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    SAE AS 6015A-2011 HOSE ASSEMBLY POLYTETRAFLUOROETHYLENE PARA ARAMID REINFORCED 275 4000 PSI MAX FLARELESS TITANIUM FITTINGS STRAIGHT TO 90 DEGREE《4000 psi 275 ℉直通对90弯头的非扩口钛管接头用对位芳纶增强聚.pdf

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    SAE AS 6015A-2011 HOSE ASSEMBLY POLYTETRAFLUOROETHYLENE PARA ARAMID REINFORCED 275 4000 PSI MAX FLARELESS TITANIUM FITTINGS STRAIGHT TO 90 DEGREE《4000 psi 275 ℉直通对90弯头的非扩口钛管接头用对位芳纶增强聚.pdf

    1、AEROSPACE STANDARD HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARAARAMID REINFORCED, 275 F, 4000 PSI MAX, FLARELESS, TITANIUM FITTINGS, STRAIGHT TO 90 DEGREE AS6015Copyright 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 AS6015SHEET 1 OF 5REV.APROCUREMENT SPECIFICATION: /2/ AS5951SAE Technical Standards Board Rules provide that: “This report ispublishedby SAE toadvance thestate of techn

    4、icalandengineering 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 b

    5、ereaffirmed, revised, orcancelled. SAE invites yourwrittencomments andsuggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS6015ARATIONALE REVISE TITLE FOR 4000 PSI MAX USAGE, REMOVED /21/ FROM FIG. 1, AND CORRECTED USAG

    6、E CHARACTERISTICS, MARKING, AND PROOF PRESSURE REQUIREMENTS. FIGURE 1 - FLARELESS HOSE ASSEMBLY, STRAIGHT TO 90 DEGREE ELBOW FIGURE 2 - POLYESTER ABRASION SLEEVE CUFF /20/ AEROSPACE STANDARD AS6015SHEET 2 OF 5REV.AHOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED, 275 F, 4000 PSI MAX, F

    7、LARELESS, TITANIUM FITTINGS, STRAIGHT TO 90 DEGREE TABLE 1 - HOSE AND FITTING DIMENSIONS BASIC HOSE ASSEMBLY NO. AS6015 SIZE CODE SIZE /14/ FITTING TYPE REF THREAD T PER AS8879 HOSEIDMIN A1 MAXA2 MAXREF BGAGE BASICC /7/ FITTING DIA. MIN.REF/9/ D1 REF/9/ D2 E/8/ MAXREFFHEXGMIN GMAX STRAIGHTFITTING BA

    8、LL SIZE MIN THRU /7/ INELBOW FITTING BALL SIZE MIN THRU /7/INEE.250 .250 SE.4375-20UNJF-3B .5625-18UNJF-3B .212 .212 1.92 2.02 2.06 2.12 .2930.4120.133 .133 .16 .16 .055.055.68 .68 .56 .69.74 .81 .87 .94 .120 .120 .113 .113 GGG.375 .375 .375 RSE.4375-20UNJF-3B .5625-18UNJF-3B .7500-16UNJF-3B .298 .2

    9、98 .298 2.12 2.16 2.29 2.35 2.35 2.49 .2930.4120.5600.133 .226 .226 .16 .16 .19 .055.055.066.85 .85 .85 .56 .69 .88.74 .81 .99 .87 .94 1.12 .120 .203 .203 .113 .192 .192 HHH.500 .500 .500 RSE.5625-18UNJF-3B .7500-16UNJF-3B .8750-14UNJF-3B .391 .391 .391 2.38 2.51 2.58 2.58 2.58 2.65 .4120.5600.6730.

    10、226 .330 .330 .16 .19 .20 .055.066.066.98 .98 .98 .69 .88 1.00.81 .99 1.14 .94 1.12 1.34 .203 .297 .297 .192 .281 .281 JJJ.625 .625 .625 RSE.7500-16UNJF-3B .8750-14UNJF-3B 1.0625-12UNJF-3B .485 .485 .485 3.02 3.09 3.34 3.16 3.16 3.28 .5600.6730.8100.330 .410 .410 .19 .20 .23 .066.066.0661.10 1.10 1.

