1、 AEROSPACE STANDARD NUT, COUPLING, RIGID, FIXED CAVITY, THREADED, FERRULE TYPE TUBE ENDS, TYPE II AS1735Copyright 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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4、r any particularuse, includingany patent infringement arising therefrom,is the soleresponsibility of theuser.”SAE reviewseachtechnical reportatleasteveryfiveyearsatwhichtimeitmayberevised,reaffirmed,stabilized,orcancelled. SAEinvites yourwritten comments andsuggestions.RATIONALE AS1735D HAS BEEN REA
5、FFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY. AS1735 SHEET 1 OF 4 REV. D PROCUREMENT SPECIFICATION: /3/ AS1730 SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AS1735D FIGURE 1 - NUT AEROSPACE STANDARD AS1735 SHEET 2 OF
6、 4REV. D NUT, COUPLING, RIGID, FIXED CAVITY, THREADED, FERRULE TYPE TUBE ENDS, TYPE II TABLE 1 - NUT DIMENSIONS BASIC NO. AS1735 SIZE CODE /15/ (TUBE SIZE) THREAD T PER FED-STD-H28/2 OR ASME B1.1 /10/ MOD A B PL C +.005 -.000 D D TOL 04 05 06 08 10 12 16 20 24 28 32 36 40 44 48 56 64 72 80 .250 .312
7、 .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-2B .750-12 UN-2B .812-12 UN-2B .937-12 UN-2B 1.062-12 UN-2B 1.250-12 UNF-2B 1.500-12 UNF-2B 1.750-12 UN-2B 2.000-12 UN-2B 2.250-12 UN-2B 2.500-12 UN-2B 2.750-12 UN-2B 3.000-12 UN-2B 3.250-12
8、 UN-2B 3.625-12 UN-2B 4.125-12 UN-2B/ 4.625-12 UNS-2B/10/ 5.125-12 UNS-2B/10/ 5.625-12 UNS-2B/10/ .187 .187 .187 .187 .187 .187 .187 .187 .250 .250 .250 .250 .250 .250 .250 .250 .250 .250 .250 4 4 4 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 .529 .580 .635 .762 .900 1.033 1.284 1.534 1.783 2.045 2.292 2.549 2.
9、800 3.045 3.395 3.895 4.395 4.895 5.378 .583 .644 .689 .815 .960 1.128 1.386 1.628 1.878 2.138 2.382 2.638 2.888 3.138 3.513 4.013 4.513 5.015 5.500 +.002/-.000 +.002/-.000 +.002/-.000 +.003/-.000 +.003/-.000 +.003/-.000 +.003/-.000 +.003/-.000 +.003/-.000 +.003/-.000 +.003/-.000 +.003/-.000 +.003/-
10、.000 +.003/-.000 +.004/-.000 +.004/-.000 +.004/-.000 +.005/-.000 +.005/-.000 TABLE 2 - NUT DIMENSIONS AND WEIGHTS BASIC NO. AS1735 SIZE CODE /15/ E +.010 -.000 /11/ F +010 -.000 G MAX H +.010 -.000 J .015 K L MAX 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 .
