Universal test connector and method of assembly

• US 6,960,102 B2
• Filed: 11/27/2002
• Issued: 11/01/2005
• Est. Priority Date: 11/27/2002
• Status: Expired due to Fees

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Styles, Robert
• Primary Examiner(s): DINH, PHUONG K
• Application Number:
  US10/305,763
• Publication Number:
  US 20040102090A1
• Time in Patent Office: 1,070 Days
• Field of Search: 439/276, 439/604, 439/606, 439/695, 439/730, 439/932, 439/158
• US Class Current: 439/604
• CPC Class Codes: H01R 13/514 composed as a modular blocks or assembly, i.e. composed of co-operating parts provided with contact members or holding contact members between them
• CPC Class Codes: H01R 2201/20 for testing or measuring purposes
• CPC Class Codes: H01R 4/023 between cables or wires and terminals
• CPC Class Codes: H01R 4/72 using a heat shrinking insulating sleeve

Abstract

A method of assembling an electrical test connector for testing connectivity in aircraft wire harness fitted with military specification or other electrical connectors. In a particular embodiment, the test connector is manually assembled on site by a technician from components that are readily and inexpensively available, providing ease and speed in completing connectivity or other wire testing. The test connector has a mating insert, selected and configured to mate with an identified aircraft connector present on the harness to be tested. Insulation and internal wire support is provided by packing the wire connections with a potting material and covering the test connector with an optional heat shrink tubing. Alignment to the aircraft connector may be keyed with the use of a visual indicator applied to the covering. The components as a kit and the assembled test connector are also provided.

Claims

1. A method of assembling a test connector to attach a test wire harness comprising at least one wire to a connector of an aircraft wire harness, the method comprising:

joining the at least one wire of the test wire harness to an insert having a plurality of electrical contacts configured to mate with the aircraft wire harness connector;

packing each joined wire of the test harness with non-conductive potting material where each joined wire is joined to the insert; and

directly covering the non-conductive potting material with non-conductive, heat shrink tubing material, while maintaining the electrical contacts substantially exposed and not covered by the heat shrink tubing.

2. The method of claim 1, further comprising forming an alignment indicator on the test connector.

3. The method of claim 2, wherein the alignment indicator is formed by creating a mark on the test connector.

4. The method of claim 1, wherein the insert is substantially circular in cross section.

5. The method of claim 1, wherein the aircraft wire harness connector is a military specification electrical connector and insert is a military specification connector insert configured to mate to the military specification electrical connector.

6. The method of claim 1, further comprising testing the connectivity of the test wires after they are joined to the insert.

7. The method of claim 1, wherein the at least one wire of the test wire harness is joined to the insert by soldering.

8. The method of claim 1, wherein the non-conductive potting material is selected from a group consisting of epoxy, silicone, rubber, acrylic, or polyurethane.

9. The method of claim 1, wherein the insert has electrical sockets.

10. The method of claim 1, wherein the insert has electrical pins.

11. The method of claim 1, wherein the insert has a combination of at least one electrical socket and at least one electrical pin.

12. A method of manually assembling a test connector to attach a test wire harness having at least one wire to a connector of an aircraft wire harness, the aircraft wire harness connector having an alignment key, the method comprising:

joining the at least one wire of the test wire harness to an insert having a plurality of electrical contacts configured to mate with the aircraft wire harness connector;

packing each joined wire of the test wire harness with non-conductive potting material where each joined wire is joined to the insert;

directly covering the non-conductive potting material and joined wires with non-conductive, heat shrink tubing material while maintaining the electrical contacts substantially exposed and not covered by the heat shrink tubing material; and

forming an alignment indicator on the heat shrink tubing.

13. The method of claim 12, wherein the aircraft wire harness connector is a military specification electrical connector and insert is a military specification connector insert configured to mate to the military specification electrical connector.

14. A test connector assembly for use in connecting a test wire harness having test wires to a connector of an aircraft wire harness, the test connector assembly comprising:

a mating insert configured to mate with the aircraft wire harness connector, the insert having a first side, an opposed second side, and a plurality of electrical contacts, each contact having one end configured to mate with an aircraft connector and another end joined to a test wire from the test wire harness;

a non-conductive potting material manually inserted between the joined test wires proximate to the insert; and

non-conductive, heat shrink tubing installed directly around the potting material and joined test wires,

wherein the plurality of electrical contacts are substantially exposed and not covered by the heat shrink tubing.

15. The test connector assembly of claim 14, further comprising an alignment indicator mark formed on the heat shrink tubing.

16. The test connector assembly of claim 14, wherein the test connector insert is substantially circular in cross section.

17. The test connector assembly of claim 14, wherein the aircraft wire harness connector is a military specification electrical connector and insert is a military specification connector insert configured to mate to the military specification electrical connector.

18. The test connector assembly of claim 14, wherein the non-conductive potting material is selected from a group consisting of epoxy, silicone, rubber, acrylic, or polyurethane.

19. The test connector assembly of claim 14, wherein the insert has electrical sockets.

20. The test connector assembly of claim 14, wherein the insert has electrical pins.

21. The test connector assembly of claim 14, wherein the insert has a combination of at least one electrical socket and at least one electrical pin.

22. A kit for assembling at least one test connector for use in connecting a test wire harness comprising at least one wire to at least one predetermined connector of an aircraft wire harness, the kit comprising:

at least one conductive mating connector insert having a plurality of electrical contact configured to mate with the predetermined aircraft wire harness connector;

non-conductive potting material to support the at least one wire of the test wire harness wires when joined to the insert; and

non-conductive heat shrink tubing to directly cover the potting material and joined test wires, while maintaining the electrical contacts substantially exposed and covered by the heat shrink tubing.

23. The kit of claim 22, wherein the aircraft wire harness connector is a military specification electrical connector and each insert is a military specification connector insert configured to mate to the military specification electrical connector.

24. The kit of claim 23, further comprising solder for connecting the test wire harness to the military specification connector insert.

25. The kit of claim 22, further comprising marker material to identify key mating alignment of the test connector to the aircraft connector.

26. The kit of claim 22, wherein such non-conductive potting material is selected from a group consisting of epoxy, silicone, rubber, acrylic, or polyurethane.

27. The kit of claim 22, wherein the at least one insert has electrical sockets.

28. The kit of claim 22, wherein the at least one insert has electrical pins.

29. The kit of claim 22, wherein the at least one insert has a combination of at least one electrical socket and at least one electrical pin.