NAVY MIL-PRF-18148 2 REV G-2009 PLUG ELECTRIC FOUR-WIRE AIRCRAFT STORAGE BATTERY《飞机蓄电池4线电插头》.pdf

《NAVY MIL-PRF-18148 2 REV G-2009 PLUG ELECTRIC FOUR-WIRE AIRCRAFT STORAGE BATTERY《飞机蓄电池4线电插头》.pdf》由会员分享，可在线阅读，更多相关《NAVY MIL-PRF-18148 2 REV G-2009 PLUG ELECTRIC FOUR-WIRE AIRCRAFT STORAGE BATTERY《飞机蓄电池4线电插头》.pdf（6页珍藏版）》请在麦多课文档分享上搜索。

1、AMSC N/A FSC 5935 MIL-PRF-18148/2 30 September 2009 SUPERSEDING MS25182G 1 June 1984 PERFORMANCE SPECIFICATION SHEET PLUG, ELECTRIC, FOUR-WIRE, AIRCRAFT STORAGE BATTERY This specification is approved for use by all Departments and Agencies of the Department of Defense. The requirements for acquiring

2、 the product described herein shall consist of this specification sheet and MIL-PRF-18148. REQUIREMENTS: 1. Part or identifying number. The part or identifying number (PIN) of the plug covered by this specification sheet shall be MS25182-2. The MS25182-2 is a four-wire electric plug used with aircra

3、ft storage batteries. The plug shall mate with the pins of MS3509-series receptacles to meet mechanical engagement and electrical resistance requirements. 2. Dimensions and weight. The dimensions and weight of the plug shall be as specified in 3.12.3 of MIL-PRF-18148 and 3.12.4 as modified herein an

4、d as shown on figure 1 contained herein. 3. MIL-PRF-18148 variance. The plug shall comply with MIL-PRF-18148 except as follows. 3.1 Modify the following paragraphs: 3.8.2 Electrical connections. Insert after the first sentence: “Each four-wire MS25182-2 plug shall include as its electrical connectio

5、ns four sockets with their axes horizontal and in a plane parallel to the face of the receptacle. Each plug shall be usable with four 000-gauge wires conforming to SAE-AS50861/2 for Type 2. Each plug shall include four wire entry holes on the sides, through which the wires may be brought into the so

6、ckets. Each plug shall be made so that the wires shall enter it horizontally and in a plane parallel to the face of the receptacle. Each plug shall be made so that the wire which enters the left wire entry hole, as viewed looking at the front (handle) face of the plug, can be connected to the negati

7、ve contact only, and the wire which enters the right wire entry hole can be connected to the positive contact only. “-“ and “+“ shall be marked on the front, back, bottom, or sides of the plug so as to identify the wires connected to INCH-POUND Provided by IHSNot for ResaleNo reproduction or network

8、ing permitted without license from IHS-,-,-MIL-PRF-18148/2 2 the plug. The plug shall be made so that it is not possible to assemble it with any of the marking not in its proper location. Each plug shall include two setscrews for retaining the wires in the sockets that can be accessed after removing

9、 the cover of the plug. Each plug shall include two threaded terminals for retaining the wires in the sockets The axes of the threaded terminals shall be perpendicular to the face of the receptacle. Each threaded terminal shall include a hexagonal wrenching socket. Each plug shall include two wrench

10、 entry holes on the front face, and shall be made so that the threaded terminals can be operated by a wrench inserted in the wrench entry holes. No part of the electric circuit of the plug shall be exposed except through the wire, wrench, and contact entry holes.“ 3.10.1 Delete this paragraph. 3.12.

11、4 Weight. Insert after the first sentence: “The weight of each four-wire MS25182-2 plug shall be not greater than 1.10 pounds.“ VERIFICATION 1. MIL-PRF-18148 variance. The plug shall comply with MIL-PRF-18148 except as follows. 4.2 Qualification inspection. Insert after the end of the first sentence

12、: “(see table I of the specification sheet).“ 4.3 Conformance inspection. Insert after the end of the first sentence: “(see table I of the specification sheet).“ 4.5.5 Plug preparation procedure. Insert as a new first sentence: “Whenever electric connection must be made to the plug, four 000-gauge w

13、ires conforming to SAE-AS50861/2 for Type 2 shall be connected to the plug in accordance with 3.8.2 as modified by MIL-PRF-18148/2.“ 6.9 Supersession data. Delete the text and insert. “Connector plugs previously procured to MS25182 are superseded by MIL-PRF-18148/2”. 6.10 International standardizati

