1、 AEROSPACE STANDARD BODY, COUPLING, RIGID, FIXED CAVITY, THREADED, FERRULE TYPE TUBE ENDS, TYPE I AS1732Copyright 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, mechanica
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3、05REAFFIRMED 2015-01THIRD ANGLE PROJECTION CUSTODIAN: G-3/G-3A REV.EFEDERAL SUPPLY CLASS 4730 SAETechnicalStandardsBoard Rulesprovidethat:“Thisreportispublished bySAEto advance the state oftechnicaland engineering sciences.The use ofthisreportisentirelyvoluntary,anditsapplicabilityandsuitabilityfora
4、nyparticularuse,includinganypatentinfringementarising therefrom,isthe sole responsibilityoftheuser.”SAEreviewseachtechnicalreportatleasteveryfiveyearsatwhich time itmaybe revised,reaffirmed,stabilized,orcancelled.SAEinvitesyourwritten commentsandsuggestions.RATIONALE AS1732E HAS BEEN REAFFIRMED TO C
5、OMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY. AS1732 SHEET 1 OF 4 REV. E PROCUREMENT SPECIFICATION: /3/ AS1730 SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AS1732E FIGURE 1 BODY AEROSPACE STANDARD AS1732 SHEET 2 OF 4 REV. E BOD
6、Y, COUPLING, RIGID, FIXED CAVITY, THREADED, FERRULE TYPE TUBE ENDS, TYPE I TABLE 1 - COUPLING BODY DIMENSIONS BASIC NO. AS1732 SIZE CODE /14/ (TUBE SIZE) THREAD T PER FED-STD-H28/2 OR ASME B1.1 /10/ MOD A +.005 -.000 B +.005 -.000 C +.010 -.000 D +.000 -.010 E +.005 -.000 F +.005 -.000 G G TOL H 04
7、05 06 08 10 12 16 20 24 28 32 36 40 44 48 56 64 72 80 .250 .312 .375 .500 .625 .750 1.000 1.250 1.500 1.750 2.000 2.250 2.500 2.750 3.000 3.500 4.000 4.500 5.000 .687-12 UN-2A .750-12 UN-2A .812-12 UN-2A .937-12 UN-2A 1.062-12 UN-2A 1.250-12 UNF-2A 1.500-12 UNF-2A 1.750-12 UN-2A 2.000-12 UN-2A 2.250
8、12 UN-2A 2.500-12 UN-2A 2.750-12 UN-2A 3.000-12 UN-2A 3.250-12 UN-2A 3.625-12 UN-2A 4.125-12 UN-2A 4.625-12 UNS-2A /10/ 5.125-12 UNS-2A /10/ 5.625-12 UNS-2A /10/ .680 .743 .805 .930 1.055 1.243 1.493 1.743 1.993 2.243 2.493 2.743 2.993 3.243 3.618 4.118 4.603 5.103 5.602 .529 .580 .635 .762 .900 1.
9、033 1.284 1.534 1.783 2.045 2.292 2.545 2.800 3.045 3.395 3.895 4.395 4.895 5.378 .480 .535 .590 .716 .850 .984 1.235 1.485 1.735 1.965 2.235 2.485 2.713 2.961 3.340 3.840 4.340 4.840 5.325 .298 .353 .408 .534 .668 .802 1.053 1.303 1.553 1.783 2.053 2.283 2.531 2.781 3.158 3.658 4.158 4.658 5.143 .2
10、33 .295 .358 .483 .609 .734 .984 1.235 1.480 1.730 1.981 2.231 2.481 2.731 2.979 3.479 3.979 4.479 4.979 .375 .437 .500 .625 .750 .890 1.142 1.392 1.642 1.895 2.145 2.395 2.645 2.895 3.145 3.645 4.155 4.655 5.155 .254 .316 .379 .504 .630 .755 1.005 1.256 1.506 1.756 2.006 2.257 2.507 2.757 3.007 3.5
11、09 4.009 4.509 5.009 +.005/-.000 +.005/-.000 +.005/-.000 +.005/-.000 +.005/-.000 +.005/-.000 +.005/-.000 +.005/-.000 +.005/-.000 +.005/-.000 +.005/-.000 +.005/-.000 +.005/-.000 +.005/-.000 +.005/-.000 +.005/-.000 +.005/-.000 +.006/-.000 +.006/-.000 .645 .645 .645 .645 .675 .675 .675 .675 .760 .760 .
