1、 AEROSPACE STANDARD FEMALE FERRULE, THREADLESS - FLEXIBLE, FIXED CAVITY, SELF-BONDING, SWAGED AS4735Copyright 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, p
2、hotocopying, 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 ISSUED 1995-11REAFFIRMED2004-0
3、5REVISED 2015-02THIRD ANGLE PROJECTION CUSTODIAN: G-3/G-3A REV.B FEDERAL SUPPLY CLASS 4730 AS4735 SHEET 1 OF 3 REV. B PROCUREMENT SPECIFICATION: /4/ AS1650SAE Technical Standards Board Rules provide that: “This report ispublished by SAE toadvance thestate of technicalandengineering sciences. Theuse
4、ofthisreport is entirelyvoluntary, andits applicability and suitability forany particularuse,including any patent infringement arising therefrom, isthe soleresponsibilityofthe user.”SAE reviews eachtechnicalreport at least every five years at which time itmay berevised,reaffirmed, stabilized, orcanc
5、elled. SAE invites yourwrittencomments andsuggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS4735B RATIONALE CORRECTED PASSIVATION SPECIFICATION AND TYPES AND ADDED PRI-QPL REQUIREMENTS. FIGURE 1 - FEMALE FERRULE TABL
6、E 1 - DIMENSIONS AND WEIGHTS /6/ BASIC NO. AS4735 /14/ SIZE CODE NOM TUBE SIZE REF A .003 B .010 C .015 D REF E F .001 M N LB/EA NOM REF ALUM LB/EA NOM REF CRES LB/EA NOM REF TI 08 .500 .507 .955 .516 .622 .470 .007 3 4 .010 .030 .017 10 .625 .633 .955 .516 .747 .595 .007 3 4 .012 .035 .020 12 .750
7、.758 1.035 .596 .887 .720 .007 3 4 .018 .050 .028 16 1.000 1.008 1.193 .676 1.139 .970 .008 4 5 .026 .074 .042 20 1.250 1.259 1.193 .676 1.389 1.220 .008 4 5 .031 .088 .050 24 1.500 1.509 1.282 .676 1.639 1.470 .009 5 6 .040 .112 .064 28 1.750 1.759 1.282 .676 1.889 1.720 .009 5 6 .045 .127 .072 32
8、2.000 2.009 1.322 .706 2.142 1.970 .009 5 6 .053 .151 .086 36 2.250 2.259 1.338 .706 2.392 2.220 .009 5 6 .060 .168 .096 40 2.500 2.510 1.338 .706 2.642 2.470 .011 5 6 .064 .181 .103 48 3.000 3.010 1.338 .706 3.142 2.970 .011 5 6 .074 .210 .119 56 3.500 3.512 1.368 .706 3.642 3.470 .012 6 7 .086 .24
9、1 .137 64 4.000 4.012 1.546 .706 4.151 3.970 .013 7 8 .113 .319 .181 AEROSPACE STANDARD AS4735 SHEET 2 OF 3 REV. B FEMALE FERRULE, THREADLESS - FLEXIBLE, FIXED CAVITY, SELF-BONDING, SWAGED NOTES: /1/ MATERIAL: a. CODE LETTER A - TYPE 2024-T6, T851, T8510, OR T8511 ALUMINUM ALLOY PER AMS-QQ-A-225/6,
10、AMS4120, AMS4339, AMS-QQ-A-200/3, WW-T-700/3, ASTM B211, OR ASTM B241. b. CODE LETTER C - 1. TYPE 17-4PH, CONDITION H1075 STA, CORROSION RESISTANT STEEL PER AMS5643. 2. TYPE 15-5PH, CONDITION H1150 STA, CORROSION RESISTANT STEEL PER AMS5659. c. CODE LETTER T - TYPE 6Al-4V, CONDITION A, TITANIUM ALLO
11、Y PER AMS4928 OR AMS4967 (MIL-T-9047). 2. HEAT TREATMENT: a. MATERIAL CODE LETTER A - IF THE RAW MATERIAL IS PROCURED IN THE SOLUTION TREATED CONDITION, AGE TO THE FINAL CONDITION PER AMS-H-6088 OR AMS2770. b. MATERIAL CODE LETTER C - 1. TYPE 17-4PH - AGE TO CONDITION H1075 PER MIL-H-6875 OR AMS2759
12、/3. 2. TYPE 15-5PH - AGE TO CONDITION H1150 PER MIL-H-6875 OR AMS2759/3. c. MATERIAL CODE LETTER T - NONE. 3. FINISH: a. MATERIAL CODE LETTER A - CHEMICAL CONVERSION COAT PER MIL-C-5541, CLASS 3. b. MATERIAL CODE LETTER C - PASSIVATE PER AMS2700 TYPE 2 OR TYPE 8. c. MATERIAL CODE LETTER T - NONE. /4
13、/ PROCUREMENT SPECIFICATION: AS1650 UNLESS SPECIFIED OTHERWISE ON THIS STANDARD. PRODUCT SUPPLIED TO THIS SPECIFICATION SHALL BE MANUFACTURED BY AN ACCREDITED MANUFACTURER AS LISTED IN THE PERFORMANCE REVIEW INSTITUTE (PRI) QUALIFIED PRODUCTS LIST (QPL) PRI-QPL-AS1650 FOR THIS STANDARD. SEE www.eAud
14、itN FOR CURRENT QPL ONLINE. /5/ IDENTIFICATION: MARK PER AS478-30 USING .062 INCH OR LARGER CHARACTERS. MARK AS A MINIMUM THE MANUFACTURERS NAME, TRADEMARK OR CAGE CODE, COMPLETE “AS” NUMBER AND DATE OF MANUFACTURE IN QUARTERS (1Q98 = FIRST QUARTER 1998). SIZES 12 AND SMALLER MAY BE INDIVIDUALLY BAG
15、GED WITH A TAG PER AS478-35D CONTAINING THE PREVIOUS INFORMATION. /6/ OTHER DIMENSIONS AND TOLERANCES ARE SPECIFIED AND CONTROLLED BY THE SUPPLIER. THE SUPPLIER IS RESPONSIBLE TO ENSURE COMPATIBILITY WITH THE ASSEMBLY AND COMPLIANCE WITH THE REQUIREMENTS OF THE PROCUREMENT SPECIFICATION. 7. INVENTOR
16、IED PARTS CONFORMING TO THE PREVIOUS ISSUE MAY BE USED TO DEPLETION. 8. 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
17、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. 9. INTERPRETATION OF DRAWING PER AS4296. 10. SURFACE TEXTURE: SYMBOLS PER ASME Y14.36M.
18、REQUIREMENTS PER ASME B46.1. UNLESS OTHERWISE SPECIFIED, MACHINED SURFACES TO BE 125 MICROINCHES Ra. AEROSPACE STANDARD AS4735 SHEET 3 OF 3 REV. B FEMALE FERRULE, THREADLESS - FLEXIBLE, FIXED CAVITY, SELF-BONDING, SWAGED 11. BREAK EDGES .003 TO .015 UNLESS OTHERWISE SPECIFIED. 12. DIMENSIONING AND TOLERANCING PER ASME Y14.5M-1994. 13. DIMENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED, TOLERANCES: LINEAR DIMENSIONS .005, ANGULAR DIMENSIONS 030. /14/ EXAMPLE OF PART NUMBER:
