1、 AEROSPACE STANDARD FITTING, SLEEVE, FLARED AS5176Copyright 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, without the
2、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 1999-01REVISED 2008-07 REAFFIRMED 2015-04THIRD ANGLE PROJECTION CUSTODIAN
3、: G-3/G-3B REV.C FEDERAL SUPPLY CLASS 4730AS5176 SHEET 1 OF 4 REV. C PROCUREMENT SPECIFICATION: /4/ AS4841SAE Technical Standards Board Rules provide that: “This report ispublishedby SAE toadvance thestate of technicalandengineering sciences. Theuse ofthisreportis entirelyvoluntary, andits applicabi
4、lity 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 andsuggesti
5、ons. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS5176C RATIONALE AS5176C HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY. FIGURE 1 - FITTING, SLEEVE INACTIVE IN PART /18/ AEROSPACE STANDARD AS5176 SHEET 2
6、 OF 4 REV. C FITTING, SLEEVE, FLARED TABLE 1A - DIMENSIONS B - J BASIC NO. AS5176 /15/ SIZE CODE (NOMINAL TUBE SIZE) B +.003 -.000 C +.000 -.003 F .005 G +.000 -.003 J 02 .125 .130 .172 .205 .267 .125 03 .188 .193 .234 .267 .329 .141 04 .250 .255 .297 .315 .383 .141 05 .312 .318 .366 .375 .445 .156
7、06 .375 .380 .432 .441 .502 .172 08 .500 .505 .562 .589 .682 .219 10 .625 .631 .690 .705 .797 .234 12 .750 .756 .826 .880 .972 .266 16 1.000 1.006 1.081 1.130 1.222 .281 20 1.250 1.260 1.339 1.412 1.534 .312 24 1.500 1.510 1.609 1.630 1.784 .344 28 1.750 1.762 1.882 1.945 2.159 .375 32 2.000 2.014 2
8、.159 2.195 2.409 .406 40 2.500 2.516 2.659 2.695 2.911 .469 48 3.000 3.016 3.172 3.195 3.411 .531 TABLE 1B - DIMENSIONS M - W AND WEIGHTS BASIC NO. AS5176 /15/ SIZE CODE M R W LB/EA APPROX REF COPPER LB/EA APPROX REF STEEL LB/EA APPROX REF TITANIUM 02 .344 .031 .005 .00215 .00203 .00112 03 .406 .031
9、 .005 .00331 .00313 .00173 04 .406 .031 .005 .00407 .00385 .00212 05 .438 .031 .005 .00567 .00536 .00296 06 .500 .047 .005 .00753 .00711 .00392 08 .562 .062 .005 .0154 .0146 .00804 10 .656 .062 .005 .0206 .0195 .0108 12 .688 .078 .005 .0249 .0235 .0130 16 .781 .094 .010 .0485 .0458 .0253 20 .906 .09
10、4 .010 .0814 .0767 .0424 24 1.125 .109 .010 .129 .122 .0672 28 1.125 .109 .010 .208 .197 .109 32 1.188 .109 .010 .272 .257 .142 40 1.312 .109 .010 .378 .357 .197 48 1.375 .109 .010 .503 .475 .262 AEROSPACE STANDARD AS5176 SHEET 3 OF 4 REV. C FITTING, SLEEVE, FLARED NOTES: NOTICE: THIS DOCUMENT REFER
11、ENCES A PART WHICH CONTAINS CADMIUM AS A PLATING MATERIAL. CONSULT LOCAL OFFICIALS IF YOU HAVE QUESTIONS CONCERNING CADMIUMS USE. /1/ MATERIAL: a. DASH AS CODE LETTER - TYPE 4130 STEEL BAR PER AMS6370 OR TYPE 4140 STEEL BAR PER AMS6382. /2/ b. CODE LETTER B - TYPE 360 COPPER ALLOY BAR PER ASTM B 16/
12、 B 16M OR AMS4610. c. CODE LETTER J - TYPE 304 CORROSION RESISTANT STEEL BAR PER AMS5639. d. CODE LETTER K - TYPE 316 CORROSION RESISTANT STEEL BAR PER AMS5648. e. CODE LETTER R - TYPE 321 CORROSION RESISTANT STEEL BAR PER AMS5645. f. CODE LETTER S - TYPE 347 CORROSION RESISTANT STEEL BAR PER AMS564
