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本文(DLA MIL-DTL-83723 67 B-2009 CONNECTORS ELECTRICAL (CIRCULAR ENVIRONMENT RESISTING) PLUG THREADED COUPLING (PUSH-PULL QUICK-DISCONNECT WITHOUT LANYARD) CRIMP SOCKET CONTACT SERIES I.pdf)为本站会员(postpastor181)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!

DLA MIL-DTL-83723 67 B-2009 CONNECTORS ELECTRICAL (CIRCULAR ENVIRONMENT RESISTING) PLUG THREADED COUPLING (PUSH-PULL QUICK-DISCONNECT WITHOUT LANYARD) CRIMP SOCKET CONTACT SERIES I.pdf

1、 DETAIL SPECIFICATION SHEET CONNECTORS, ELECTRICAL, (CIRCULAR, ENVIRONMENT RESISTING), PLUG, THREADED COUPLING, (PUSH-PULL, QUICK-DISCONNECT WITHOUT LANYARD), CRIMP SOCKET CONTACT, SERIES III, CLASSES A, G, M, R, T, W AND Z This specification is approved for use by all Departments and Agencies of th

2、e Department of Defense. The requirements for acquiring the product described herein shall consist of this specification sheet and MIL-DTL-83723. FIGURE 1. Dimensions and configurations. AMSC N/A FSC 5935 INCH-POUND MIL-DTL-83723/67B 29 June 2009 SUPERSEDING MIL-C-83723/67A (USAF) 17 December 1991 P

3、rovided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-83723/67B 2 Shell size A dia B dia C dia D dia E dia F thread G dia H dia 8 .704 (17.88) .290 (7.37) .470 (11.94) .370 (9.40) .305 (7.75) .500-20 UNF-2A .437 (11.10) .294 (7.47) 10 .829 (21.06) .

4、388 (9.86) .600 (15.24) .497 (12.62) .405 (10.29) .625-24 UNEF-2A .572 (14.53) .428 (10.87) 12 1.016 (25.81) .558 (14.17) .724 (18.39) .613 (15.57) .531 (13.49) .750-20 UNEF-2A .687 (17.45) .598 (15.19) 14 1.079 (27.41) .627 (15.93) .849 (21.56) .738 (18.75) .665 (16.89) .875-20 UNEF-2A .812 (20.62)

5、 .667 (16.94) 16 1.204 (30.58) .772 (19.61) .974 (24.74) .863 (21.92) .790 (20.07) 1.000-20 UNEF-2A .937 (23.80) .794 (20.17) 18 1.345 (34.16) .860 (21.84) 1.030 (26.16) .919 (23.34) .869 (22.07) 1.0625-18 UNEF-2A .992 (25.20) .900 (22.86) 20 1.470 (37.34) .985 (25.02) 1.154 (29.31) 1.044 (26.52) .9

6、94 (25.25) 1.1875-18 UNEF-2A 1.117 (28.37) 1.025 (26.04) 22 1.595 (40.51) 1.110 (28.19) 1.279 (32.49) 1.169 (29.69) 1.119 (28.42) 1.3125-18 UNEF-2A 1.242 (31.55) 1.150 (29.21) 24 1.720 (43.69) 1.235 (31.37) 1.404 (35.66) 1.294 (32.87) 1.244 (31.60) 1.4375-18 UNEF-2A 1.367 (34.72) 1.275 (32.39) FIGUR

7、E 1. Dimensions and configurations - Continued. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-83723/67B 3 Shell size J K M 8 .405 (10.29) .396 (10.06) .612 (15.54) 1.095 (27.81) 10 .526 (13.36) .517 (13.13) .737 (18.72) 1.240 (31.50) 12 .69

8、6 (17.68) .687 (17.45) .925 (23.50) 1.432 (36.37) 14 .765 (19.43) .756 (19.20) .987 (25.07) 1.490 (37.85) 16 .892 (22.66) .883 (22.43) 1.112 (28.24) 1.711 (43.46) 18 .998 (25.35) .989 (25.12) 1.237 (31.42) 1.815 (46.10) 20 1.123 (28.52) 1.114 (28.30) 1.362 (34.59) 1.962 (49.83) 22 1.248 (31.70) 1.23

