SAE AS 5587B-2009 CLAMP LOOP PLAIN SUPPORT AIRCRAFT《航空器支持平面式环状夹具》.pdf

上传人:postpastor181 文档编号:1024888 上传时间:2019-03-21 格式:PDF 页数:3 大小:52.72KB
下载 相关 举报
SAE AS 5587B-2009 CLAMP LOOP PLAIN SUPPORT AIRCRAFT《航空器支持平面式环状夹具》.pdf_第1页
第1页 / 共3页
SAE AS 5587B-2009 CLAMP LOOP PLAIN SUPPORT AIRCRAFT《航空器支持平面式环状夹具》.pdf_第2页
第2页 / 共3页
SAE AS 5587B-2009 CLAMP LOOP PLAIN SUPPORT AIRCRAFT《航空器支持平面式环状夹具》.pdf_第3页
第3页 / 共3页
亲,该文档总共3页,全部预览完了,如果喜欢就下载吧!
资源描述

1、 AEROSPACE STANDARD CLAMP, LOOP, PLAIN, SUPPORT, AIRCRAFT AS5587Copyright 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, mechanical, photocopying, recording, or otherwise

2、, 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 ISSUED 2000-09REVISED 2009-06 REAFFIRMED 2015-04THIRD ANGLE PROJEC

3、TION CUSTODIAN: G-3/G-3E REV.B FEDERAL SUPPLY CLASS 5340AS5587 SHEET 1 OF 3 REV. B PROCUREMENT SPECIFICATION: NONESAE Technical Standards Board Rules provide that: “This report ispublishedby SAE toadvance thestate of technicalandengineering sciences. Theuse ofthisreportis entirelyvoluntary, andits a

4、pplicability and suitability forany particular use,including any patent infringement arising therefrom, is thesole responsibilityoftheuser.”SAE reviews eachtechnicalreport at least every five years at which time itmay berevised,reaffirmed, stabilized, orcancelled. SAE invites yourwrittencomments and

5、suggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS5587B RATIONALE AS5587B HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY. FIGURE 1 - CLAMP TABLE 1 - DIMENSIONS SIZE CODE RANGE /10/ G MIN G MAX R A

6、L ALLOY W .015 AL ALLOY C .005 CRES W .015 CRES C .005 X .015 02 - 10 .062 .078 .062 .500 .218 .375 .204 .188 11 - 19 .062 .078 .109 .500 .218 .500 .218 .218 20 - 32 .094 .125 .125 .500 .218 .500 .218 .218 33 - 66 .125 .156 .125 .500 .218 .500 .218 .218 AEROSPACE STANDARD AS5587 SHEET 2 OF 3 REV. B

7、CLAMP, LOOP, PLAIN, SUPPORT, AIRCRAFT TABLE 2 - DIMENSIONS AND SIZE CODE SIZE CODE TUBE DIA D AL ALLOY CRES AL ALLOY CRES /10/ OD (REF) E E T T 02 .125 .125 .360 .360 .030 - .035 .017 - .023 03 .188 .188 .423 .423 .030 - .035 .017 - .023 04 .250 .250 .457 .457 .030 - .035 .017 - .023 05 .313 .313 .4

8、98 .498 .030 - .035 .017 - .023 06 .375 .375 .529 .529 .030 - .035 .017 - .023 07 .438 .438 .560 .560 .030 - .035 .017 - .023 08 .500 .500 .592 .592 .030 - .035 .017 - .023 09 .563 .563 .623 .623 .030 - .035 .017 - .023 10 .625 .625 .654 .654 .030 - .035 .017 - .023 11 .688 .688 .752 .749 .046 - .05

9、4 .028 - .036 12 .750 .750 .783 .780 .046 - .054 .028 - .036 13 .813 .813 .814 .811 .046 - .054 .028 - .036 14 .875 .875 .845 .842 .046 - .054 .028 - .036 15 .938 .938 .877 .858 .046 - .054 .028 - .036 16 1.000 1.000 .908 .889 .046 - .054 .028 - .036 17 1.063 1.063 .939 .920 .046 - .054 .028 - .036

10、18 1.125 1.125 .970 .951 .046 - .054 .028 - .036 19 1.188 1.188 1.002 .983 .046 - .054 .028 - .036 20 1.250 1.250 1.062 1.030 .058 - .068 .028 - .036 21 1.313 1.313 1.093 1.061 .058 - .068 .028 - .036 22 1.375 1.375 1.124 1.092 .058 - .068 .028 - .036 23 1.438 1.438 1.156 1.124 .058 - .068 .028 - .0

11、36 24 1.500 1.500 1.187 1.155 .058 - .068 .028 - .036 25 1.563 1.563 1.218 1.186 .058 - .068 .028 - .036 26 1.625 1.625 1.249 1.217 .058 - .068 .028 - .036 27 1.688 1.688 1.281 1.249 .058 - .068 .028 - .036 28 1.750 1.750 1.312 1.280 .058 - .068 .028 - .036 29 1.812 1.812 1.344 1.312 .058 - .068 .02

