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本文(SAE AS 6013A-2011 HOSE ASSEMBLY POLYTETRAFLUOROETHYLENE PARA ARAMID REINFORCED 275 4000 MAX PSI FLARELESS TITANIUM FITTINGS STRAIGHT TO STRAIGHT《3000 psi 275℉直通对直通的非扩口钛管接头用对位芳纶增强聚四氟乙.pdf)为本站会员(explodesoak291)主动上传,麦多课文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文库(发送邮件至master@mydoc123.com或直接QQ联系客服),我们立即给予删除!

SAE AS 6013A-2011 HOSE ASSEMBLY POLYTETRAFLUOROETHYLENE PARA ARAMID REINFORCED 275 4000 MAX PSI FLARELESS TITANIUM FITTINGS STRAIGHT TO STRAIGHT《3000 psi 275℉直通对直通的非扩口钛管接头用对位芳纶增强聚四氟乙.pdf

1、AEROSPACE STANDARD HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED, 275 F, 4000 MAX PSI, FLARELESS, TITANIUM FITTINGS, STRAIGHT TO STRAIGHT AS6013Copyright 2011 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transm

2、itted, 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: 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB

3、 ADDRESS: http:/www.sae.org ISSUED 2009-02REVISED 2011-12THIRD ANGLE PROJECTION CUSTODIAN: G-3/G-3D REV.AFEDERAL SUPPLY CLASS 4720 AS6013SHEET 1 OF 5REV.APROCUREMENT SPECIFICATION: /2/ AS5951SAE Technical Standards Board Rules provide that: “This report ispublishedby SAE toadvance thestate of techni

4、calandengineering 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 be

5、reaffirmed, revised, orcancelled. SAE invites yourwrittencomments andsuggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS6013ARATIONALE REVISE TITLE FOR 4000 PSI MAX USAGE, REMOVED /21/ FROM FIG. 1, AND CORRECTED USAGE

6、 CHARACTERISTICS, MARKING, AND PROOF PRESSURE REQUIREMENTS. FIGURE 1 - FLARELESS HOSE ASSEMBLY, STRAIGHT TO STRAIGHT FIGURE 2 - POLYESTER ABRASION SLEEVE CUFF /20/ AEROSPACE STANDARD AS6013SHEET 2 OF 5REV.AHOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED, 275 F, 4000 MAX PSI, FLARELESS

7、, TITANIUM FITTINGS, STRAIGHT TO STRAIGHT TABLE 1 - HOSE AND FITTING DIMENSIONS BASIC HOSE ASSEMBLY NO. AS6013 SIZE CODE SIZE /14/FITTING TYPE REF THREAD T PER AS8879 HOSEIDMINAMAXREF BGAGEBASICC /7/ FITTINGDIA.MIN.REF /9/D1REF /9/D2E/8/MAXREFFHEXBALLSIZEMINTHRU/7/ IN EE.250 .250 SE.4375-20UNJF-3B .

8、5625-18UNJF-3B .212.2121.922.02.2930.4120.133.133.16.16.055.055.68 .68 .56.69.120.120GGG.375 .375 .375 RSE.4375-20UNJF-3B .5625-18UNJF-3B .7500-16UNJF-3B .298.298.2982.122.162.29.2930.4120.5600.133.226.226.16.16.19.055.055.066.85 .85 .85 .56.69.88.120.203.203HHH.500 .500 .500 RSE.5625-18UNJF-3B .750

9、0-16UNJF-3B .8750-14UNJF-3B .391.391.3912.382.512.58.4120.5600.6730.226.330.330.16.19.20.055.066.066.98 .98 .98 .69.881.00.203.297.297JJJ.625 .625 .625 RSE.7500-16UNJF-3B .8750-14UNJF-3B 1.0625-12UNJF-3B .485.485.4853.023.093.34.5600.6730.8100.330.410.410.19.20.23.066.066.0661.101.101.10.881.001.25.

10、297.369.369KKK.750 .750 .750 RSE.8750-14UNJF-3B 1.0625-12UNJF-3B 1.3125-12UNJ-3B .602.602.6023.984.044.15.6730.81001.0620.410.510.510.20.23.30.066.066.0661.401.401.401.001.251.50.369.459.459MM1.000 1.000 RS1.0625-12UNJF-3B 1.3125-12UNJ-3B .852.8524.494.61.81001.0620.510.750.23.30.066.0661.801.801.25

11、1.50.459.675TABLE 2 - HOSE OR SLEEVE OUTSIDE DIAMETERS /10/ (MAXIMUM UNLESS OTHERWISE NOTED) SLEEVECODE SLEEVEMATERIAL TEMPLIMITF SIZE.250SIZE.375SIZE.500SIZE.625SIZE.750SIZE1.000 - (-) INDICATES HOSE ONLY NO SLEEVE (REF) 275 .420-.590 .525-.760 .750-.925 .870-.985 .980-1.180 1.264-1.580 G FIRESLEEV

