ImageVerifierCode 换一换
格式:PDF , 页数:9 ,大小:278.48KB ,
资源ID:421695      下载积分:5000 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-421695.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 6067-2000 Aerospace Series Pin Quick Release Self-Retaining Positive Locking Double Acting Button Handle Edition P 2《航空航天系列.栓快速释放自我保护阳极锁双钮扣手柄.P2版》.pdf)为本站会员(sofeeling205)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 6067-2000 Aerospace Series Pin Quick Release Self-Retaining Positive Locking Double Acting Button Handle Edition P 2《航空航天系列.栓快速释放自我保护阳极锁双钮扣手柄.P2版》.pdf

1、- - - AECMA STANDARD prEN 6067 NORME AECMA Edition P 2 AECMA NORM October 2000 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - 6-1200 BRUXELLES - Tel. (+32) 2 775 81 10 - Fax. (+32) 2 775 81 11 - Nota - Extra copies can be supplied by E.N.A.E. - Technopolis 54 -

2、 199. rue Jean-Jacques Rousseau - 92138 ISSY-LEC-MOULINEAUX CEDEX I I ICs: Descriptors: 2000-40-31 ENGLISH VERSION AECMA Mr Lck Gulledelle 94 8-1200 BRUXELLES Aerospace series Pin, quick release, self-retaining, Positive locking, double acting, Button handle Supersedes edition P 1 August 1998 Srie a

3、rospatiale Broche, dclenchement rapide, imperdable, verrouillage double action, Poigne bouton poussoir Luft- und Raumfahrt Kugelsperrbolren, selbstsichernd, doppeltwirkend, Druckknopfbettigung This %emspace Series“ Prestandard has been drawn up under the responsibility of AECMA (The European Associa

4、tion 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 Prestandard, the technical content shal

5、l not be changed to an extent that inferchangeability is affected, physically or functionally, without re-identification of the standard. After examination and signature of the AECMA Standard Checking Centre (NPS) and formal agreement of the OfEcial Services of the Member countries it will be submit

6、ted as a draft European Standard to CEN (European Committee for Standardization) for formal vote. AIBfF3 Chairman I Edition approved for publication 1 Comments should be sent within six months after the date of Dublication to Copyright Association Europeene des Constructeurs de Materiel Aerospatial

7、Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD-AECMA PREN bOb7-ENGL 2000 = 303233L 0038773 732 Page 2 prEN 6067: 2000 Contents list Scope Normative references . . 3 Required characteristics 3 Designation . 8 Marking 9 Te

8、chnical specification 9 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-,-,-STD.AECMA PREN bOb7-ENGL 2000 S LOL23Ll 001877Li b57 = Page 3 prEN 6067: 2000 I

9、 Scope This standard specifies the dimensions, tolerances and the required characteristics of a quick release, self retaining, positive locking, double acting pin with button handle for aerospace application. 2 Normative references This European Standard incorporates by dated or undated reference pr

10、ovisions from other publications. These normative references are at the appropriate places in the text and the publications are listed hereafter. For dated references, subsequent amendments to or revisions of any of these publications apply to this European Standard only when incorporated in it by a

11、mendment or revision. For undated references the latest edition of the publication referred to applies. EN 2424 AMS 5678 AMS-QQ-S-763 AMS-S-6758 AMS-T-6736 ASTM A 108 ASTM A 228 ASTM A 240 ASTM A 31 3 ASTM A 967 MIL- P-23460 QQ-P-416 Aerospace series - Marking of aerospace products Steel, corrosion

12、resistant, wire 17CR-7.1 NI-1 .lAL , cold drawn, precipitation-hardenable, (UNS S 177000) 1) Steel bars, wire, shapes, and forgings, corrosion resistant 1) Steel, chrome-molybdenum (41 30) bars and reforging stock (Aircraft Quality) 1) Tubing, chrome-molybdenum (4130 or 8630) steel, seamless and wel

13、ded 1) Standard specification for steel bars, carbon, cold finished, standard quality 2) Standard specification for steel wire, music spring quality 21 Standard specification for heat-resisting chromium and chromium-nickel stainless steel plate, sheet, and strip for pressure vessels 2) Standard spec

14、ification for stainless steel spring wire 2) Standard specification for chemical passivation treatments for stainless steel parts 2) Pin, quick-release, self-retaining, positive-locking 3) Plating, cadmium (electrodeposited) 3) 3 Required characteristics 3.1 Configuration, dimensions, tolerances See

15、 figure 1 and tables I, 2 and 3. Dimensions and tolerances are expressed in inches (millimetres) i) Published by: Society of Automotive Engineers (CAE), 400 Commonwealth drive, Warrendale, PA 15096 - 0001. 2) Published by: American Society for Testing and Materials. (ASTM), 100 Barr Harbor Dr., West

16、 Conshohocken, 3) Published by: Department Of Defense (DOD) the Pentagon, Washington DC 20301. PA I 9428-2959 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from I

17、HS-,-,-STDeAECMA PREN bOb7-ENGL 2GOo 3012311 0038975 595 Page 4 prEN 6067: 2000 ,soa 1 Code L + 0.020 O + yo8 3 Table 2 : Grip length Grip length Code I L Grip length Code I L + 0.020 O + yoal 70 2.600 2.700 (68,581 7.000 (1 77,80) 7.1 O0 (1 8OW 7.200 (1 82,88) 7.300 (1 85,42) 0.400 O4 I (10,16) 71

