1、 AEROSPACE STANDARD COUPLING ASSEMBLY, THREADLESS - FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING AS7515Copyright 2017 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,
2、mechanical, 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 ISSUED2017-09THIR
3、D ANGLE PROJECTION CUSTODIAN: G-3/G-3A FEDERAL SUPPLY CLASS 4730 AS7515 SHEET 1 OF 3 PROCUREMENT SPECIFICATION: AS7510 /4/ SAETechnicalStandardsBoard Rulesprovidethat:“Thisreportispublished bySAEto advance the state oftechnicaland engineering sciences.The use ofthisreportisentirelyvoluntary,anditsap
4、plicabilityandsuitabilityforanyparticularuse,includinganypatentinfringementarising therefrom,isthe sole responsibilityoftheuser.”SAEreviewseachtechnicalreportatleasteveryfiveyearsatwhich time itmaybe revised,reaffirmed,stabilized,orcancelled.SAEinvitesyourwritten commentsandsuggestions.SAE values yo
5、ur input. To provide feedback on this Technical Report, please visit http:/standards.sae.org/AS7515 RATIONALE NEW PART STANDARD AS PART OF AS7510 TO SUPERSEDE AS5835. FIGURE 1 COUPLING BODY AEROSPACE STANDARD AS7515 SHEET 2 OF 3 COUPLINGASSEMBLY, THREADLESS - FLEXIBLE, FIXED CAVITY, CURRENT CARRYING
6、, SELF BONDING TABLE 1 DIMENSIONS AND WEIGHTS /6/ BASIC NO AS7515 /17/ SIZE CODE NOM TUBE SIZE REF A MAX /8/ B MAX C +.003 -.007 D MAX /8/ E MIN /8/ F MAX /9/ MAX WEIGHT LB/EA (REF) 08 .500 1.17 .895 .646 .640 .777 1.85 .050 10 .625 1.30 .895 .646 .765 .902 1.98 .053 12 .750 1.48 1.019 .750 .925 1.0
7、83 2.16 .062 16 1.000 1.77 1.107 .830 1.190 1.364 2.45 .076 20 1.250 2.02 1.107 .830 1.440 1.611 2.70 .084 24 1.500 2.30 1.107 .830 1.690 1.881 2.98 .098 28 1.750 2.56 1.107 .830 1.940 2.133 3.24 .114 32 2.000 2.84 1.161 .874 2.193 2.406 3.52 .131 36 2.250 3.09 1.161 .874 2.443 2.656 3.77 .142 40 2.
8、500 3.35 1.171 .874 2.693 2.910 4.03 .155 48 3.000 3.87 1.211 .874 3.193 3.414 4.55 .205 56 3.500 4.41 1.301 .964 3.693 3.936 5.09 .250 64 4.000 4.93 1.331 .994 4.202 4.448 5.61 .284 NOTES /1/ MATERIAL: MATERIAL CODE LETTER A TYPE 2024-T351, T851, T8510, OR T8511 ALUMINUM ALLOY PER AMS-QQ-A-225/6, A
9、MS4120, AMS4339, AMS-QQ-A-200/3, AMS-WW-T-700/3 OR ASTM B211. 2. HEAT TREATMENT: MATERIAL CODE LETTER A IF THE RAW MATERIAL IS PROCURED IN THE SOLUTION TREATED CONDITION, AGE TO THE T851 OR T8511 CONDITION PER AMS2770 OR AMS2772. 3. FINISH: MATERIAL CODE LETTER A ANODIZE PER AMS2472, OR MIL-A-8625,
10、TYPE II, CLASS 2, DYE BLUE, SIMILAR IN COLOR TO AMS-STD-595 NO. 15180 or 15095, DUPLEX SEALED, EXCEPTAREAS NOTED IN NOTE 7 TO BE CHEMICAL CONVERSION COATED PER MIL-DTL-5541, CLASS 3. /4/ COUPLING BODIES SUPPLIED TO THIS SPECIFICATION SHALL BE MANUFACTURED AND ASSEMBLED BY AN ACCREDITED MANUFACTURER
