet 100 Degrees reduced flush head close tolerance Inch series (Edition P 3)《航空航天系列 紧公差100°小埋头铆钉 英制系列 第P3版》.pdf

1、ASD STANDARD NORME ASD ASD NORM prEN 6069 Edition P 3 September 2008 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATIONAvenue de Tervuren, 270 - B-1150 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 763 3565 - www.asd-stan.orgICS: Supersedes Edition P 2 November

2、 2005 Descriptors: ENGLISH VERSION Aerospace series Rivet, 100 reduced flush head, close tolerance Inch series Srie arospatiale Rivets de prcision, 100 tte fraise petite Srie en inches Luft- und Raumfahrt Vollniet, 100 reduzierter Senkkopf, enge Toleranz Zoll-Reihe This “Aerospace Series“ Prestandar

3、d has been drawn up under the responsibility of ASD-STAN (The AeroSpace and Defence Industries Association of Europe - Standardization). It is published for the needs of the European Aerospace Industry. It has been technically approved by the experts of the concerned Domain following member comments

4、. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, without re-identification of the standard. After examination and review by users and formal agreement of ASD-STAN, it will be

5、submitted as a draft European Standard (prEN) to CEN (European Committee for Standardization) for formal vote and transformation to full European Standard (EN). The CEN national members have then to implement the EN at national level by giving the EN the status of a national standard and by withdraw

6、ing any national standards conflicting with the EN. Edition approved for publication 30 September 2008 Comments should be sent within six months after the date of publication to ASD-STAN Mechanical Domain Copyright 2008 by ASD-STAN prEN 6069:20082 Contents Page Foreword2 1 Scope 3 2 Normative refere

7、nces3 3 Requirements.4 3.1 Configuration, dimensions, tolerances and mass .4 3.2 Material and surface treatment.7 4 Designation 7 5 Marking .8 5.1 Material identification8 5.2 Manufacturers identification.8 5.3 Identification of oversize rivets9 6 Technical specification .9 6.1 Aluminium alloy rivet

8、s 9 6.2 Heat resisting alloy NI-PD9001 (NiCu31) rivets 9 6.3 Titanium alloy rivets 9 Foreword This standard was reviewed by the Domain Technical Coordinator of ASD-STANs Mechanical Domain. After inquiries and votes carried out in accordance with the rules of ASD-STAN defined in ASD-STANs General Pro

9、cess Manual, this standard has received approval for Publication. prEN 6069:20083 1 Scope This standard specifies the dimensions, tolerances and mass of rivets with 100 reduced flush head, close tolerance, inch series, for aerospace application. 2 Normative references The following referenced docume

10、nts are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. ISO 8080, Aerospace Anodic treatment of titanium and titanium alloys Sulfuric ac

11、id process. 1)EN 2115, Aerospace series Aluminium alloy 2117-T42 Wire for solid rivets D 10 mm. 2)EN 2116, Aerospace series Aluminium alloy 2017A-T42 Wire for solid rivets D 10 mm. 2)EN 2117, Aerospace series Aluminium alloy AL-P5056A (5056A)-H32 Wire for solid rivets D 10 mm. 2)EN 2424, Aerospace s

12、eries Marking of aerospace products. EN 2941, Aerospace series Nickel alloy rivets Technical specification. EN 3115, Aerospace series Aluminium alloy 7050- T73 Wire for solid rivets D 10mm. 2)EN 4372, Aerospace series Heat resisting nickel alloy with copper NI-PD9001 (NiCu31) Wire for solid rivets D

13、 10 mm. 2)EN 6104, Aerospace series Rivets, solid, in aluminium or aluminium alloy Inch series Technical specification. 2)EN 6118, Aerospace series Process specification Aluminium base protection for fasteners. 2)AMS 4982, Titanium alloy wire 44.5 Cb. 3)MIL-C-5541, Military specification, Chemical c

14、onversion coatings on aluminium and aluminium alloys. 3)MIL-A-8625, Military specification, Anodic coatings for aluminum and aluminum alloys. 3)NASM5674, Rivets, structural, aluminium alloy, titanium columbium alloy, general specification for. 4)NAS9800, Head protrusion gaging, 100 flush head fasten

15、ers, gage block, gage diameters and stylus. 4) 1) Published by: International Organisation for Standardization, Case postal 56, CH-1211 Geneva 20 (www.iso.org). 2) Published as ASD Prestandard at the date of publication of this standard. 3) Published by: Society of Automotive Engineers (SAE), 400 Co