11、691 .753 .816 .941 1.066 1.253 1.503 1.753 2.003 2.253 2.503 2.753 3.003 3.253 3.628 4.128 4.613 5.113 5.613 .787 .850 .912 1.037 1.172 1.360 1.610 1.860 2.110 2.360 2.620 2.870 3.125 3.370 3.751 4.256 4.756 5.266 5.765 .829 .892 .954 1.079 1.214 1.402 1.652 1.902 2.152 2.402 2.662 2.912 3.162 3.412
12、 3.793 4.298 4.798 5.308 5.807 .338 .338 .338 .338 .354 .354 .354 .414 .429 .429 .429 .455 .455 .455 .455 .455 .455 .543 .543 .065 .065 .065 .065 .065 .065 .065 .065 .065 .065 .065 .100 .100 .100 .100 .100 .100 .130 .130 .300 .300 .300 .300 .315 .315 .315 .375 .375 .375 .375 .392 .392 .392 .392 .392
13、 .392 .475 .475 .553 .553 .553 .553 .569 .569 .569 .629 .644 .644 .644 .705 .705 .705 .705 .705 .705 .823 .823 .009 .010 .011 .013 .016 .019 .023 .030 .035 .039 .046 .058 .063 .068 .079 .092 .104 .144 .161 AEROSPACE STANDARD AS1735 SHEET 3 OF 4REV. D NUT, COUPLING, RIGID, FIXED CAVITY, THREADED, FER
14、RULE TYPE TUBE ENDS, TYPE II NOTES: 1. MATERIAL CODE D: a. ALUMINUM ALLOY 2024-T6, 2024-T851, OR 2024-T8511 PER AMS-QQ-A-225/6, ASTM B 210, AMS-QQ-A-200/3, OR AMS-WW-T-700/3. b. ALUMINUM ALLOY 2014-T6 PER AMS-QQ-A-225/4 OR AMS-QQ-A-200/2. 2. FINISH: MATERIAL CODE D: ANODIZE PER MIL-A-8625, TYPE II,
15、CLASS 2, COLOR MAGENTA. /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 STANDARD. SEE . FOR CURRENT QPL ON-LINE. /4/ IDENTIFICATION PER AS478 METHOD 30
16、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 TAG PER AS478 METHOD 35D CONTAINING THIS INFORMATION. ALL PARTS SHALL BE MARK
17、ED 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 COMPATIBILITY WITH THE ASSEMBLY AND COMPLIANCE WITH THE PERFORMANCE REQUIREMENTS OF A
18、S1730. /6/ KNURL MAY BE MEDIUM DIAMOND, MEDIUM PLAIN SPIRAL, OR FINE STRAIGHT. 7. LUBRICATION: THREADS SHALL BE COATED WITH SOLID FILM LUBRICANT TO A THICKNESS OF .0003 TO .0005 PER AS5272 TYPE I (MIL-L-46010 HAS BEEN SUPERSEDED BY MIL-PRF-46010) OVERSPRAY ALLOWED. 8. SURFACE TEXTURE: SYMBOLS PER AS
19、ME Y14.36M; REQUIREMENTS PER ASME Y14.36. UNLESS OTHERWISE SPECIFIED, MACHINED SURFACES TO BE 125 in Ra. 9. DIMENSIONING AND TOLERANCING: ASME Y14.5M-1994. /10/ NUT SIZES 64, 72, AND 80 HAVE THREADS WITH REDUCED PITCH DIAMETERS AS FOLLOWS: a. 64: 4.5559 +.0087/-.0000 b. 72: 5.0559 +.0087/-.0000 c. 8
20、0: 5.5559 +.0090/-.0000 /11/ NO THREAD MARKS ON DIAMETER “E”. THREAD MARKS IN .040/.065 RADIUS ADJACENT TO THE 15 DEGREE THREAD CHAMFER IS ACCEPTABLE. 12. INVENTORIED PARTS CONFORMING TO THE PREVIOUS REVISION MAYBE USED TO DEPLETION. 13. DIMENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED, TOLERANCES:
21、LINEAR DIMENSIONS .010, ANGULAR DIMENSIONS 2 DEGREES. 14. BREAK EDGES .003 TO .015 UNLESS OTHERWISE SPECIFIED. AEROSPACE STANDARD AS1735 SHEET 4 OF 4REV. D NUT, COUPLING, RIGID, FIXED CAVITY, THREADED, FERRULE TYPE TUBE ENDS, TYPE II /15/ EXAMPLE OF PART NUMBER: AS1735 D 16 BASIC NUT NUMBER NUT SIZE
22、 IN .062 in INCREMENTS (16 = 1 in TUBE SIZE) NUT MATERIAL CODE (D = ALUMINUM ALLOY) 16. 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 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.
