Avionics system interface electrical connector
First Claim
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1. An electrical connector comprising:
- a first pass-through connector;
a second pass-through connector;
a center portion coupled between said first pass-through connector and said second pass-through connector and comprising a plurality of electrical connection points on an exterior surface of said center portion;
an adapter ring configured to couple about said center portion; and
a plurality of pass-through wires extending from first pass-through connector to said second pass-through connector through said center portion, wherein said plurality of electrical connection points are electronically coupled to said plurality of pass-through wires.
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Abstract
An electrical connector includes a first pass-through connector, a second pass-through connector, and a center portion coupled between the first pass-through connector and the second pass-through connector. The center portion includes a plurality of electrical connection points on an exterior surface of the center portion. The electrical connector also includes a plurality of pass-through wires extending from the first pass-through connector to the second pass-through connector through the center portion, wherein the plurality of electrical connection points are electronically coupled to the plurality of pass-through wires.
27 Citations
40 Claims
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1. An electrical connector comprising:
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a first pass-through connector; a second pass-through connector; a center portion coupled between said first pass-through connector and said second pass-through connector and comprising a plurality of electrical connection points on an exterior surface of said center portion; an adapter ring configured to couple about said center portion; and a plurality of pass-through wires extending from first pass-through connector to said second pass-through connector through said center portion, wherein said plurality of electrical connection points are electronically coupled to said plurality of pass-through wires. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11)
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12. An avionics system interface comprising:
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a wire harness comprising a plurality of wires; a wire harness connector coupled to said wire harness and said plurality of wires; a disconnect connector; and an electrical connector coupled between said wire harness connector and said disconnect connector, said electrical connector comprising; a first pass-through connector coupled to said wire harness connector; a second pass-through connector coupled to said disconnect connector; a center portion coupled between said first pass-through connector and said second pass-through connector and comprising a plurality of electrical connection points on an exterior surface of said center portion; an adapter ring configured to couple about said center portion; and a plurality of pass-through wires extending from first pass-through connector to said second pass-through connector through said center portion, wherein said plurality of electrical connection points are electronically coupled to said plurality of pass-through wires. - View Dependent Claims (13, 14, 15, 16, 17, 18, 19, 20, 21)
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22. An electrical connector for use with a wire harness connector the electrical connector comprising:
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a first pass-through connector, wherein said first pass-through connector comprises a sleeve and a first removable insert of a plurality of removable inserts positioned within said sleeve, wherein said plurality of removable inserts are interchangeable based on a configuration of the wire harness connector; a second pass-through connector; a center portion coupled between said first pass-through connector and said second pass-through connector and comprising a plurality of electrical connection points on an exterior surface of said center portion; and a plurality of pass-through wires extending from first pass-through connector to said second pass-through connector through said center portion, wherein said plurality of electrical connection points are electronically coupled to said plurality of pass-through wires. - View Dependent Claims (23, 24, 25, 26, 27, 28, 29, 30, 31)
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32. An avionics system interface comprising:
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a wire harness comprising a plurality of wires; a wire harness connector coupled to said wire harness and said plurality of wires; a disconnect connector; and an electrical connector coupled between said wire harness connector and said disconnect connector, said electrical connector comprising; a first pass-through connector coupled to said wire harness connector, wherein said first pass-through connector comprises a sleeve and a first removable insert of a plurality of removable inserts positioned within said sleeve, wherein said plurality of removable inserts are interchangeable based on a configuration of said wire harness connector; a second pass-through connector coupled to said disconnect connector; a center portion coupled between said first pass-through connector and said second pass-through connector and comprising a plurality of electrical connection points on an exterior surface of said center portion; and a plurality of pass-through wires extending from first pass-through connector to said second pass-through connector through said center portion, wherein said plurality of electrical connection points are electronically coupled to said plurality of pass-through wires. - View Dependent Claims (33, 34, 35, 36, 37, 38, 39, 40)
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Specification