ImageVerifierCode 换一换
格式:PDF , 页数:4 ,大小:117.75KB ,
资源ID:1023623      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-1023623.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 AS 1735D-2009 NUT COUPLING RIGID FIXED CAVITY THREADED FERRULE TYPE TUBE ENDS TYPE II《带螺纹的套环型管端固定空腔刚性对开螺母 II型》.pdf)为本站会员(wealthynice100)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 AS 1735D-2009 NUT COUPLING RIGID FIXED CAVITY THREADED FERRULE TYPE TUBE ENDS TYPE II《带螺纹的套环型管端固定空腔刚性对开螺母 II型》.pdf

1、 AEROSPACE STANDARD NUT, COUPLING, RIGID, FIXED CAVITY, THREADED, FERRULE TYPE TUBE ENDS, TYPE II AS1735Copyright 2015 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanica

2、l, 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: +1 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org ISSUED1984-01REVISED2009-0

3、5REAFFIRMED2015-01THIRD ANGLE PROJECTION CUSTODIAN: G-3/G-3A REV.D FEDERAL SUPPLY CLASS 4730 SAE Technical StandardsBoardRulesprovidethat:“ThisreportispublishedbySAE toadvancethestateoftechnicalandengineering sciences. The use of thisreport isentirelyvoluntary, andits applicability andsuitability fo

4、r any particularuse, includingany patent infringement arising therefrom,is the soleresponsibility of theuser.”SAE reviewseachtechnical reportatleasteveryfiveyearsatwhichtimeitmayberevised,reaffirmed,stabilized,orcancelled. SAEinvites yourwritten comments andsuggestions.RATIONALE AS1735D HAS BEEN REA

5、FFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY. AS1735 SHEET 1 OF 4 REV. D PROCUREMENT SPECIFICATION: /3/ AS1730 SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AS1735D FIGURE 1 - NUT AEROSPACE STANDARD AS1735 SHEET 2 OF

6、 4REV. D NUT, COUPLING, RIGID, FIXED CAVITY, THREADED, FERRULE TYPE TUBE ENDS, TYPE II TABLE 1 - NUT DIMENSIONS BASIC NO. AS1735 SIZE CODE /15/ (TUBE SIZE) THREAD T PER FED-STD-H28/2 OR ASME B1.1 /10/ MOD A B PL C +.005 -.000 D D TOL 04 05 06 08 10 12 16 20 24 28 32 36 40 44 48 56 64 72 80 .250 .312

7、 .375 .500 .625 .750 1.000 1.250 1.500 1.750 2.000 2.250 2.500 2.750 3.000 3.500 4.000 4.500 5.000 .687-12 UN-2B .750-12 UN-2B .812-12 UN-2B .937-12 UN-2B 1.062-12 UN-2B 1.250-12 UNF-2B 1.500-12 UNF-2B 1.750-12 UN-2B 2.000-12 UN-2B 2.250-12 UN-2B 2.500-12 UN-2B 2.750-12 UN-2B 3.000-12 UN-2B 3.250-12

8、 UN-2B 3.625-12 UN-2B 4.125-12 UN-2B/ 4.625-12 UNS-2B/10/ 5.125-12 UNS-2B/10/ 5.625-12 UNS-2B/10/ .187 .187 .187 .187 .187 .187 .187 .187 .250 .250 .250 .250 .250 .250 .250 .250 .250 .250 .250 4 4 4 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 .529 .580 .635 .762 .900 1.033 1.284 1.534 1.783 2.045 2.292 2.549 2.

9、800 3.045 3.395 3.895 4.395 4.895 5.378 .583 .644 .689 .815 .960 1.128 1.386 1.628 1.878 2.138 2.382 2.638 2.888 3.138 3.513 4.013 4.513 5.015 5.500 +.002/-.000 +.002/-.000 +.002/-.000 +.003/-.000 +.003/-.000 +.003/-.000 +.003/-.000 +.003/-.000 +.003/-.000 +.003/-.000 +.003/-.000 +.003/-.000 +.003/-

10、.000 +.003/-.000 +.004/-.000 +.004/-.000 +.004/-.000 +.005/-.000 +.005/-.000 TABLE 2 - NUT DIMENSIONS AND WEIGHTS BASIC NO. AS1735 SIZE CODE /15/ E +.010 -.000 /11/ F +010 -.000 G MAX H +.010 -.000 J .015 K L MAX ALUM WEIGHT LB/EA APPROX REF 04 05 06 08 10 12 16 20 24 28 32 36 40 44 48 56 64 72 80 .

11、691 .753 .816 .941 1.066 1.253 1.503 1.753 2.003 2.253 2.503 2.753 3.003 3.253 3.628 4.128 4.613 5.113 5.613 .787 .850 .912 1.037 1.172 1.360 1.610 1.860 2.110 2.360 2.620 2.870 3.125 3.370 3.751 4.256 4.756 5.266 5.765 .829 .892 .954 1.079 1.214 1.402 1.652 1.902 2.152 2.402 2.662 2.912 3.162 3.412

12、 3.793 4.298 4.798 5.308 5.807 .338 .338 .338 .338 .354 .354 .354 .414 .429 .429 .429 .455 .455 .455 .455 .455 .455 .543 .543 .065 .065 .065 .065 .065 .065 .065 .065 .065 .065 .065 .100 .100 .100 .100 .100 .100 .130 .130 .300 .300 .300 .300 .315 .315 .315 .375 .375 .375 .375 .392 .392 .392 .392 .392