11、LISTED IN THE PERFORMANCE REVIEW INSTITUTE (PRI) QUALIFIED PRODUCTS (QPL) LIST (QPL) FOR PRI-QPL-AS7510. THE QPL IS AVAILABLE AT www.eAuditN. /5/ IDENTIFICATION: MARK PER AS478-15A OR AS478-30 USING .062 OR LARGER CHARACTERS. MARK AS A MINIMUM THE MANUFACTURERS NAME, AND/OR CAGE CODE, COMPLETE “AS”
12、NUMBER AND DATE OF MANUFACTURE IN ACCORDANCE WITH MIL-STD-130. SIZES 20 AND SMALLER MAY BE INDIVIDUALLY BAGGED WITH A TAG PER AS478-35D CONTAINING THE PREVIOUS INFORMATION. /6/ OTHER DIMENSIONS AND TOLERANCES NOT SPECIFIED ARE CONTROLLED BY THE MANUFACTURER. THE MANUFACTURER IS RESPONSIBLE TO ENSURE
13、 COMPATIBILITY WITH THE ASSEMBLY AND COMPLIANCE WITH THE REQUIREMENTS OF THE PROCUREMENT SPECIFICATION. /7/ FOR ALUMINUM ALLOY PARTS, THE BONDING SPRING CAVITIES TO BE CONDUCTIVE AND BE COMPATIBLE WITH THE ANODIZE FINISH. BONDING SPRING MUST BE WITHIN THE MAXIMUM “B” DIMENSION. /8/ THIS DIAMETER IS
14、NOT A TRUE CIRCLE BECAUSE OF TOLERANCE BUILD-UP IN THE HINGE AND LATCH AREA. /9/ THE F IS A MAXIMUM ENVELOPE DIMENSION BASED ON 2 TIMES THE TUBE CENTERLINE RADIUS OVER THE VISUAL TACTILE LATCH INDICATOR (VTLI). 10. THE CLAMSHELL ASSEMBLY SHALL PROVIDE AN ELECTROSTATIC BOND PATH BETWEEN THE CONNECTIN
15、G FERRULES AND THE SLEEVE CONTACT AREA AS DEFINED IN AS7514. AEROSPACE STANDARD AS7515 SHEET 3 OF 3 COUPLINGASSEMBLY, THREADLESS - FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING 11 THE CLAMSHELL BODY SHALL INCLUDE A NON-METALLIC, NON-CONDUCTIVE VISUAL TACTILE LATCH INDICATION (VTLI) THAT CON
16、FIRMS A CLOSED AND LATCHED CONDITION WITH THE PAWLS FULLY LATCHED AND SEATED. THE SUPPLIER SHALL SELECT A SUITABLE MATERIAL THAT MEETS THE PERFORMANCE AND ENVIRONMENTAL REQUIREMENTS OF AS7510. 12. INTERPRETATION OF DRAWING PER AS4296. 13. SURFACE TEXTURE: SYMBOLS PER ASME Y14.36M; REQUIREMENTS PER A
17、SME B46.1. UNLESS OTHERWISE SPECIFIED, MACHINED SURFACE TO BE 125 MICROINCHES Ra. 14. BREAK EDGES .003 TO .015, UNLESS OTHERWISE SPECIFIED. 15. DIMENSION AND TOLERANCE PER ASME Y14.5 2009. 16. DIMENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED, TOLERANCES: LINEAR DIMENSIONS .005, ANGULAR DIMENSIONS 03
18、0. /17/ EXAMPLE OF PART NUMBER: AS7515 A 32 BASIC PART NUMBER MATERIAL CODE LETTER /1/ SIZE CODE, TUBE SIZE IN .062 INCH INCREMENTS (SEE TABLE 1) EXAMPLE OF PART NUMBER: AS7515A32 SPECIFICATION NOTES 1. REVISION INDICATOR: A CHANGE BAR (l) LOCATED IN THE LEFT MARGIN IS FOR THE CONVENIENCE OF THE USE
19、R 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.