    11、10 .88 1.00 1.25.99 1.14 1.33 1.12 1.34 1.55 .297 .369 .369 .281 .349 .349 KKK.750 .750 .750 RSE.8750-14UNJF-3B 1.0625-12UNJF-3B 1.3125-12UNJ-3B .602 .602 .602 3.98 4.04 4.15 4.15 4.15 4.58 .6730.81001.0620.410 .510 .510 .20 .23 .30 .066.066.0661.40 1.40 1.40 1.00 1.25 1.501.14 1.33 1.57 1.34 1.55 1

    12、.77 .369 .459 .459 .349 .434 .434 MM1.000 1.000 RS1.0625-12UNJF-3B 1.3125-12UNJ-3B .852 .852 4.49 4.61 4.83 5.00 .81001.0620.510 .750 .23 .30 .066.0661.80 1.80 1.25 1.501.33 1.57 1.55 1.77 .459 .675 .434 .638 TABLE 2 - HOSE OR SLEEVE OUTSIDE DIAMETERS /10/ (DIAMETERS ARE MAXIMUM UNLESS OTHERWISE NOT

    13、ED) 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 1.264-1.580G FIRESLEEVE (AS1072 SIL-FG) (5 MIN) /11/ /12/ /13/ 275 .970 1.150 1.380 1.500 1.750 2.060 F ABRASION

    14、 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 1.339-1.675TABLE 3 - HOSE ASSEMBLY LENGTH TOLERANCES HOSE ASSEMBLY LENGTH TOLERANCE UNDER 18 in .125 in 18 TO

    15、 36 in EXCLUSIVE .250 in 36 TO 50 in EXCLUSIVE .500 in 50 in AND OVER 1% AEROSPACE STANDARD AS6015SHEET 3 OF 5REV.AHOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED, 275 F, 4000 PSI MAX, FLARELESS, TITANIUM FITTINGS, STRAIGHT TO 90 DEGREE TABLE 4 - WEIGHTS /19/ HOSE OR SLEEVECODE HOSE,

    16、PART OR SLEEVE UNITSSIZE.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, SHRINK-ON (POLYOLEFIN AS1073, CODE B) /18/LB/IN .002 .003 .003 .003 .005 .007 NONE FIR

    17、ESLEEVE CLAMP LB/EA .019 .019 .019 .024 .024 .028 NONE FITTING END (STRAIGHT) /14/ R S E LB/EALB/EALB/EA.057.068.091.102.127.137.162.188.221.247.300.539.592.6381.038 1.084 NONE FITTING END (90 DEGREE) /14/ R S E LB/EALB/EALB/EA.072.095.118.129.163.173.198.241.274.300.426.665.718.8911.291 1.337 K ABR

    18、ASION SLEEVE POLYESTER WITH HOSE 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 APPLICA

    19、BLE STANDARDS, TABLE 2. /2/ PRODUCT 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

    20、. FITTINGS SHALL BE PERMANENTLY ATTACHED TO HOSE. 4. OPERATING CHARACTERISTICS PER AS5951EXCEPT FOR USE IN HYDRAULIC SYSTEMS UP TO 4000 PSI. BASED ON SWIVEL NUT “T” THREAD AEROSPACE STANDARD AS6015SHEET 4 OF 5REV.AHOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED, 275 F, 4000 PSI MAX, F

    21、LARELESS, TITANIUM FITTINGS, STRAIGHT TO 90 DEGREE /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 USED, IT SHALL BE LOCATED OVER THE COLLAR. THE CHARACTERS SHALL BE A MINIMUM OF .06 IN HIGH

    22、. 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 POLYOLEFIN SHRINK SLEEVE PER AS1073 CODE A. /6/ HOSE LENGTH: LENGTH “L” IS A FOUR DIGIT NUMBER

    23、OF WHICH THE FIRST THREE DIGITS 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

    24、” MEASUREMENT, ADD D1 TO LENGTH “L” FOR NAS1760 END STYLES OR D2 TO LENGTH “L” FOR AS4458 GLOBESEAL END STYLES. /7/ HOSE FITTING 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,

    25、COLLAR OR NIPPLE MAY EXCEED 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 GROO

    26、VE IN NUT, RETAINER WIRE 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: TH

    27、E TABLE 2 SLEEVE DIAMETERS 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 I

    28、NSTALLATION TO PREVENT 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 MAR

    29、KING: ADD “AS1055 TYPE 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

    30、LETTER SIZE PER TABLE 1 (EXPANDED) NOTE: SPECIFY STRAIGHT FITTING SIZE FOLLOWED BY THE ELBOW FITTING SIZE 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

    31、 = NO SAFETY WIRE HOLES 17. THIS PART STANDARD TAKES PRECEDENCE OVER AS5951 IN CASES OF CONFLICT. AEROSPACE STANDARD AS6015SHEET 5 OF 5REV.AHOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED, 275 F, 4000 PSI MAX, FLARELESS, TITANIUM FITTINGS, STRAIGHT TO 90 DEGREE /18/ THE SHRINK-ON POLY

    32、OLEFIN SLEEVE SHALL COVER THE ENTIRE HOSE AND A MINIMUM OF 50% OF THE COLLARS ON BOTH ENDS OF THE ASSEMBLY. /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

    33、 CUFF 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 (|) LO

    34、CATED 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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