12、E (AS1072 SIL-FG) (5 MIN) /11/ /12/ /13/ 275 .970 1.15 1.38 1.50 1.750 2.060 F ABRASION SLEEVE SHRINK-ON (POLYOLEFIN AS1073-CODE B) /18/ 275 .650 .830 .990 1.060 1.260 1.670 K INTEGRAL ABRASION SLEEVE (BRAIDED) POLYESTER 275 .495-.685 .600-.855 .825-1.020 .945-1.080 1.055-1.275 1.339-1.675 TABLE 3 -

13、 HOSE ASSEMBLY LENGTH TOLERANCES HOSE ASSEMBLY LENGTH TOLERANCE UNDER 18 in .125 in 18 TO 36 in EXCLUSIVE .250 in 36 TO 50 in EXCLUSIVE .500 in 50 in AND OVER 1% AEROSPACE STANDARD AS6013SHEET 3 OF 5REV.AHOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED, 275 F, 4000 MAX PSI, FLARELESS,

14、TITANIUM FITTINGS, STRAIGHT TO STRAIGHT TABLE 4 - WEIGHT /19/ HOSE OR SLEEVECODE HOSE, PART OR SLEEVE UNITS SIZE.250SIZE.375SIZE.500SIZE.625SIZE.750SIZE1.000 - HOSE ONLY LB/IN .010 .014 .020 .023 .032 .055 G FIRESLEEVE AS1072 (5 min PER AS1055) LB/IN .016 .019 .028 .029 .037 .041 F PROTECTIVE SLEEVE

15、, SHRINK-ON (POLYOLEFIN AS1073, CODE B) /18/ LB/IN .002 .003 .003 .003 .005 .007 NONE FIRESLEEVE CLAMP LB/EA .019 .019 .019 .024 .024 .028 NONE FITTING END (STRAIGHT) /14/ R S ELB/EALB/EALB/EA- .057.068.091.102.127.137.162.188.221.247.300.539.592.6381.038 1.084 - K ABRASION SLEEVE POLYESTER WITH HOS

16、E LB/IN .013 .017 .023 .026 .035 .058 TABLE 5 - CUFF LENGTH HOSE SIZE LENGTH (INCHES) .25 .250 2.50 .375 3.00 .500 3.75 .625 4.50 .750 5.50 1.00 6.75 NOTES: 1. MATERIALS: a. HOSE AND FITTINGS - PER AS5951. b. THE COLLARS MAY BE STAINLESS STEEL. c. SLEEVES - SEE APPLICABLE STANDARDS, TABLE 2. /2/ PRO

17、DUCT SUPPLIED TO THIS SPECIFICATION SHALL BE MANUFACTURED AND ASSEMBLED BY AN ACCREDITED MANUFACTURER OR ASSEMBLED BY AN ACCREDITED DISTRIBUTOR LISTED ON THE PRI-QPL-AS5951 FOR THIS STANDARD. SEE http:/ FOR CURRENT QPL ONLINE. 3. CONSTRUCTION AND PERFORMANCE PER AS5951. FITTINGS SHALL BE PERMANENTLY

18、 ATTACHED TO HOSE. 4. OPERATING CHARACTERISTICS PER AS5951 EXCEPT FOR USE IN HYDRAULIC SYSTEMS UP TO 4000 PSI BASED ON SWIVEL NUT “T” THREAD. /5/ MARKING: MARKING SHALL BE PER AS5951 EXCEPT OPERATING PRESSURE 4000 PSI MAX ON A STAINLESS STEEL BAND NOT OVER 1.0 IN WIDE OR ON THE COLLAR. IF A BAND IS

19、USED, IT SHALL BE LOCATED OVER THE COLLAR. THE CHARACTERS SHALL BE A MINIMUM OF .06 IN HIGH. THE BAND SHALL BE SO DESIGNED AS TO REMAIN TIGHT ON THE COLLAR TO PREVENT RELATIVE MOVEMENT AND SHALL BE OF SUFFICIENT STRENGTH TO PREVENT REMOVAL BY HAND. MARKING BAND SHALL BE COVERED WITH TRANSPARENT POLY

20、OLEFIN SHRINK SLEEVE PER AS1073 CODE A. AEROSPACE STANDARD AS6013SHEET 4 OF 5REV.AHOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED, 275 F, 4000 MAX PSI, FLARELESS, TITANIUM FITTINGS, STRAIGHT TO STRAIGHT /6/ HOSE LENGTH: LENGTH “L” IS A FOUR DIGIT NUMBER OF WHICH THE FIRST THREE DIGITS

21、 DESCRIBE THE HOSE ASSEMBLY LENGTH IN WHOLE INCHES, AND THE FOURTH DIGIT, THE FRACTION OF AN INCH IN EIGHTHS. LENGTH “L” IS MEASURED FROM “GAGE DIAMETER” TO “GAGE DIAMETER”. FOR LENGTH TOLERANCES SEE TABLE 3. TO CONVERT “GAGE DIAMETER” TO “GAGE DIAMETER” TO “END TO END” MEASUREMENT, ADD TWO TIMES “D

