SAE AS 85049 52C-2011 Connector Accessories Electrical Strain Relief Nonenvironmental Self-Locking and Non-self-Locking Straight Category 4B (for AS50151 Crimp MIL-DTL-26482 series.pdf

1、AEROSPACE STANDARD CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, NONENVIRONMENTAL, SELF-LOCKING AND NON-SELF-LOCKING, STRAIGHT, CATEGORY 4B (FOR AS50151 CRIMP, MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, AND MIL-DTL-83723 SERIES III CONNECTORS) AS85049/52Copyright 2011 SAE International All rights

2、 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 otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and

3、 Canada) Tel: 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org ISSUED 1998-08REVISED 2011-01THIRD ANGLE PROJECTION CUSTODIAN: AE-8/AE-8C1 REV.CFEDERAL SUPPLY CLASS 5935 AS85049/52SHEET 1 OF 5REV. CPROCUREMENT SPECIFICATION: AS85049SAE Tech

4、nicalStandards Board Rules provide that: “This report ispublishedbySAE toadvance thestate of technicalandengineering sciences. Theuse of this report is entirely voluntary, andits applicability andsuitability forany particular use,including any patent infringement arising therefrom, isthe solerespons

5、ibilityof the user.”SAE reviews eachtechnicalreport at least every five years at which time it may bereaffirmed, revised, orcancelled. SAE invites yourwritten comments andsuggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standar

6、ds/AS85049/52CRATIONALE REVISED TO CORRECT THE PROCURMENT PART NUMBER EXAMPLE AND ALIGNED SPECIFICATION TO COMPLY WITH SAE GUIDELINES. NOTICE THE REQUIREMENTS FOR PROCURING THE PRODUCT DESCRIBED HEREIN SHALL CONSIST OF THIS SPECIFICATION SHEET AND THE LATEST ISSUE OF SAE AS85049. AS85049/118 IS RECO

7、MMENDED FOR NEW DESIGN. NON-SELF-LOCKING OR SELF-LOCKING COUPLING FIGURE 1 - CONFIGURATION AND DIMENSIONS Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS85049/52SHEET 2 OF 5REV.

8、 CCONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, NONENVIRONMENTAL, SELF-LOCKING AND NON-SELF-LOCKING, STRAIGHT, CATEGORY 4B (FOR AS50151 CRIMP, MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, AND MIL-DTL-83723 SERIES III CONNECTORS) TABLE 1A - DIMENSIONS (NON-SELF-LOCKING ONLY) DASHNUMBER FOR CONNECTOR

9、 SHELL SIZE (REF) NONSELF-LOCKING AS81703SERIES 3 MIL-DTL-26482SERIES 2 AS50151CRIMP MIL-DTL-83723SERIES IIIA MAX DIAL .062 M MAX(SEE NOTE 5) R MAX -3 3 .669 (16.99) .890 (22.61) .63 (16.0) .540 (13.72)-8 8 8S 8 .617 (15.67) .890 (22.61) .63 (16.0) -10 10 10S, 10SL 10 .734 (18.64) 1.000 (25.40) .74

10、18.8) -12 7 12 12S, 12 12 .858 (21.79) 1.125 (28.58) .86 (21.8) -14 12 14 14S, 14 14 .984 (24.99) 1.125 (28.58) .86 (21.8) -16 19 16 16S, 16 16 1.112(28.24) 1.250 (31.75) .99 (25.2) -18 27 18 18 18 1.218(30.94) 1.500 (38.10) 1.24 (31.5) -20 37 20 20 20 1.345(34.16) 1.625 (41.28) 1.36 (34.5) -22 22

11、22 22 1.468(37.29) 1.750 (44.45) 1.49 (37.8) -24 24 24 24 1.593(40.46) 1.875 (47.63) 1.61 (40.9) .540 (13.72)-28 28 1.969(50.01) 2.187 (55.55) 1.76 (44.7) .702 (17.83)-32 32 2.219(56.36) 2.375 (60.33) 1.95 (49.5) -36 36 2.469(62.71) 2.750 (69.85) 2.33 (59.2) -40 40 2.719(69.06) 2.938 (74.63) 2.51 (6

12、3.8) -44 44 2.969(75.41) 3.312 (84.12) 2.89 (73.4) -48 48 3.219(81.76) 3.687 (93.65) 3.26 (82.8) .702 (17.83)-61 61 1.653(41.99) 1.875 (47.63) 1.61 (40.9) .540 (13.72)TABLE 1B - DIMENSIONS (SELF-LOCKING ONLY) DASHNUMBER FOR CONNECTOR SHELL SIZE (REF) SELF-LOCKING AS81703SERIES 3 MIL-DTL-26482SERIES

