The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Oct. 10, 2023

Filed:

Jun. 15, 2021
Applicant:

Aptiv Technologies (2) S.à R.l., Luxembourg, LU;

Inventors:

David R. Peterson, Aurora, OH (US);

Jared Bilas, North Bloomfield, OH (US);

Joseph Sudik, Niles, OH (US);

Jonathan D. Weidner, Conneautville, PA (US);

Sean P. Krompegel, Canfield, OH (US);

Jesse Braun, Warren, OH (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H01R 12/77 (2011.01); H01B 7/08 (2006.01); H01B 13/00 (2006.01); H01R 4/02 (2006.01); H01R 4/2429 (2018.01); H01R 13/424 (2006.01); H01R 43/02 (2006.01); H01R 43/20 (2006.01); H01R 43/28 (2006.01);
U.S. Cl.
CPC ...
H01R 12/771 (2013.01); H01B 7/0823 (2013.01); H01B 13/0036 (2013.01); H01R 4/023 (2013.01); H01R 4/2429 (2013.01); H01R 13/424 (2013.01); H01R 43/02 (2013.01); H01R 43/20 (2013.01); H01R 43/28 (2013.01);
Abstract

A method of forming an electrical cable assembly includes providing a multiconductor flat cable comprising wires arranged in a coplanar fashion with each other and encased within a planar dielectric structure, cutting a slot in the planar dielectric structure intermediate the wires, thereby forming wing features in the dielectric structure extending from the wires, removing portions of the dielectric structure from ends of the wires, wherein portions of wing features remain, attaching the exposed wires to terminals, wherein the terminals define prongs, and attaching the portions of the wing features to by inserting the prongs within holes defined in the portions of the wing features, thereby retaining the wires to the terminals.


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