18、0.500 O5 1 (12,701 28 72 29 73 0.600 30 5.200 52 I (132,08) 7.400 74 I (187,96) 0.800 O8 I (20,32) 31 3.1 O0 (78,741 5.300 53 1 (134,62) 7.500 75 I (190,501 0.900 O9 I (22,86) 3.200 32 I (81,28) 5.400 5.500 7.600 7.700 7.800 (1 98,12) 7.900 (200,66) 55 1 (139,70) 1 .o00 1.100 1.200 l2 (30,48) 3.300

19、3.400 3.500 (88,901 3.600 36 (91,44) 5.600 5.700 1.300 l3 I (33,02) 5.800 58 I (147,32) 8.000 8o I (203,20) 1.400 l4 I (3536) 3.700 37 I (93,98) 1.500 1 (38,101 3.800 3.900 4.000 (1 01,60) 4.100 (1 04,14) 8.200 8.300 1.600 1.700 1.800 (45,721 1 .goo (48,261 6.100 6.200 8.400 84 1 (213,36) 6.300 63 1

20、 (160,021 8.500 85 (215,90) 4.200 42 I (106,68) 8.600 2.000 2o I (50,80) 4.300 4.400 6.500 6.600 6.700 (1 70,18) 2.100 21 I (53,341 8.800 88 I (22332) 8.900 89 I (226,06) 4.500 4.600 4.700 (1 19,38) 6.800 68 I (172,72) 9.000 I (228,60) 6.900 69 I (175,26) 7.100 1 (231,141 (continued) (continued) (co

21、ntinued) (continued) 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-,-,-STD*AECMA PREN bOb7-ENGL 2000 W 103231i 0038978 2TV 9 Page 7 prEN 6067: 2000 Code

22、92 93 94 Table 2 (concluded) L + 0.020 (t t508 ) 9.200 (233,68) 9.300 (236,22) 9.400 (238,76) O Diameter Code Nominal inch 03 311 6 04 1 14 05 511 6 06 318 07 711 6 08 112 o9 911 6 10 518 12 314 14 718 16 I 9.500 9.600 9.700 (246,38) Double Shear Tensile Strength Recommended min. min. Hole Diameter

23、max. min. LBS LBS (daw (daw 4 600 200 O. 1940 o. 1900 (2 046) (88) (4,931 (4,83) 8 200 230 0.2540 0.2500 (3 648) (102) (6.45) (635) 12 800 510 0.3165 0.3125 18 400 575 0.3790 0.3750 25 O00 710 0.4425 0.4375 32 800 1160 0.5050 0.5000 (14 590) (51 5) (12,83) (12,70) 41 200 I 420 0.5675 0.5625 (18 327)

24、 (631) (1441) (1429) 51 200 2 070 0.6300 0.6250 (22 775) (920) (16,OO) (15,87) 73 600 2 950 0.7570 0.7500 (32 739) (1 312) (1923) (1 9,05) 100 O00 3 900 0.8820 0.8750 (44 482) (I 734) (22,401 (22.22) 131 O00 5 480 1 .o1 O0 1 .o000 (58 272) (2 437) (25,651 (25,40) (5 694) (226) (8,041 (7,941 (8 185)

25、(255) (9,631 (9,521 (11 121) (31 5) (1 1,24) (11,ll) 3.2 Mechanical characteristics See table 3 Table 3 : Mechanical characteristics, hole diameter Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or netwo

26、rking permitted without license from IHS-,-,-Page 8 prEN 6067: 2000 Spindle Button Spring Handle 3.3 Materials, finishes See table 4. Alloy steel 4130 (HRC 36 to 40) as per AMs-S-6758 Carbon steel as per ASTM A 108 Music wire as per ASTM A 228 Carbon steel as per ASTM A 108 or CRES 302 as per QQ-S-7

27、63 Table 4 : Materials, finishes Head ELEMENTS I Alloy steel 4130 as per MIL-S-6758 (HRC 36 to 40) or Carbon steel as per ASTM A 108 (HRC 36 to 40) Figure 1 4ttaching Ring o Music wire as per ASTM A 228 o Balls Ring Handle o CRES 440C (HRC 58 to 62) as per AMS-QQ-S-763 CRES 17-7 PH as per AMS 5678 (

28、heat treatment to CH 900) or CRES 302 as per ASTM A 313 Description I Description block Pin, quick release, self-retaining, positive locking, double acting, button handle MATERIAL Identity block EN6067T04-1 O I Alloy steel 4130 (HRC 36 to 40) as per AMs-T-6736 or AMs-S-6758 I- Number of this standar

29、d Handle code (see figure i) Diameter code (see table I) TAB Carbon steel as per ASTM A 108 or CRES 302 as per ASTM A 240 FINISH Cadmium plated as per QQ-P-4 1 6 type I I, class 2 Cadmium plated as per QQ-P-416 type II, class 2 Passivated as per ASTM A 967 Cadmium plated as per QQ-P-416 type II, cla

30、ss 2 Cadmium plated as per QQ-P-416 type II, class 2 Passivated as per ASTM A 967 Cadmium plated as per QQ-P-416 type II, class 2 4 Designation EXAMPLE : NOTE: If necessary, the code 19005 shall be placed between the description block and the identity block Copyright Association Europeene des Constr

31、ucteurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD-AECMA PREN bOb7-ENGL 2000 10123LL 00187aO 752 Page 9 prEN 6067: 2000 5 Marking Paris shall be marked as per EN 2424, style P (see figure 1). 6 Technical specification See MIL-P-23460. 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