1、 SAE AS6213 ADOPTION NOTICE SAE AS6213, “Fitting, Adapter, Port, Reducer, 37 Degree Spherical, Flared“, was adopted on 13 August 2014 for use by the Department of Defense (DoD). Proposed changes by DoD activities must be submitted to the DoD Adopting Activity: DLA Land and Maritime, ATTN: VAI, 3990
2、East Broad Street, Columbus, OH 43218-3990 or fluidflowdla.mil. Copies of these documents are available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org. CONCLUDING MATERIAL Custodians: Pre
3、paring activity: Army -AV DLA - CC Navy - AS Air Force - 99 (Project 4730-2014-067) DLA - CC NOTE: The activities listed above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information abov
4、e using the ASSIST Online database at https:/assist.dla.mil. AMSC N/A FSC 4730 AEROSPACE STANDARD FITTING, ADAPTER, PORT, REDUCER, 37 DEGREE SPHERICAL, FLARED AS6213Copyright 2012 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or tr
5、ansmitted, in any form or by any means, electronic, 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
6、SAE WEB ADDRESS: http:/www.sae.org ISSUED 2012-09THIRD ANGLE PROJECTION CUSTODIAN: G-3/G-3B FEDERAL SUPPLY CLASS 4730 AS6213 SHEET 1 OF 4 PROCUREMENT SPECIFICATION: /4/ AS6076SAE Technical Standards Board Rules provide that: “This report ispublishedby SAE toadvance thestate of technicalandengineerin
7、g sciences. Theuse ofthis report is entirely voluntary, andits applicability and suitability forany particular use,including any patent infringement arising therefrom, isthe soleresponsibilityofthe user.”SAE reviews eachtechnicalreport at least every five years at which time itmay berevised, reaffir
8、med, stabilized, orcancelled. SAE invites yourwrittencomments andsuggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS6213 RATIONALE THIS SAE AEROSPACE STANDARD (AS) ESTABLISHES THE REQUIREMENTS FOR THE ADAPTER, PORT, R
9、EDUCER, WITH 37 DEGREE SPHERICAL FLARED TUBE. FIGURE 1 - FITTING AEROSPACE STANDARD AS6213 SHEET 2 OF 4 FITTING, ADAPTER, PORT, REDUCER, 37 DEGREE SPHERICAL, FLARED TABLE 1 - DIMENSIONS AND WEIGHTS BASIC NO. AS6213 /19/ SIZE CODE NOMINAL TUBE SIZE PORT #1 NOMINAL TUBE SIZE PORT #2 S THREAD PER AS887
10、9 CLASS 3B T THREAD PER AS8879 CLASS 3A D .010 H J M LB EA APPROX AL REF LB EA APPROX STL REF LB EA APPROX TI REF 0403 .250 .188 .4375-20UNJF .3750-24UNJF .668 .678- .691 .672 1.297 .0378 .109 .0599 0504 .312 .250 .5000-20UNJF .4375-20UNJF .730 .740 - 753 .672 1.500 .0433 .124 .0685 0604 .375 .250 .
11、5625-18UNJF .4375-20UNJF .793 .803 - .816 .630 1.391 .0511 .147 .0809 0605 .375 .313 .5625-18UNJF .5000-20UNJF .793 .803 - .816 .630 1.375 .0534 .153 .0846 0804 .500 .250 .7500-16UNJF .4375-20UNJF .980 .990 - 1.003 .750 1.609 .0649 .186 .103 0805 .500 .313 .7500-16UNJF .5000-20UNJF .980 .990 - 1.003