13、2 AS50151CRIMP MIL-DTL-83723SERIES III A MAX L MAX M MAX (SEE NOTE 5) R MAX -3 1/ 3 -8 8 8S 8 .885 (22.48) 1.04 (26.42) .73 (18.54) .710 (18.03) -10 10 10S, 10SL 10 1.010 (25.65) 1.16 (29.46) .85 (21.59) .710 (18.03) -12 7 12 12S, 12 12 1.135 (28.83) 1.29 (32.77) .98 (24.89) .710 (18.03) -14 12 14 1

14、4S, 14 14 1.260 (32.00 1.29 (32.77) .98 (24.89) .710 (18.03) -16 19 16 16S, 16 16 1.385 (35.18) 1.41 (35.81) 1.10 (27.94) .710 (18.03) -18 27 18 18 18 1.510 (38.35) 1.66 (42.16) 1.35 (34.29) .710 (18.03) -20 37 20 20 20 1.635 (41.53) 1.79 (45.47) 1.48 (37.59) .710 (18.03) -22 22 22 22 1.760 (44.70)

15、1.91 (48.51) 1.60 (40.64) .710 (18.03) -24 24 24 24 1.885 (47.88) 2.04 (51.82) 1.73 (43.94) .710 (18.03) -28 28 2.135 (54.23) 2.35 (59.69) 1.88 (47.75) .890 (22.61) -32 32 2.395 (60.83) 2.60 (66.04) 2.13 (54.10) .890 (22.61) -36 36 2.635 (66.93) 2.91 (73.91) 2.44 (61.98) .890 (22.61) -40 40 2.885 (7

16、3.28) 3.10 (78.74) 2.63 (66.80) .890 (22.61) -44 44 3.135 (79.63) 3.47 (88.14) 3.00 (76.20) .890 (22.61) -48 48 3.385 (85.98) 3.87 (98.30) 3.40 (86.36) .890 (22.61) -61 1/ 61 1/ NOT AVAILABLE ON SELF-LOCKING CONFIGURATION. Copyright SAE International Provided by IHS under license with SAENot for Res

17、aleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS85049/52SHEET 3 OF 5REV. CCONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, NONENVIRONMENTAL, SELF-LOCKING AND NON-SELF-LOCKING, STRAIGHT, CATEGORY 4B (FOR AS50151 CRIMP, MIL-DTL-26482 SERIES 2, AS81703 SERI

18、ES 3, AND MIL-DTL-83723 SERIES III CONNECTORS) TABLE 1C - DIMENSIONS (N0N-SELF-LOCKING AND SELF-LOCKING, CONTINUED) NON-SELF-LOCKING AND SELF LOCKING DASHNUMBER F (SEE NOTE 4) G MAX S.020 TMAXUMAXW+.000 -.062 SCREWLENGTHSCREWSIZEWIRE BUNDLE ACCOMMODATION RANGE MAX MIN -3 1/ .204 (5.18) .125 (3.18) .

19、782 (19.86) .250 (6.35) .140 (3.56) .145 (3.68) .500 (12.70) 6-32 -8 .204 (5.18) .125 (3.18) .782 (19.86) .500 (12.70) -10 .286 (7.26) .187 (4.75) .862 (21.89) .500 (12.70) -12 .416 (10.57) .291 (7.39) 1.003 (25.48) .625 (15.88) -14 .476 (12.09) .351 (8.92) 1.061 (26.95) .625 (15.88) -16 .625 (15.88

20、) .501 (12.73) 1.334 (33.88) .250 (6.35) .140 (3.56) .145 (3.68) .625 (15.88) 6-32 -18 .706 (17.93) .518 (13.16) 1.466 (37.24) .375 (9.53) .171 (4.34) .176 (4.47) .750 (19.05) 8-32 -20 .831 (21.11) .581 (14.76) 1.572 (39.93) .176 (4.47) .875 (22.23) -22 .956 (24.28) .644 (16.36 1.688 (42.88) .176 (4

21、47) 1.000(25.40) -24 1.081 (27.46) .706 (17.93) 1.790 (45.47) .375 (9.53) .171 (4.34) .208 (5.28) 1.125(28.58) -28 1.187 (30.15) .750 (19.05) 2.035 (51.69) .500 (12.70) .203 (5.16) .270 (6.86) 1.250(31.75) 8-32 -32 1.250 (31.75) .875 (22.23) 2.386 (60.60) .270 (6.86) 1.250(31.75) -20 -36 1.375 (34.

22、93) .938 (23.83) 2.496 (63.40) .395(10.03) 1.500(38.10) -40 1.500 (38.10) .938 (23.83) 2.566 (65.18) .500 (12.70) 1.500(38.10) -44 1.750 (44.45) 1.188 (30.18) 2.860 (72.64) .625 (15.88) 1.750(44.45) -48 1.875 (47.63) 1.312 (33.32) 3.344 (84.94) .625 (15.88) .203 (5.16) .395(10.03) 2.000(50.80) -20 -