12、8 - .036 30 1.875 1.875 1.374 1.342 .058 - .068 .028 - .036 31 1.938 1.938 1.406 1.374 .058 - .068 .028 - .036 32 2.000 2.000 1.437 1.405 .058 - .068 .028 - .036 33 2.062 2.062 1.468 1.444 .058 - .068 .036 - .044 34 2.125 2.125 1.499 1.475 .058 - .068 .036 - .044 35 2.188 2.188 1.531 1.507 .058 - .0

13、68 .036 - .044 36 2.250 2.250 1.562 1.538 . 058 - .068 .036 - .044 37 2.312 2.312 1.594 1.570 .058 - .068 .036 - .044 38 2.375 2.375 1.624 1.600 .058 - .068 .036 - .044 40 2.500 2.500 1.687 1.663 .058 - .068 .036 - .044 42 2.625 2.625 1.752 1.728 .058 - .068 .036 - .044 43 2.680 2.680 1.778 1.754 .0

14、58 - .068 .036 - .044 44 2.750 2.750 1.812 1.788 .058 - .068 .036 - .044 45 2.812 2.812 1.844 1.820 .058 - .068 .036 - .044 46 2.875 2.875 1.875 1.851 .058 - .068 .036 - .044 48 3.000 3.000 1.937 1.913 .058 - .068 .036 - .044 50 3.125 3.125 2.000 1.976 .058 - .068 .036 - .044 52 3.250 3.250 2.062 2.

15、038 .058 - .068 .036 - .044 54 3.375 3.375 2.125 2.101 .058 - .068 .036 - .044 56 3.500 3.500 2.187 2.163 .058 - .068 .036 - .044 58 3.625 3.625 2.250 2.226 .058 - .068 .036 - .044 64 4.000 4.000 2.437 2.413 .058 - .068 .036 - .044 66 4.125 4.125 2.500 2.476 .058 - .068 .036 - .044 AEROSPACE STANDAR

16、D AS5587 SHEET 3 OF 3 REV. B CLAMP, LOOP, PLAIN, SUPPORT, AIRCRAFT NOTES: /1/ MATERIAL: a. CODE LETTER C - TYPE 321 CORROSION RESISTANT STEEL PER AMS5510. b. CODE LETTER D - 2024-0 ALUMINUM ALLOY PER AMS-QQ-A-250/5. 2. HEAT TREATMENT: a. CODE LETTER D - HEAT TREAT TO T42 TEMPER IN ACCORDANCE WITH AM

17、S2770. 3. FINISH: a. CODE LETTER C - PASSIVATE PER AMS2700 TYPE 6 OR 7. b. CODE LETTER D - CHEMICAL CONVERSION COATING PER MIL-DTL-5541, CLASS 1A. TOUCHUP IS PERMITTED WITHIN THE LIMITS SPECIFIED IN MIL-DTL-5541. 4. CLOSURE TEST: THE CLAMP SHALL BE INSTALLED ON A BAR HAVING A DIAMETER EQUAL TO THE N

18、OMINAL D DIAMETER WITHIN .001. DIMENSION G (GAP) SHALL BE RESTRAINED WITHIN THE SPECIFIED TOLERANCE LIMITS AND THE HOLES SHALL BE IN ALIGNMENT WITHIN .010. THE BAND WIDTH STRAIGHTNESS (PARALLEL TO THE BAR AXIS) SHALL BE WITHIN .010. /5/ IDENTIFICATION: MARK PART NUMBER AND MANUFACTURERS NAME, TRADEM

19、ARK OR CAGE CODE PER AS478- 2A1, AS478-2D1, or AS478-2E1. DO NOT MARK IN RADIUS. 6. REMOVE BURRS AND SHARP EDGES. 7. DIMENSIONING AND TOLERANCING: ASME Y14.5M-1994. 8. FORMING OF THE 90 DEGREE BEND FOOT IN ALUMINUM BANDS SHALL BE PERFORMED IN THE ANNEALED CONDITION. CURLING (SIZING) MAY BE DONE SUBS

20、EQUENT TO HEAT TREATMENT. 9. DIMENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED, TOLERANCE: LINEAR DIMENSIONS .010, ANGULAR DIMENSIONS 5 DEGREES. /10/ EXAMPLE OF PART NUMBER: 11. A CHANGE BAR ( l ) LOCATED IN THE LEFT MARGIN IS FOR THE CONVENIENCE OF THE USER IN LOCATING AREAS WHERE TECHNICAL REVISION

21、S, 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.

展开阅读全文
相关资源
猜你喜欢
相关搜索

当前位置:首页 > 标准规范 > 国际标准 > 其他

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