12、 .750 1.547 .0672 .193 .107 0806 .500 .375 .7500-16UNJF .5625-18UNJF .980 .990 - 1.003 .750 1.547 .0698 .200 .111 1004 .625 .250 .8750-14UNJF .4375-20UNJF 1.103 1.113 - 1.128 .810 1.672 .0713 .205 .113 1005 .625 .313 .8750-14UNJF .5000-20UNJF 1.103 1.113 - 1.128 .810 1.656 .0737 .212 .117 1006 .625
13、.375 .8750-14UNJF .5625-18UNJF 1.103 1.113 - 1.128 .810 1.641 .0763 .219 .121 1008 .625 .500 .8750-14UNJF .7500-16UNJF 1.103 1.113 - 1.128 .810 1.750 .090 .258 .143 1206 .750 .375 1.0625-12UNJ .5625-18UNJF 1.353 1.363 - 1.380 .940 1.813 .102 .294 .162 1208 .750 .500 1.0625-12UNJ .7500-16UNJF 1.353 1
14、.363 - 1.380 .940 1.922 .116 .334 .184 1210 .750 .625 1.0625-12UNJ .8750-14UNJF 1.353 1.363 - 1.380 .940 2.016 .131 .376 .207 1606 1.000 .375 1.3125-12UNJ .5625-18UNJF 1.603 1.613 - 1.630 .970 1.922 .123 .352 .194 1608 1.000 .500 1.3125-12UNJ .7500-16UNJF 1.603 1.613 - 1.630 .970 2.032 .136 .391 .21
15、6 1610 1.000 .625 1.3125-12UNJ .8750-14UNJF 1.603 1.613 - 1.630 .970 2.109 .151 .434 .293 1612 1.000 .750 1.3125-12UNJ 1.0625-12UNJ 1.603 1.613 - 1.630 .970 2.203 .179 .514 .283 2008 1.250 .500 1.6250-12UNJ .7500-16UNJF 1.853 1.863 - 1.880 1.010 2.172 .137 .392 .216 2010 1.250 .625 1.6250-12UNJ .875
16、0-14UNJF 1.853 1.863 - 1.880 1.010 2.250 .151 .435 .240 2012 1.250 .750 1.6250-12UNJ 1.0625-12UNJ 1.853 1.863 - 1.880 1.010 2.328 .179 .515 .284 2016 1.250 1.000 1.6250-12UNJ 1.3125-12UNJ 1.853 1.863 - 1.880 1.010 2.297 .224 .642 .354 NOTES: NOTICE THIS DOCUMENT REFERENCES A PART WHICH CONTAINS CADM
17、IUM AS A PLATING MATERIAL. CONSULT LOCAL OFFICIALS IF YOU HAVE QUESTIONS CONCERNING CADMIUMS USE. /1/ MATERIAL: a. CODE LETTER F - TYPE 4140 STEEL BAR PER AMS6349 OR AMS6382 OR TYPE 4130 STEEL BAR PER AMS-S-6758 OR AMS6370 EXCEPT HEAT TREATMENT PER PROCUREMENT SPECIFICATION. b. CODE LETTER J - TYPE
18、304 CORROSION RESISTANT STEEL BAR PER AMS-QQ-S-763 OR AMS5639 EXCEPT HARDNESS PER PROCUREMENT SPECIFICATION. c. CODE LETTER K - TYPE 316 CORROSION RESISTANT STEEL BAR PER AMS-QQ-S-763 OR AMS5648 EXCEPT HARDNESS PER PROCUREMENT SPECIFICATION. d. CODE LETTER R - TYPE 321 CORROSION RESISTANT STEEL BAR
19、PER AMS-QQ-S-763 OR AMS5645 EXCEPT HARDNESS PER PROCUREMENT SPECIFICATION. e. CODE LETTER T - TYPE 6AL-4V TITANIUM ALLOY BAR PER AMS4928. f. CODE LETTER W - TYPE 7075-T73 ALUMINUM ALLOY BAR PER AMS-QQ-A-225/9; OR TYPE 7075-T7351 ALUMINUM ALLOY BAR PER AMS4124. AEROSPACE STANDARD AS6213 SHEET 3 OF 4
20、FITTING, ADAPTER, PORT, REDUCER, 37 DEGREE SPHERICAL, FLARED 2. HEAT TREATMENT: a. MATERIAL CODE LETTER F - HARDNESS SHALL BE 92 HRB TO 40 HRC PER PROCUREMENT SPECIFICATION. b. OTHER CODE LETTERS - NONE. /3/ FINISH: a. MATERIAL CODE LETTER F - CADMIUM PLATE PER AMS-QQ-P-416, TYPE II, CLASS 2, DYE BL
21、ACK. b. MATERIAL CODE LETTERS J, K, AND R - PASSIVATE PER AMS2700, TYPE 6 OR 7. c. MATERIAL CODE LETTER T - FLUORIDE PHOSPHATE CONVERSION COAT PER AMS2486 OR ANODIZE PER AMS2488 TYPE 2. d. MATERIAL CODE LETTER W: 1. ANODIZE PER AMS2472 OR MIL-A-8625, TYPE II, CLASS 2, DYE BROWN, DUPLEX SEAL PER PROC