22、1” FOR NAS1760 END STYLES OR TWO TIMES D2 FOR AS4458 GLOBESEAL END STYLES TO LENGTH “L”. /7/ HOSE ASSEMBLY INSIDE DIAMETER SHALL BE VERIFIED BY PASSING THE DESIGNATED, OR LARGER, SPHERICAL BALL PER TABLE 1 THROUGH THE HOSE ASSEMBLY. /8/ DISTANCE ACROSS CORNERS OF COUPLING NUT, COLLAR OR NIPPLE MAY E

23、XCEED THIS DIMENSION. /9/ FITTING ENDS MUST COMPLY WITH NAS1760, AS4458 OR EQUIVALENT. DIMENSION D1 APPLIES TO NAS1760 AND D2 APPLIES TO AS4458. FITTINGS SHALL MATE WITH AS5863. COUPLING NUTS SHALL BE FUNCTIONAL EQUIVALENT TO AS4370 EXCEPT FOR WIRE GROOVE. THREADS AND WIRE GROOVE IN NUT, RETAINER WI

24、RE AND FITTING END WIRE GROOVE SHALL BE COATED WITH AS5272 TYPE 1 SOLID FILM LUBRICANT. /10/ OUTSIDE DIAMETERS: DIAMETERS ARE LISTED FOR CLAMP SELECTION. TUBULAR SLEEVES MAY NOT BE A PERFECT ROUND AND SHALL BE MEASURED WITH A DIAMETER MEASUREMENT TAPE. /11/ SLEEVE DIAMETERS: THE TABLE 2 SLEEVE DIAME

25、TERS FOR AS1072 SLEEVES APPLY WHEN THE SLEEVE IS COMPRESSED, OR CLAMPED TO CONTACT THE HOSE, IN THIS CASE, A WRINKLE MAY OCCUR OVER APPROXIMATELY 10% OF THE SLEEVE CIRCUMFERENCE. /12/ FIRESLEEVE: THE CUT ENDS OF THE FIRESLEEVE SHALL BE COATED WITH RTV SILICONE RUBBER PRIOR TO INSTALLATION TO PREVENT

26、 WICKING OF FLUIDS. THE FIRESLEEVE ENDS SHALL BE SECURED TO THE HOSE ASSEMBLY END FITTINGS WITH CORROSION RESISTANT STEEL BANDS. AFTER INSTALLATION, CRACKS OR VOIDS IN THE FIRESLEEVE, WHICH EXPOSE THE FIBERGLASS, SHALL BE COATED WITH RTV SILICONE RUBBER. /13/ IDENTIFICATION MARKING: ADD “AS1055 TYPE

27、 IIB CLASS A-S/P” TO IDENTIFICATION MARKING TO SHOW LEVEL OF COMPLIANCE, “FIRE RESISTANT 275 F (5 MIN), WITH AS1055.” /14/ JUMP SIZE CODE EXPLANATION: a. R-STEP DOWN 1 STANDARD LETTER SIZE PER TABLE 1 (REDUCED) b. S-HOSE SIZE (NO REDUCTION OR EXPANSION) c. E-STEP UP 1 STANDARD LETTER SIZE PER TABLE

28、1 (EXPANDED) NOTE: WHEN FITTING SIZE CHANGES EXIST, SPECIFY SMALLER FITTING PRIOR TO THE LARGER FITTING IN THE PART NUMBER. 15. DIMENSIONING AND TOLERANCING: ASME Y14.5M-1994. /16/ SAFETY WIRE HOLES LOCATION AND DIAMETER PER AS1043 AS FOLLOWS: a. L = TWO OR THREE HOLES PER HEX SIZE PER AS1043 b. C =

29、 NO SAFETY WIRE HOLES 17. THIS PART STANDARD TAKES PRECEDENCE OVER AS5951 IN CASES OF CONFLICT. /18/ THE SHRINK-ON POLYOLEFIN SLEEVE SHALL COVER THE ENTIRE HOSE AND A MINIMUM OF 50% OF THE COLLARS ON BOTH ENDS OF THE ASSEMBLY. AEROSPACE STANDARD AS6013SHEET 5 OF 5REV.AHOSE ASSEMBLY, POLYTETRAFLUOROE

30、THYLENE, PARA ARAMID REINFORCED, 275 F, 4000 MAX PSI, FLARELESS, TITANIUM FITTINGS, STRAIGHT TO STRAIGHT /19/ FITTING WEIGHTS ARE REFERENCE AND BULK HOSE AND SLEEVE WEIGHTS ARE MAXIMUM. /20/ THE INTEGRAL POLYESTER ABRASION SLEEVE, CODE K, SHALL HAVE A SUPPORT CUFF IN ACCORDANCE WITH FIGURE 2. THE CU

31、FF MAY BE CONTOURED AND HAVE A MINIMUM THICKNESS OF .10 INCHES. THE CUFF SHALL BE ADHERED TO THE FITTING COLLAR/SOCKET AND HOSE. THE CUFF MATERIAL SHALL BE A SILICONE MATERIAL THAT IS COMPATIBLE WITH AIRCRAFT FLUIDS. 21. THE ACCEPTANCE TEST PROOF PRESSURE SHALL BE 8000 PSI. 22. A CHANGE BAR (|) LOCA

32、TED 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 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.23. EXAMPLE OF PART NUMBER:

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