16、mmonwealth Drive, Warrendale, PA 15096-0001 (www.sae.org). 4) Published by: Aerospace Industries Association, 1000 Wilson Boulevard, Suite 1700, Arlington, VA 22209-3928, USA (www.aia-aerospace.org). prEN 6069:20084 3 Requirements 3.1 Configuration, dimensions, tolerances and mass The configuration

17、shall conform with Figure 1. The dimensions, tolerances and mass shall conform with Figure 1 and Tables 1 and 3. Dimensions and tolerances of oversizes (for repair purposes only) shall conform with Figure 1 and Tables 2 and 3. Dimensions and tolerances are expressed in millimetres. Marking ( see 5 )

18、 D1)AS2)2) F A3)10030EC WPB3)L 0,254Head-cocking angelrelative to axisof rivet 1/2 max. 0,254 max. rad. 0,127 A A1R14)Key 1 Angular misalignment of rivet head to rivet shank axis 0,5 max. 2 Marking (see Clause 5) a0,025 mm shank diameter increase is permissible within 2,54 mm of the based of the hea

19、d. bChamfered ends with radius to the R1dimensions or a 20 chamfer to dimension “S”. cMaximum head diameters are to theoretical sharp corners as measured by projection. dMeasurement method for inspection of head characteristics in accordance with NAS9800. Figure 1 Configuration 0,051a b c d 2 1 R1b

20、c 100 0,5 0,254 max. rad. prEN 6069:20085 Table 1 Dimensions and tolerances Diameter code D Nominal diameter A A1B C E F P R1S W 0,03 max. min. min. Ref. + 0,050 0,13 max. min. 0,25 0,25 max. min. 3 2,38 3,709 3,623 3,263 0,54 2,31 0,291 0,248 0,74 0,58 3,028 3,0234 3,18 4,923 4,835 4,475 0,71 3,53

21、0,336 0,291 0,99 0,79 4,135 4,1305 3,97 6,226 6,141 5,781 0,93 0,084,83 0,457 0,412 1,24 0,99 5,151 5,1466 4,76 7,635 7,543 7,183 1,19 5,15 0,610 0,559 1,50 1,19 6,200 6,1957 5,56 8,880 8,790 8,430 1,38 7,00 0,670 0,612 1,75 1,37 7,310 7,3058 6,36 10,014 9,907 9,547 1,51 0,100,08to 0,15 8,15 0,677 0

22、,618 1,98 1,57 8,420 8,415Table 2 Dimensions and tolerances for oversize rivets D A A1B C E F P R1S W Diameter code 0,03 max. min. min. Ref. + 0,050 0,13 max. min. 0,25 0,25 max. min. 5X 4,37 6,630 6,540 6,18 0,93 0,08 5,10 0,628 0,578 1,24 0,99 5,151 5,1466X 5,16 8,040 7,950 7,59 1,19 6,25 0,781 0,

23、728 1,50 1,19 6,200 6,1957X 5,96 9,280 9,190 8,83 1,38 0,100,08to 0,15 7,25 0,836 0,782 1,75 1,37 7,310 7,305prEN 6069:20086 Table 3 Length code and mass Diameter code Lengtha,b3 4 5 6 7 8 codeL 0,254 Mass c kg/ 1 000 parts 03 4,76 0,06 0,11 04 6,35 0,08 0,15 0,24 05 7,94 0,10 0,18 0,29 0,43 06 9,52

24、 0,12 0,22 0,35 0,51 0,71 07 11,11 0,14 0,25 0,40 0,59 0,81 1,07 08 12,70 0,16 0,29 0,46 0,67 0,92 1,21 09 14,29 0,18 0,32 0,51 0,75 1,03 1,35 10 15,87 0,20 0,36 0,57 0,83 1,14 1,49 11 17,46 0,22 0,40 0,62 0,90 1,24 1,63 12 19,05 0,24 0,43 0,68 0,98 1,35 1,77 13 20,64 0,26 0,47 0,73 1,06 1,46 1,91 1