9、9 (31.47) 1.487 (37.77) 2.070 (52.58) 24 1.373 (34.87) 1.364 (34.65) 1.612 (40.94) 2.195 (55.75) Inches mm Inches mm Inches mm Inches mm Inches mm .031 0.79 .363 9.22 .667 16.94 .992 25.20 1.294 32.87 .035 0.89 .367 9.32 .687 17.45 .994 25.25 1.313 33.35 .045 1.14 .370 9.40 .696 17.68 .998 25.35 1.3

10、45 34.16 .051 1.30 .377 9.58 .704 17.88 1.000 25. 40 1.362 34. 59 .054 1.37 .378 9.60 .705 17.91 1.016 25.81 1.364 34.65 .061 1.55 .388 9.86 .708 17.98 1.025 26.04 1.367 34.72 .068 1.73 .396 10.06 .724 18.39 1.044 26.52 1.373 34.87 .070 1.78 .400 10.16 .730 18.54 1.063 27.00 1.432 36.37 .076 1.93 .4

11、02 10.21 .737 18.72 1.079 27.41 1.438 36.53 .081 2.06 .428 10.87 .738 18.75 1.090 27.69 1.470 37.34 .087 2.21 .437 11.10 .750 19.05 1.095 27.81 1.487 37.77 .092 2.34 .465 11.81 .756 19.20 1.110 28.19 1.490 37.85 .096 2.44 .468 11.89 .765 19.43 1.112 28.24 1.595 40.51 .097 2.46 .470 11.94 .772 19.61

12、1.114 28.30 1.612 40.94 .107 2.72 .481 12.22 .790 20.07 1.117 28.37 1.711 43.46 .114 2.90 .497 12.62 .794 20.17 1.119 28.42 1.720 43.69 .118 3.00 .500 12.70 .812 20.62 1.123 28.52 1.815 46.10 .130 3.30 .510 12.95 .829 21.06 1.130 28.70 1.962 49.83 .146 3.71 .526 13.36 .849 21.56 1.150 29.21 2.070 52

13、.58 .150 3.81 .531 13.49 .860 21.84 1.154 29.31 2.129 54.08 FIGURE 1. Dimensions and configurations - Continued. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-83723/67B 4 Inches mm Inches mm Inches mm Inches mm Inches mm .190 4.38 .558 14.1

14、7 .863 21.92 1.169 29.69 2.195 55.75 .206 5.23 .572 14.53 .869 22.07 1.180 29.97 2.353 59.77 .210 5.33 .580 14.73 .875 22.23 1.188 30.18 .222 5.64 .583 14.81 .883 22.43 1.204 30.58 .225 5.72 .598 15.19 .892 22.66 1.224 31.09 .263 6.68 .600 15.24 .898 22.81 1.235 31.37 .282 7.16 .612 15.54 .900 22.86

15、 1.237 31.42 .285 7.24 .613 15.57 .919 23.34 1.239 31.47 .290 7.37 .625 15.88 .925 23.50 1.240 31.50 .294 7.47 .627 15.93 .937 23.80 1.242 31.55 .305 7.75 .643 16.33 .975 24.77 1.248 31.70 .309 7.85 .646 16.41 .985 25.02 1.275 32.39 .320 8.13 .662 16.89 .987 25.07 1.279 32.49 NOTES: 1. Dimensions ar

16、e in inches. 2. Metric equivalents are given for information only. 3. Unless otherwise specified, tolerances are .010 (0.25) for two place decimals, .005 (.13 mm) for three place decimals, and 1oand 30 for angular dimensions. 4. The dimensions showing the relationship between the coupling ring and s

17、hell apply only when the coupling ring is in the full forward position. 5. The quick-disconnect connector plug is intended to be used with series III threaded coupling receptacles MIL-DTL-83723/82 and MIL-DTL-83723/84 with the adapter MIL-DTL-83723/70 permanently attached to the receptacle. 6. Coupl

18、ing of the quick-disconnect plug connector is to be accomplished by a straight axial push with no cocking of the coupling mechanism. 7. Uncoupling of the quick-disconnect plug connector is to be accomplished by a straight axial pull on the outer coupling ring. 8. See table I for contact cavities req

19、uiring this dimension. FIGURE 1. Dimensions and configurations - Continued. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-83723/67B 5 Shell size P P1 P2 P3 P4 R R1 8 1.457 (37.01) 1.869 (47.47) 2.018 (51.26) 5.838 (148.29) 1.848 (46.94) .83