14、on agreement implementation. This specification implements STANAG-3660 ED.2(8). When amendment, revision, or cancellation of this specification is proposed, the preparing activity must coordinate the action with the U.S. National Point of Contact for the international standardization agreement, as i

15、dentified in the ASSIST database at http:/assist.daps.dla.mil. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-18148/2 3 FIGURE 1. Dimensions and configuration for PIN MS25182-2. 1.100 1.532 .004 Provided by IHSNot for ResaleNo reproduction o

16、r networking permitted without license from IHS-,-,-MIL-PRF-18148/2 4 FIGURE 1. Dimensions and configuration for PIN MS25182-2 - Continued. 2.437 MAXDOUBLE THREAD, PITCH OF EACH THREAD .785 INCH Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF

17、-18148/2 5 TABLE I. Qualification inspection and conformance inspection of plugs. Qualification sample number Conformance inspection sample number Test number Examinations and tests 1 2 3 1 2 Requirement paragraph Method of inspection paragraph 1 INCOMING INSPECTION X X X X X 3.9, 3.12.1 4.5.1 2 VIS

18、UAL AND MECHANICAL INSPECTION X X X X X 3.4 through 3.10, 3.12.2, table II 4.5.2 3 DIMENSIONS X X 3.12.3, Reqmt 2 4.5.3 4 WEIGHT X X X X X 3.12.4, Reqmt 2 4.5.4 PLUG PREPARATION X X X X X - 4.5.5 5 STRESS TESTS AT 77F 5a Dielectric strength X X X X X 3.11, 3.12.5 4.5.6.1 5b Insulation resistance X X

19、 X X X 3.11, 3.12.6 4.5.7.1 5c Operating torque X X X X X 3.11, 3.12.7 4.5.8.1 5d Contact resistance X X X X X 3.11, 3.12.8 4.5.9.1 6 STRESS TESTS AT -65F 6a Dielectric strength X 3.11, 3.12.5 4.5.6.2 6b Insulation resistance X 3.11, 3.12.6 4.5.7.2 6c Operating torque X 3.11, 3.12.7 4.5.8.2 6d Conta

20、ct resistance X 3.11, 3.12.8 4.5.9.2 7 STRESS TESTS AT 160F 7a Dielectric strength X 3.11, 3.12.5 4.5.6.3 7b Insulation resistance X 3.11, 3.12.6 4.5.7.3 7c Operating torque X 3.11, 3.12.7 4.5.8.3 7d Contact resistance X 3.11, 3.12.8 4.5.9.3 8 LIFE TEST X X 3.11, 3.12.10, 3.12.7, 3.12.8 4.5.11.1, 4.

21、5.8.1, 4.5.9.1 9 TEMPERATURE SHOCK TEST X 3.11, 3.12.11, 3.12.5, 3.12.7, 3.12.8 4.5.12, 4.5.6.1, 4.5.8.1, 4.5.9.1 10 MECHANICAL SHOCK TEST X 3.11, 3.12.12, 3.12.5 4.5.13, 4.5.6.1 11 HUMIDITY TEST X 3.11, 3.12.14, 3.12.6, 3.12.7, 3.12.8 4.5.14, 4.5.7.1, 4.5.8.1, 4.5.9.1 12 IMMERSION X 3.10, 3.11, 3.1

22、2.15, 3.12.6, 3.12.7, 3.12.8 4.5.15, 4.5.7.1, 4.5.8.1, 4.5.9.1 13 SALT FOG TEST X X X X X 3.10, 3.11, 3.12.15, 3.12.6, 3.12.7, 3.12.8 4.5.16, 4.5.7.1, 4.5.8.1, 4.5.9.1 14 VIBRATION TEST X X 3.11, 3.12.13, 3.12.5, 3.12.7, 3.12.8 4.5.17.1, 4.5.6.1, 4.5.8.1, 4.5.9.1 Provided by IHSNot for ResaleNo repr

23、oduction or networking permitted without license from IHS-,-,-MIL-PRF-18148/2 6 CONCLUDING MATERIAL Custodians: Preparing activity: Army - AV Navy - AS Navy - AS Air Force - 85 DLA - CC Agent: Navy - SH Reviewer activities: (Project 5935-2009-158) Army - CR, MI Air Force - 99 DLA - GS NOTE: The acti

24、vities 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-,-,-