23、61 1/ 1.081 (27.46) .706 (17.93) 1.775 (45.09) .375 (9.53) .171 (4.34) .208 (5.28) 1.125(28.58) 8-32 1/ NOT AVAILABLE ON SELF-LOCKING CONFIGURATION. NOTES 1. DIMENSIONS ARE IN INCHES. 2. METRIC EQUIVALENTS ARE BASED UPON 1.00 INCH = 25.4 MM AND SHALL BE IN ACCORDANCE WITH ASTM E 380, PARAGRAPH 4.5,

24、METHOD A AND ASTM E 29, ROUNDING-OFF METHOD. 3. DIMENSIONS APPLY AFTER PLATING. 4. “WIRE BUNDLE ACCOMMODATION RANGE” DIMENSION IS DEFINED AS THE ENVELOPE AREA OF THE WIRE BUNDLE. THIS DIMENSION IS NOT MEANT TO DEFINE THE CLAMP HARDWARE LIMITS. 5. MEASURED FROM THE ROOT OF THE TOOTH TO THE BACK OF TH

25、E CLAMP. REQUIREMENTS 1. CONNECTOR ACCESSORY DESIGN AND CONSTRUCTION DIMENSIONS AND CONFIGURATION: SEE FIGURE 1 AND TABLE 1. 2. INTERFACE DIMENSIONS: IN ACCORDANCE WITH SAE AS85049, FIGURE 4 OR 4A. 3. ACCESSORIES CONSIST OF A COUPLING NUT AND STRAIN RELIEF. 4. DETENTED SELF-LOCKING PROVIDES A POSITI

26、VE AUDIBLE DETENTED COUPLING. OPTION “N” IS A FREE SPINNING SELF-LOCKING COUPLING. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS85049/52SHEET 4 OF 5REV. CCONNECTOR ACCESSORIES

27、 ELECTRICAL, STRAIN RELIEF, NONENVIRONMENTAL, SELF-LOCKING AND NON-SELF-LOCKING, STRAIGHT, CATEGORY 4B (FOR AS50151 CRIMP, MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, AND MIL-DTL-83723 SERIES III CONNECTORS) 5. THE STRAIN RELIEF ACCOMMODATES SAE AS85049/127 BUSHING STRIP. 6. CLAMPS SHALL HAVE NO PROT

28、RUSIONS OR SHARP EDGES WHICH MAY PINCH CABLE. 7. MATERIAL AND FINISH: SEE TABLE 2. ACCESSORIES SHALL BE AS SHOWN IN TABLE 2. TABLE 2 - MATERIAL AND FINISH FIGURE MATERIAL FINISH 1ALUMINUM ALLOY IN ACCORDANCE WITH SAE AS85049 AN 1/W 2/1 CORROSION RESISTANT STEEL 300 SERIES IN ACCORDANCE WITH SAE AMS

29、763 S1/ NOT FOR NAVY USE. AIR FORCE USE IS FOR SPACE APPLICATIONS ONLY. W IS THE PREFERRED FINISH. 2/ W IS NOT FOR USE IN SPACE APPLICATION. ALSO SEE SPECIFICATION NOTE 8. CLAMPS, SCREWS AND LOCK WASHERS: 300 SERIES CORROSION-RESISTANT STEEL, PASSIVATE. 9. SELF-LOCKING DEVICE: CORROSION RESISTANT MA

30、TERIAL. 10. ACCESSORIES ARE NOT RECOMMENDED FOR CONNECTORS USING COAX, DATA BUS, SIZES 8, 6, 4 OR 0 CONDUCTORS. USE SAE AS85049/118. WHEN USED WITH MAXIMUM DENSITY ARRANGEMENTS, CLAMP MAY OPEN OUTER WIRE SEALS. 11. QUALIFICATION: SEE SAE AS85049, CATEGORY 4B. 12. PART OR IDENTIFYING NUMBER (PIN): M8

31、5049/ 52 S 10 WEXAMPLE:BASIC PART NUMBER SPECIFICATION SHEET CONFIGURATIONS; “S” FOR DETENTED SELF-LOCKING (SEE REQMT 4) “N” FOR NON-DETENTED SELF-LOCKING “-1-“ (DASH) FOR NON-SELF-LOCKING DASH NUMBER FINISH (SEE TABLE 2) Copyright SAE International Provided by IHS under license with SAENot for Resa

32、leNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS85049/52SHEET 5 OF 5REV. CCONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, NONENVIRONMENTAL, SELF-LOCKING AND NON-SELF-LOCKING, STRAIGHT, CATEGORY 4B (FOR AS50151 CRIMP, MIL-DTL-26482 SERIES 2, AS81703 SERIE

33、S 3, AND MIL-DTL-83723 SERIES III CONNECTORS) 13. SUPERSESSION DATA: SPECIFICATION NOTES NOTICE THIS DOCUMENT REFERENCES A PART WHICH CONTAINS CADMIUM AS A PLATING MATERIAL. CONSULT LOCAL OFFICIALS IF YOU HAVE QUESTIONS CONCERNING CADMIUMS USE. A CHANGE BAR (|) LOCATED IN THE LEFT MARGIN IS FOR THE

34、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. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-