25、4 22,22 0,28 0,50 0,79 1,14 1,57 2,05 15 23,81 0,30 0,54 0,84 1,22 1,67 2,19 16 25,40 0,32 0,57 0,90 1,30 1,78 2,34 17 26,99 0,61 0,95 1,38 1,89 2,48 18 28,57 0,64 1,01 1,46 2,00 2,62 20 31,75 0,71 1,11 1,61 2,21 2,90 22 34,92 0,78 1,22 1,77 2,43 3,18 24 38,10 0,85 1,33 1,93 2,64 3,46 28 44,45 1,55

26、2,24 3,07 4,02 32 50,80 1,77 2,56 3,50 4,59 40 63,50 4,36 5,71 aLength missing in table can be created in 1/16 inch (1,59 mm) steps, e.g. length code 19 corresponds to: 19/16 inch (30,16 mm). b1/32 inch (0,79 mm) length increments may be obtained by adding code 5 after the last digit of part number,

27、 e.g. length code 06-5 corresponds to: 6/16 inch (9,53 mm) + 1/32 inch (0,79 mm) = 13/32 inch (10,32 mm). cMass based on aluminium alloy with a density of 2,79 kg/dm3, refer to Table 4 for conversion factors. prEN 6069:2008 7 3.2 Material and surface treatment See Table 4. Table 4 Material code Diam

28、eter code Material code 3 4 5 5X 6 6X 7 7X 8 Surface treatment (code see Clause 4) Density kg/dm3Multiplicatorof mass (see Table 3) AD Aluminium alloy 2117-T4 per EN 2115 2,75 0,98 D Aluminium alloy 2017A-T4 per EN 2116 2,79 1 B a Aluminium alloy AL-P5056A (5056A)-H32 per EN 2117 2,64 0,95 KE Alumin

29、ium alloy 7050-T73 per EN 3115 Yellow chromated per MIL-C-5541, class 1A Anodized per MIL-A-8625, type II, class 1, clear a 2,82 1,01 N Heat resisting nickel alloy NI-PD9001 (NiCu31) per EN 4372, annealed None 8,85 3,17 T Anodized per ISO 8080 V Titanium alloy 44.5 Cb, heat treat: annealed per AMS 4

30、982 IVD per EN 6118 5,8 2,08 aNot for new design. 4 Designation EXAMPLE Description block RIVET Identity block EN6069D6X6A5 Number of this standard Material code (see Table 4) Diameter code (see Tables 1 and 2) Length code in 1/16 inch* (see Table 3). When the diameter code has no letter add between

31、 diameter code and length code a dash ”-“. Surface treatment for Al alloy (see Table 4): - No code indicates yellow chromated, - Code “A“ indicates anodised (not for new design) Additional length code (see Table 3) (1/16 of an inch plus 1/32 inch)*. When surface treatment has no letter code add betw

32、een length code and additional length code a dash ”-“. *For supplying purpose only, see footnotes aand bin Table 3. prEN 6069:20088 5 Marking 5.1 Material identification Symbol on head, see Figure 2. EN 2115 EN 2116 EN 2117 Indented 0,2 mm max Embossed 0,2 mm max Embossed 0,2 mm max EN 3115 EN 4372

33、AMS 4982 Embossed 0,2 mm max Embossed 0,2 mm max Indented 0,25 mm max Figure 2 Material identification 5.2 Manufacturers identification EN 2424, style F to be embossed or indented on rivet head. Manufacturers identification is required on rivet heads for diameter code 4 and larger. 0,8 max 0,8 max 0

34、,8 max 0,8 max 1,020 min 1,780 max 0,762 min 1,270 max0,8 max prEN 6069:2008 9 5.3 Identification of oversize rivets Symbol on rivet shank end, see Figure 3. Triangular shape indented 0,2 mm max. Figure 3 Identification of oversize rivets (the criteria being legibility) 6 Technical specification 6.1

35、 Aluminium alloy rivets Aluminium alloy rivets shall conform with the requirements of EN 6104. 6.2 Heat resisting alloy NI-PD9001 (NiCu31) rivets NI-PD9001 (NiCu31) rivets shall conform with the requirements of EN 2941. Shear strength Rc= 340 MPa to 407 MPa. Note Rivets manufactured prior to August 1st2005 with a maximum shear strength of 450 MPa may be procured and used until stocks are depleted. 6.3 Titanium alloy rivets Titanium alloy 44.5 Cb rivets shall conform with the requirements of NASM5674 except for the finish as stated. 0,8 mm max max 0,5 D

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