12、760 .760 .760 .760 .705 .705 .705 .884 .868 AEROSPACE STANDARD AS1732 SHEET 3 OF 4 REV. E BODY, COUPLING, RIGID, FIXED CAVITY, THREADED, FERRULE TYPE TUBE ENDS, TYPE I TABLE 2 - COUPLING BODY DIMENSIONS AND DESIGN INFORMATION BASIC NO. AS1732 SIZE CODE /14/ J K LENGTH K TOL M N PLACES P PLACES S LEN
13、GTH S TOL W O-RINGS DASH NO. /11/ ALUM WEIGHT LB/EA APPROX REF 04 05 06 08 10 12 16 20 24 28 32 36 40 44 48 56 64 72 80 .234 .234 .234 .234 .250 .250 .250 .250 .250 .250 .250 .279 .279 .279 .309 .309 .309 .409 .409 .090 .090 .090 .090 .100 .100 .100 .100 .100 .100 .105 .110 .110 .110 .060 .060 .100
14、100 .100 +.005/-.000 +.005/-.000 +.005/-.000 +.005/-.000 .010 .010 .010 .010 .010 .010 .010 .010 .010 .010 .010 .010 .010 .010 .010 .045 .045 .045 .045 .045 .045 .045 .045 .045 .075 .075 .075 .075 .075 .075 .075 .075 .075 .075 4 4 4 4 4 4 4 4 5 5 5 5 5 5 5 5 4 6 6 5 5 5 5 5 5 5 5 6 6 6 6 6 6 6 6 5
15、7 7 .127 .127 .127 .127 .150 .150 .150 .150 .150 .125 .125 .125 .125 .125 .125 .125 .142 .151 .135 +.020/-.010 +.020/-.010 +.020/-.010 +.020/-.010 .015 .015 .015 .015 .015 +.020/-.010 +.020/-.010 +.020/-.010 +.020/-.010 +.020/-.010 +.020/-.010 +.020/-.010 .015 +.020/-.010 +.020/-.010 .008-.010 .008-
16、010 .008-.010 .008-.010 .008-.010 .008-.010 .008-.010 .008-.010 .008-.010 .008-.010 .008-.010 .008-.010 .008-.010 .008-.010 .008-.010 .014-.016 .014-.016 .020-.024 .020-.024 012 013 014 016 018 020 024 028 030 032 034 036 038 040 042 044 046 048 050 .007 .008 .010 .013 .016 .021 .027 .033 .041 .045
17、 .050 .058 .064 .071 .094 .106 .120 .178 .196 AEROSPACE STANDARD AS1732 SHEET 4 OF 4 REV. E BODY, COUPLING, RIGID, FIXED CAVITY, THREADED, FERRULE TYPE TUBE ENDS, TYPE I NOTES: 1. MATERIAL CODE D: ALUMINUM ALLOY 2024-T6, 2024-T851, OR 2024-T8511 PER AMS-QQ-A-225/6, ASTM B 210, AMS-WW-T-700/3, OR AMS
18、QQ-A-200/3. 2. FINISH: MATERIAL CODE D: ANODIZE PER MIL-A-8625, TYPE II, CLASS 2, COLOR MAGENTA. /6/ /3/ PRODUCT SUPPLIED TO THIS SPECIFICATION SHALL BE MANUFACTURED BY AN ACCREDITED MANUFACTURER LISTED IN THE PERFORMANCE REVIEW INSTITUTE (PRI) QUALIFIED PRODUCTS LIST FOR PRI-QPL-AS1730 FOR THIS ST
19、ANDARD. SEE . FOR CURRENT QPL ON-LINE. /4/ IDENTIFICATION PER AS478 METHOD 30 INCLUDING THE MANUFACTURERS NAME, TRADEMARK, OR CAGE CODE, COMPLETE “AS“ PART NUMBER, AND DATE OF MANUFACTURE IN QUARTERS (3Q95 = THIRD QUARTER 1995). SIZES 12 AND SMALLER MAY BE INDIVIDUALLY PLACED IN A PLASTIC BAG WITH A
20、 TAG PER AS478 METHOD 35D CONTAINING THIS INFORMATION. ALL PARTS SHALL BE MARKED AS A MINIMUM WITH THE MANUFACTURES NAME, TRADEMARK OR CAGE CODE AND DATE OF MANUFACTURE. /5/ THE MANUFACTURER WILL SPECIFY AND CONTROL CERTAIN SPECIFIC DIMENSIONS AND TOLERANCES AND WILL BE RESPONSIBLE TO ASSURE COMPATI
21、BILITY WITH THE ASSEMBLY AND COMPLIANCE WITH THE PERFORMANCE REQUIREMENTS OF AS1730. /6/ SURFACES NOTED FINISHED WITH CHEMICAL CONVERSION COATING PER MIL-DTL-5541, TYPE 1, CLASS 3. 7. SURFACE TEXTURE: SYMBOLS PER ASME Y14.36M; REQUIREMENTS PER ASME B46.1. UNLESS OTHERWISE SPECIFIED, MACHINED SURFACE
22、S TO BE 125 in Ra. 8. DIMENSIONING AND TOLERANCING: ASME Y14.5M-1994. 9. DIMENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED, TOLERANCES: LINEAR DIMENSIONS .010, ANGULAR DIMENSIONS 2 DEGREES. /10/ BODY SIZES 64, 72, AND 80 HAVE THREADS WITH REDUCED PITCH DIAMETERS AS FOLLOWS: a. 64: 4.5539 +.0000/-.006
23、7 b. 72: 5.0539 +.0000/-.0067 c. 80: 5.5538 +.0000/-.0069 /11/ SIZE NUMBERS FOR O-RING SEALS ARE SELECTED FROM AS568. /12/ GROOVE WIDTH IS SPECIFIED AND CONTROLLED BY THE MANUFACTURER BUT WITH THE VARIANCE BETWEEN GROOVE WIDTHS NOT EXCEEDING .015. 13. BREAK EDGES .003 TO .015 UNLESS OTHERWISE SPECIF
24、IED. /14/ EXAMPLE OF PART NUMBER: AS1732 D 16 BASIC COUPLING BODY COUPLING BODY SIZE IN .062 in INCREMENTS NUMBER (16 = 1 in TUBE SIZE) COUPLING BODY MATERIAL CODE (D = ALUMINUM ALLOY) 15. A CHANGE BAR (I) LOCATED IN THE LEFT MARGIN IS FOR THE CONVENIENCE OF THE USER IN LOCATED AREAS WHERE TECHNICAL
25、 REVISIONS, NOT EDITORIAL CHANGES, HAVE BEEN MADE TO 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. CHANGES BARS AND (R) ARE NOT USED IN ORIGINAL PUBLICATIONS, NOR IN DOCUMENTS THAT CONTAIN EDITORIAL CHANGES ONLY.
