1、AEROSPACE STANDARD FITTING, REDUCER, INTEGRAL WELD RING, 3000 PSI AS1585Copyright 2013 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 o
2、therwise, 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 1980-02REAFFIRMED 2004-07 REVISED 2013-10THIRD ANGL
3、E PROJECTION CUSTODIAN: G-3/G-3B REV.FFEDERAL SUPPLY CLASS 4730 AS1585SHEET 1 OF 3REV. FPROCUREMENT SPECIFICATION: AS1576 /6/SAE Technical Standards Board Rules provide that: “This report ispublishedby SAE toadvance thestate of technicalandengineering sciences. Theuse ofthis report is entirely volun
4、tary, 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, reaffirmed, stabilized, orcancelled. SAE invites yourwrit
5、tencomments andsuggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS1585FRATIONALE REVISE ACTIVATION DATES FOR PRI-QPL-AS1576. FIGURE 1 - FITTING, WELD RING TABLE 1 - DIMENSIONS AND WEIGHTS BASIC NO. AS1585/15/SIZE CODE
6、 NOMINAL TUBE SIZEPORT #1 NOMINAL TUBE SIZEPORT #2 A.016 B C D1.005 D2.005 T1 T2 LB/EAAPPROX. REF STEELLB/EAAPPROX. REF TI0406 .250 .375 2.632 2.702 1.218 .200 .305 .026 .036 .0226 .0128 0408 .250 .500 2.668 2.748 1.179 .200 .430 .026 .036 .0325 .0184 0608 .375 .500 2.632 2.712 1.218 .305 .430 .036
7、.036 .0364 .0206 0610 .375 .625 2.668 2.748 1.179 .305 .545 .036 .041 .0501 .0283 0810 .500 .625 2.632 2.722 1.218 .430 .545 .036 .041 .0518 .0293 0812 .500 .750 2.668 2.768 1.179 .430 .650 .036 .051 .0717 .0406 1012 .625 .750 2.632 2.732 1.218 .545 .650 .041 .051 .0746 .0422 1016 .625 1.000 2.704 2
8、.814 1.140 .545 .880 .041 .061 .119 .0674 1216 .750 1.000 2.668 2.788 1.179 .650 .880 .051 .061 .124 .0701 1220 .750 1.250 2.740 2.870 1.102 .650 1.110 .051 .071 .183 .103 1620 1.000 1.250 2.668 2.808 1.179 .880 1.110 .061 .071 .187 .106 AEROSPACE STANDARD AS1585SHEET 2 OF 3REV. FFITTING, REDUCER, I
9、NTEGRAL WELD RING, 3000 PSI NOTES: /1/ MATERIAL: a. CODE LETTER T - TYPE 6AL-4V TITANIUM ALLOY BAR PER AMS4928. b. CODE LETTER V - TYPE 15-5PH CORROSION RESISTANT STEEL BAR PER AMS5659. 2. HEAT TREATMENT: a. MATERIAL CODE LETTER T - NONE. b. MATERIAL CODE LETTER V - HEAT TREAT TO CONDITION H 1075 PE
10、R AMS2759/3. 3. FINISH: NONE. /4/ CLEANING: a. NO SUFFIX CODE LETTER IN PART NUMBER - CLEAN BY ANY SUITABLE METHOD PER PROCUREMENT SPECIFICATION. b. SUFFIX CODE LETTER “C” IN PART NUMBER - HOT ALKALINE CLEAN PER PROCUREMENT SPECIFICATION. c. SUFFIX CODE LETTER “E” IN PART NUMBER FOR TITANIUM PARTS O
11、NLY - NITRIC-HYDROFLUORIC ACID ETCH PER PROCUREMENT SPECIFICATION. 5. PACKAGING: PER PROCUREMENT SPECIFICATION. /6/ PROCUREMENT SPECIFICATION: AS1576 UNLESS OTHERWISE SPECIFIED ON THIS STANDARD. PRODUCT SUPPLIED TO THIS SPECIFICATION SHALL BE MANUFACTURED BY AN ACCREDITED MANUFACTURER AS LISTED IN T
12、HE PERFORMANCE REVIEW INSTITUTE (PRI) QUALIFIED PRODUCTS LIST PRI-QPL-AS1576 FOR THIS STANDARD. SEE www.eAuditN FOR CURRENT QPL ONLINE. THIS QPL REQUIREMENT SHALL BE IN EFFECT FOR PURCHASE ORDERS PLACED ON OR AFTER JULY 1, 2014. SUPPLIERS SEEKING LISTING ON THE INITIAL QPL MUST APPLY TO PRI FOR APPR
13、OVAL NO LATER THAN JANUARY 1, 2014. UNTIL THE QPL IS IN EFFECT, USERS OF THIS STANDARD ARE ADVISED TO CONTROL SOURCE APPROVALS. TRANSITION TO PRI-QPL SHALL BE COMPLETED BY JULY 1, 2014. /7/ IDENTIFICATION AT LOCATION SHOWN: MARK PER AS478 METHOD 3B, 5B1, 5B2, 7A2, 7A3, 7C2, 15A3, OR 15B MANUFACTURER
14、S IDENTIFICATION, CAGE CODE NUMBER OR TRADEMARK, BASIC PART NUMBER FOR SIZE 08 AND LARGER, LETTERS “AS” FOR SIZE 06 AND SMALLER AND MATERIAL CODE LETTER. 8. THIS PART IS DESIGNED FOR USE IN SYSTEMS WITH MAXIMUM OPERATING PRESSURE OF 3000 PSI WHEN ORBITAL ARC WELDED TO TITANIUM ALLOY OR CORROSION RES
15、ISTANT STEEL TUBING. 9. 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 OF THE DOCUMENT TITLE INDICATES A COMPLETE REVIS
16、ION OF THE DOCUMENT, INCLUDING TECHNICAL REVISIONS. CHANGE BARS AND (R) ARE NOT USED IN ORIGINAL PUBLICATIONS, NOR IN DOCUMENTS THAT CONTAIN EDITORIAL CHANGES ONLY. 11. INTERPRETATION OF DRAWING PER ARP4296. 11. SURFACE TEXTURE: SYMBOLS PER ASME Y14.36M. REQUIREMENTS PER ASME B46.1. UNLESS OTHERWISE
17、 SPECIFIED, MACHINED SURFACES TO BE 125 MICROINCHES Ra. 12. BREAK EDGES .003 TO .015 UNLESS OTHERWISE SPECIFIED. AEROSPACE STANDARD AS1585SHEET 3 OF 3REV. FFITTING, REDUCER, INTEGRAL WELD RING, 3000 PSI 13. DIMENSIONING AND TOLERANCING: ASME Y14.5M-1994. 14. DIMENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED, TOLERANCES: LINEAR DIMENSIONS: .010, ANGULAR DIMENSIONS 0 DEGREES 30 MINUTES. /15/ EXAMPLE OF PART NUMBER:
