SAE AS 3122A-2008 Pin Expansion - Aluminum 2024-T4 and 2024-T351 Long (UNS A92024)《2024-T4和2024-T351长型铝制膨胀销(UNS A92024)》.pdf

《SAE AS 3122A-2008 Pin Expansion - Aluminum 2024-T4 and 2024-T351 Long (UNS A92024)《2024-T4和2024-T351长型铝制膨胀销(UNS A92024)》.pdf》由会员分享，可在线阅读，更多相关《SAE AS 3122A-2008 Pin Expansion - Aluminum 2024-T4 and 2024-T351 Long (UNS A92024)《2024-T4和2024-T351长型铝制膨胀销(UNS A92024)》.pdf（2页珍藏版）》请在麦多课文档分享上搜索。

1、AEROSPACE STANDARD (R) PIN, EXPANSION - ALUMINUM, 2024-T4 AND 2024-T351, LONG (UNS A92024) AS3122Copyright 2008 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, phot

2、ocopying, recording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org ISSUED 1981-02REAFFIRMED 2007-06 REV

3、ISED 2008-09 THIRD ANGLE PROJECTION CUSTODIAN: SAE E-25 REV.AFEDERAL SUPPLY CLASS 5315 AS3122SHEET 1 OF 2REV.APROCUREMENT SPECIFICATION: NONESAE TechnicalStandards Board Rules provide that: “This report is published by SAE toadvance thestate of technical andengineering sciences. Theuse of thisreport

4、 is entirely voluntary, andits applicabilityandsuitability forany particularuse, including any patent infringement arising therefrom, is thesole responsibility oftheuser.” SAE reviews each technical report at least every five yearsat which time it may be reaffirmed, revised, orcancelled. SAE invites

5、 yourwritten commentsandsuggestions. RATIONALEUPATE SUPPLIER PART NUMERS, CLARIFY PART MARKING, UPDATE MATERIAL USAGE, CORRECT DIMENSIONAL ERRORS, AND GENERAL SAE UPDATING FOR OBSOLETE SPECIFICATIONS AND FORMATTING REQUIREMENTS. FIGURE 1 TABLE 1 - PART NUMBERS AND DIMENSIONS AEROSPACE STANDARDPART N

6、UMBER /7/MANUFACTURERS PART NUMBER /7/ANOMB NOMCMAXDNOMENOMFNOMAPPROX MASSLB/100AS3122-03 PLGA1566010A .165 .123 .032 .0417 5 .110 .018 AS3122-04 PLGA1876010A .181 .154 .040 .0417 10 .138 .031 AS3122-05 PLGA2186010A .218 .182 .040 .0208 (a) (a) .053 AS3122-06 PLGA2506010A .265 .212 .040 .0417 10 .19

7、2 .088 AS3122-07 PLGA2816010A .280 .247 .040 .0313 (a) (a) .126 AS3122-08 PLGA3436010A .335 .294 .060 .0218 (a) (a) .217 AS3122-09 PLGA4066010A .397 .357 .060 .0208 (a) (a) .378 AS3122-10 PLGA4686010A .460 .419 .060 .0208 (a) (a) .614 AS3122-11 PLGA5316010A .522 .482 .060 .0156 (a) (a) .931 AS3122-1

8、2 PLGA6566010A .590 .601 .060 .0156 (a) (a) 1.637 (a) .01.02 RADIUS INSTEAD OF A CHAMFER NOTES: 1. MATERIAL: AMS4120 SIMILAR TO UNS A92024 (AL ALLOY 2024-T4; SIZES 03 THRU 08 AND AL ALLOY 2024-T351; SIZES 09 THRU 12), OR AMS-QQ-A-225/6 UNS A92024 (AL ALLOY 2024-T4; SIZES 03 THRU 08, AND AL ALLOY 202

9、4-T351; SIZES 09 THRU 12). 2. FINISH: MIL-DTL-5541, TYPE I, CLASS 1A OR 3, DYED YELLOW. 3. PINS ARE PREWAXED TO AID DRIVING. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS3122ACopyright SAE International Provided by IHS under

10、 license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD (R) PIN, EXPANSION - ALUMINUM, 2024-T4 AND 2024-T351, LONG (UNS A92024) AS3122SHEET 2 OF 2REV.A4. SURFACE TEXTURE: SYMBOLS PER ASME Y14.36M, REQUIREMENTS PER ASME B46.1. UNLESS OTHE

11、RWISE SPECIFIED, SURFACES TO BE 250 MICROINCHES Ra. 5. BREAK EDGES .003 TO .015 UNLESS OTHERWISE SPECIFIED. 6. DIMENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED, TOLERANCE: ANGULAR DIMENSIONS 2. DIMENSIONS APPLY AFTER FINISH. /7/ MARK AS3122-( ) PART NUMBER AND MANUFACTURERS PART NUMBER ON PACKAGE IN

12、 ACCORDANCE WITH AS478, METHOD 37. 8. USE WITH AS3121 PLUGS. SEE AIR3277 FOR INSTALLATION PROCEDURES. SEE AS3589 FOR AS3121 PLUG AND AS3122 PIN SET OF PARTS. 9. DIMENSIONING AND TOLERANCING PER ASME Y14.5M-1994. 10. DO NOT USE UNASSIGNED PART NUMBERS. 11. AS, AIR AND AMS ARE SAE INTERNATIONAL PUBLIC

13、ATIONS. ASME IS AN AMERICAN SOCIETY OF MECHANICAL ENGINEERS PUBLICATION. MIL IS AN US GOVERNMENT PUBLICATION. 12. 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

14、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. APPROVED SOURCE OF SUPPLY: THE LEE CO WESTB

15、ROOK, CT FEDERAL SUPPLY CODE FOR MANUFACTURERS NO 92555. ONLY THE ITEM DESCRIBED ON THIS DRAWING WHEN PROCURED FROM THE VENDOR LISTED HEREON IS APPROVED FOR USE IN THE APPLICATIONS SPECIFYING THIS AEROSPACE STANDARD IDENTIFICATION NUMBER. A SUBSTITUTE ITEM SHALL NOT BE USED WITHOUT PRIOR TESTING AND

16、 APPROVAL BY THE DESIGN ACTIVITY RESPONSIBLE FOR THE APPLICATION. IDENTIFICATION OF THE APPROVED SOURCE HEREON IS NOT TO BE CONSTRUED AS A GUARANTEE OF PRESENT OR CONTINUED AVAILABILITY AS A SOURCE OF SUPPLY FOR THE ITEM DESCRIBED ON THE DRAWING. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-