13、 .392 .475 .475 .553 .553 .553 .553 .569 .569 .569 .629 .644 .644 .644 .705 .705 .705 .705 .705 .705 .823 .823 .009 .010 .011 .013 .016 .019 .023 .030 .035 .039 .046 .058 .063 .068 .079 .092 .104 .144 .161 AEROSPACE STANDARD AS1735 SHEET 3 OF 4REV. D NUT, COUPLING, RIGID, FIXED CAVITY, THREADED, FER

14、RULE TYPE TUBE ENDS, TYPE II NOTES: 1. MATERIAL CODE D: a. ALUMINUM ALLOY 2024-T6, 2024-T851, OR 2024-T8511 PER AMS-QQ-A-225/6, ASTM B 210, AMS-QQ-A-200/3, OR AMS-WW-T-700/3. b. ALUMINUM ALLOY 2014-T6 PER AMS-QQ-A-225/4 OR AMS-QQ-A-200/2. 2. FINISH: MATERIAL CODE D: ANODIZE PER MIL-A-8625, TYPE II,

15、CLASS 2, COLOR MAGENTA. /3/ PRODUCT SUPPLIED TO THIS SPECIFICATION SHALL BE MANUFACTURED BY AN ACCREDITED MANUFACTURER LISTED IN THE PERFORMANCE REVIEW INSTITUTE (PRI) QUALIFIED PRODUCTS LIST FOR PRI-QPL-AS1730 FOR THIS STANDARD. SEE . FOR CURRENT QPL ON-LINE. /4/ IDENTIFICATION PER AS478 METHOD 30

16、INCLUDING THE MANUFACTURERS NAME, TRADEMARK, OR CAGE CODE, COMPLETE “AS“ PART NUMBER, AND DATE OF MANUFACTURE IN QUARTERS (3Q95 = THIRD QUARTER 1995). SIZES 12 AND SMALLER MAY BE INDIVIDUALLY PLACED IN A PLASTIC BAG WITH A TAG PER AS478 METHOD 35D CONTAINING THIS INFORMATION. ALL PARTS SHALL BE MARK

17、ED AS A MINIMUM WITH THE MANUFACTURES NAME, TRADEMARK OR CAGE CODE AND DATE OF MANUFACTURE. /5/ THE MANUFACTURER WILL SPECIFY AND CONTROL CERTAIN SPECIFIC DIMENSIONS AND TOLERANCES AND WILL BE RESPONSIBLE TO ASSURE COMPATIBILITY WITH THE ASSEMBLY AND COMPLIANCE WITH THE PERFORMANCE REQUIREMENTS OF A

18、S1730. /6/ KNURL MAY BE MEDIUM DIAMOND, MEDIUM PLAIN SPIRAL, OR FINE STRAIGHT. 7. LUBRICATION: THREADS SHALL BE COATED WITH SOLID FILM LUBRICANT TO A THICKNESS OF .0003 TO .0005 PER AS5272 TYPE I (MIL-L-46010 HAS BEEN SUPERSEDED BY MIL-PRF-46010) OVERSPRAY ALLOWED. 8. SURFACE TEXTURE: SYMBOLS PER AS

19、ME Y14.36M; REQUIREMENTS PER ASME Y14.36. UNLESS OTHERWISE SPECIFIED, MACHINED SURFACES TO BE 125 in Ra. 9. DIMENSIONING AND TOLERANCING: ASME Y14.5M-1994. /10/ NUT SIZES 64, 72, AND 80 HAVE THREADS WITH REDUCED PITCH DIAMETERS AS FOLLOWS: a. 64: 4.5559 +.0087/-.0000 b. 72: 5.0559 +.0087/-.0000 c. 8

20、0: 5.5559 +.0090/-.0000 /11/ NO THREAD MARKS ON DIAMETER “E”. THREAD MARKS IN .040/.065 RADIUS ADJACENT TO THE 15 DEGREE THREAD CHAMFER IS ACCEPTABLE. 12. INVENTORIED PARTS CONFORMING TO THE PREVIOUS REVISION MAYBE USED TO DEPLETION. 13. DIMENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED, TOLERANCES:

21、LINEAR DIMENSIONS .010, ANGULAR DIMENSIONS 2 DEGREES. 14. BREAK EDGES .003 TO .015 UNLESS OTHERWISE SPECIFIED. AEROSPACE STANDARD AS1735 SHEET 4 OF 4REV. D NUT, COUPLING, RIGID, FIXED CAVITY, THREADED, FERRULE TYPE TUBE ENDS, TYPE II /15/ EXAMPLE OF PART NUMBER: AS1735 D 16 BASIC NUT NUMBER NUT SIZE

22、 IN .062 in INCREMENTS (16 = 1 in TUBE SIZE) NUT MATERIAL CODE (D = ALUMINUM ALLOY) 16. A CHANGE BAR (l) LOCATED IN THE LEFT MARGIN IS FOR THE CONVENIENCE OF THE USER IN LOCATING AREAS WHERE TECHNICAL REVISIONS, NOT EDITORIAL CHANGES, HAVE BEEN MADE TO THE PREVIOUS ISSUE OF THIS DOCUMENT. AN (R) SYMBOL TO THE LEFT OF THE DOCUMENT TITLE INDICATES A COMPLETE REVISION OF THE DOCUMENT, INCLUDING TECHNICAL REVISIONS. CHANGE BARS AND (R) ARE NOT USED IN ORIGINAL PUBLICATIONS, NOR IN DOCUMENTS THAT CONTAIN EDITORIAL CHANGES ONLY.

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