20、0 (21.08) 4.585 (116.46) 10 1.457 (37.01) 1.979 (50.27) 2.100 (53.34) 6.528 (165.81) 1.888 (47.96) .880 (22.35) 5.390 (136.91) 12 1.457 (37.01) 2.124 (53.95) 2.293 (58.24) 7.348 (186.64) 1.928 (48.97) .950 (24.13) 6.330 (160.78) 14 1.457 (37.01) 2.124 (53.95) 2.353 (59.77) 7.348 (186.64) 1.928 (48.9

21、7) 1.010 (25.65) 6.330 (160.78) 16 1.457 (37.01) 2.229 (56.62) 2.502 (63.55) 8.068 (204.93) 2.028 (51.51) 1.070 (27.18) 6.710 (170.43) 18 1.457 (37.01) 2.474 (62.84) 2.614 (66.40) 8.068 (204.93) 2.028 (51.51) 1.130 (28.70) 6.710 (170.43) 20 1.457 (37.01) 2.604 (66.14) 2.739 (69.57) 9.068 (230.33) 2.

22、148 (54.56) 1.190 (30.23) 7.740 (196.60) 22 1.457 (37.01) 2.729 (69.32) 2.864 (72.75) 9.068 (230.33) 2.148 (54.56) 1.260 (32.00) 7.740 (196.60) 24 1.457 (37.01) 2.854 (72.49) 2.989 (75.92) 9.068 (230.33) 2.228 (56.59) 1.320 (33.53) 8.030 (203.96) FIGURE 2. Plug and backshell assembly, dimensions and

23、 configurations. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-83723/67B 6 NOTES: 1. Dimensions are in inches. 2. Metric equivalents are given for information only. Metric equivalents are in parentheses. 3. Unless otherwise specified, toler

24、ances are .010 (0.25) for two place decimals, .005 (0.13) for three place decimals, and 1oand 30 for angular dimensions. FIGURE 2. Plug and backshell assembly, dimensions and configurations Continued. REQUIREMENTS: Dimensions and configurations: See figures 1 and 2. For insert arrangements, see MIL-

25、STD-1554 and table I. TABLE I. Inserts requiring reduced diameters for lead-in chamfers on contact cavities. Shell size Insert arrangements Contact cavities 8 03 1, 2, 3 10 06 1, 2, 3, 4, 5, 6 For connector accessories: See SAE-AS85049 and MIL-C-83723/16. Unless otherwise specified in the purchase o

26、rder, the following components shall be furnished with the connector: a. Contacts in accordance with SAE-AS39029 shall be furnished with the connector. Spare contacts are required for each contact size. The total quantity of spare contacts shall be 10 percent or 1, whichever is greater, of the total

27、 number of each size contact required. b. Grommet seal plugs in accordance with MS27488 shall be furnished with the connector. Total quantity shall be 15 percent of each contact size or 3, whichever is greater. c. Contact extraction tools in accordance with MIL-I-81969 shall be included in the conne

28、ctor package. Connector assembly shall include a backshell (see SAE-AS85049 and MIL-C-83723/16) to ensure compliance with moisture sealing requirements. The coupling mechanism of the connector plug shall withstand a minimum tensile load of 100 lb (45.36 kg) minimum. Load shall be applied to rear acc

29、essory hardware in a straight axial direction. The quick-disconnect connector plug shall meet the vibration and shock requirements in accordance with MIL-DTL-83723 and the coupling mechanism shall maintain the plug and receptacle in a locked condition. The tensile force required to unlock the coupli

30、ng mechanism shall be 5 lb (2.27 kg) minimum and 20 lb (9.07 kg) maximum. The locking mechanism shall meet the performance requirements of MIL-DTL-83723. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-83723/67B 7 Part or Identifying Number (

31、PIN) example: M83723/ 67 W 22 55 N Military designator Specification sheet number Class Shell size Insert arrangement Polarizing position Changes from previous issue. Marginal notations are not used in this revision to identify changes with respect to the previous issue due to the extent of the chan

32、ges. Referenced documents. In addition to MIL-DTL-83723, this document references the following: MIL-STD-1554 MS27488 MIL-I-81969 MIL-C-83723/16 MIL-DTL-83723/70 MIL-DTL-83723/82 MIL-DTL-83723/84 SAE-AS39029 SAE-AS85049 CONCLUDING MATERIAL Custodians: Preparing activity: Army - CR DLA - CC Navy - AS

33、 Air Force - 85 DLA - CC Review activities: (Project 5935-2008-103) Air Force 70, 99 NOTE: The activities listed above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information above using the ASSIST Online database at http:/assist.daps.dla.mil. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-

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