13、6. /18/ g. CODE LETTER T - 6AL-4V TITANIUM ALLOY BAR PER AMS4928. /16/ /2/ HEAT TREATMENT: a. DASH AS CODE LETTER - SEE HARDNESS REQUIREMENT PER PROCUREMENT SPECIFICATION. b. OTHER MATERIAL CODE LETTERS - NONE. 3. FINISH: a. DASH AS CODE LETTER - CADMIUM PLATE PER AMS-QQ-P-416, TYPE II, CLASS 2, DYE
14、 BLACK AND COAT WITH A LIGHT FILM OF OIL PER PROCUREMENT SPECIFICATION. b. MATERIAL CODE LETTER B - NONE. c. MATERIAL CODE LETTERS J, K, R AND S - PASSIVATE PER AMS2700, TYPE 6 OR 7. e. MATERIAL CODE LETTER T - ANODIZE PER AMS2488, TYPE 2 OR FLUORIDE PHOSPHATE CONVERSION COAT PER AMS2486. /4/ PROCUR
15、EMENT SPECIFICATION: AS4841 EXCEPT AS SPECIFIED ON THIS STANDARD. PRODUCT SUPPLIED TO THIS SPECIFICATION SHALL BE MANUFACTURED BY AN ACCREDITED MANUFACTURER LISTED IN THE NATIONAL AEROSPACE AND DEFENSE CONTRACTORS ACCREDITATION PROGRAM (NADCAP) QUALIFIED MANUFACTURER LIST FOR THIS PRODUCT TYPE. THE
16、QML IS AVAILABLE AT www.eAuditN. /5/ IDENTIFICATION AT LOCATION SHOWN: MARK MANUFACTURERS NAME, CAGE CODE OR TRADEMARK AND MATERIAL CODE LETTER PER AS478 CLASS C OR D, OR METHOD 7A3, 15A3 OR 15B. 6. INTENDED USE: THIS PART IS DESIGNED FOR USE IN SYSTEMS WITH MAXIMUM OPERATING PRESSURES AS SHOWN IN T
17、ABLE 2. AEROSPACE STANDARD AS5176 SHEET 4 OF 4 REV. C FITTING, SLEEVE, FLARED TABLE 2 - OPERATING PRESSURES FOR ASSOCIATED MATERIAL SIZE MATERIAL PSI 02-12 COPPER ALLOY 3000 16-48 COPPER ALLOY 1500 02-16 STEEL 3000 20-48 STEEL 1500 02-16 CORROSION RESISTANT STEEL 3000 20-48 CORROSION RESISTANT STEEL
18、 1500 02-16 TITANIUM ALLOY 3000 20-48 TITANIUM ALLOY 1500 7. THIS STANDARD IS THE FUNCTIONAL EQUIVALENT OF MS20819 (WITHOUT ALUMINUM) AND IS INTENDED TO BE SUITABLE AS A REPLACEMENT STANDARD. /17/ 8. A CHANGE BAR ( l ) LOCATED IN THE LEFT MARGIN IS FOR THE CONVENIENCE OF THE USER IN LOCATING AREAS W
19、HERE 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 DOCU
20、MENTS THAT CONTAIN EDITORIAL CHANGES ONLY. 9. INVENTORIED PARTS CONFORMING TO THE PREVIOUS “LETTER CHANGE” MAY BE USED TO DEPLETION. 10. INTERPRETATION OF DRAWING PER ARP4296. 11. SURFACE TEXTURE: SYMBOLS PER ASME Y14.36M; REQUIREMENTS PER ASME B46.1. UNLESS OTHERWISE SPECIFIED, MACHINED SURFACES TO
21、 BE 125 in Ra. 12. BREAK EDGES .003 TO .015 UNLESS OTHERWISE SPECIFIED. 13. DIMENSIONING AND TOLERANCING: ASME Y14.5M-1994. 14. DIMENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED, TOLERANCES: LINEAR DIMENSIONS .016, ANGULAR DIMENSIONS 030. /15/ EXAMPLE OF PART NUMBER: BASIC PART NUMBER MATERIAL CODE L
22、ETTER /1/ SIZE CODE, TUBE SIZE IN .062 INCREMENTS AS5176 J 08 /16/ TITANIUM SHALL NOT BE USED IN OXYGEN OR POTABLE WATER SYSTEMS. /17/ IF THE USER OF THIS DOCUMENT PLANS TO USE THIS DOCUMENT AS A REPLACEMENT FOR MS20819 (ALUMINUM), BE ADVISED THAT ALUMINUM WAS CANCELLED ON MS20819 AND SUBSEQUENTLY ELIMINATED ON AS5176, THE REPLACEMENT STANDARD. /18/ INACTIVE MATERIAL CODES: a. PART NUMBERS WITH MATERIAL CODE LETTER S ARE INACTIVE FOR NEW DESIGN AS OF 90 DAYS AFTER THIS REVISION DATE. USE PART NUMBERS WITH MATERIAL CODE LETTER R FOR NEW DESIGN.