22、UREMENT SPECIFICATION. 2. W CODE PARTS TO BE COATED WITH HIGH PURITY ALUMINUM ONLY WILL HAVE THE FINISH CODE LETTER “V” AFTER THE SIZE CODE IN THE PART NUMBER. HIGH PURITY ALUMINUM COAT PER PROCUREMENT SPECIFICATION. /4/ PROCUREMENT SPECIFICATION: AS6076 EXCEPT AS SPECIFIED ON THIS STANDARD. PRODUCT
23、 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 (QML) FOR THIS PRODUCT TYPE. THE QML IS AVAILABLE AT www.eAuditN. /5/ IDENTIFICATION AT LOCATION SHO
24、WN: MARK PER AS478 CLASS C OR D, OR METHOD 7A3, 15A3 OR 15B. a. FOR SIZE 06 AND SMALLER: MANUFACTURERS NAME, CAGE CODE OR TRADEMARK, LETTER “AS” AND MATERIAL CODE LETTER. b. FOR SIZE 08 AND LARGER: MANUFACTURERS NAME, CAGE CODE OR TRADEMARK, BASIC PART NUMBER, AND MATERIAL CODE LETTER. 6. INTENDED U
25、SE: THIS PART IS DESIGNED FOR USE IN TUBING CONNECTION SYSTEMS WITH MAXIMUM OPERATING PRESSURES AS FOLLOWS: a. SIZES 02 THROUGH 16 IN LOW ALLOY STEEL, CORROSION RESISTANT STEEL AND TITANIUM ALLOY AT 3000 PSI. b. SIZES 02 THROUGH 12 IN ALUMINUM ALLOY AT 3000 PSI. c. SIZE 16 IN ALUMINUM ALLOY AND SIZE
26、 20 IN ALL MATERIALS AT 1500 PSI. 7. THE INTERNAL DIAMETERS SHALL END IN A CONICAL END OF 115 DEGREE MINIMUM INCLUDED ANGLE. /8/ FOR REDUCER CONFIGURATIONS, THE PRESSURE RATING IS DETERMINED BY THE LARGEST PORT. /9/ THE HEX CORNERS MAY BE ROUNDED PER ARP1942. /10/ THE NON-REDUCER CONFIGURATION WITHO
27、UT A SUFFIX PART NUMBER CODE IS THE FUNCTIONAL EQUIVALENT OF AN894 AND MS24398 FOR THE CORRESPONDING FORGING SIZE AND IS INTENDED TO BE SUITABLE AS A REPLACEMENT STANDARD. 11. A CHANGE BAR (l) LOCATED IN THE LEFT MARGIN IS FOR THE CONVENIENCE OF THE USER IN LOCATING AREAS WHERE TECHNICAL REVISIONS,
28、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 EDITORI
29、AL CHANGES ONLY. /12/ WEIGHTS ARE FOR NON-REDUCERS ONLY. REDUCER FITTINGS WILL HAVE LOWER WEIGHTS. AEROSPACE STANDARD AS6213 SHEET 4 OF 4 FITTING, ADAPTER, PORT, REDUCER, 37 DEGREE SPHERICAL, FLARED 13. INTERPRETATION OF DRAWING PER ARP4296. 14. SURFACE TEXTURE: SYMBOLS PER ASME Y14.36M. REQUIREMENT
30、S PER ASME B46.1. UNLESS OTHERWISE SPECIFIED, MACHINED SURFACES TO BE 125 in Ra. SURFACES OF HEX FLATS MAY BE 250 in Ra. 15. BREAK ALL SHARP EDGES .003 TO .015 UNLESS OTHERWISE SPECIFIED. 16. DIMENSIONING AND TOLERANCING: ASME Y14.5M-1994. 17. DIMENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED, TOLERA
31、NCES: LINEAR DIMENSIONS .016, ANGULAR DIMENSIONS 0 DEGREES 30. 18. TITANIUM OR CADMIUM SHALL NOT BE USED FOR OXYGEN OR POTABLE WATER SYSTEMS. /19/ EXAMPLE OF PART NUMBER: AS6213 W 10 08 VTHE FINISH CODE LETTER “V” WILL BE PLACED HERE ONLY FOR MATERIAL CODE “W” PARTS THAT ARE TO BE COATED WITH HIGH PURITY ALUMINUM /3/MATERIAL CODE LETTER /1/ SIZE CODE, TUBE SIZE OF PORT#1 IN .062 INCREMENTS BASIC PART NUMBER SIZE CODE, TUBE SIZE OF PORT #2 IN .062 INCREMENTS
