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:
Aug. 08, 2017

Filed:

Dec. 24, 2013
Applicant:

Borealis Technical Limited, North Plains, OR (US);

Inventors:

Jonathan S. Edelson, Portland, OR (US);

Arlie Stonestreet, Manhatten, KS (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 25/50 (2006.01); B64C 25/40 (2006.01); B64C 25/34 (2006.01); H01R 12/70 (2011.01); H02K 3/50 (2006.01); H02K 5/22 (2006.01); H02K 7/14 (2006.01); H05K 1/02 (2006.01);
U.S. Cl.
CPC ...
B64C 25/405 (2013.01); B64C 25/34 (2013.01); H01R 12/7076 (2013.01); H02K 3/50 (2013.01); H02K 5/225 (2013.01); H02K 7/14 (2013.01); H05K 1/0265 (2013.01); H05K 2201/09227 (2013.01); Y02T 50/823 (2013.01);
Abstract

An electric connector assembly is provided that is designed to provide a simple and reliable electric connection between a source of electric power on an aircraft and a plurality of electrical connections, such as those from stator windings, in an electric drive means powering an aircraft landing gear drive wheel. The plurality of drive means electrical connections are individually connected to power distribution elements designed to significantly reduce the number of connectors required to establish an electrical connection between the drive means and an aircraft power supply. The reduced number of connectors is directed out of the wheel and guided along a path by a path guide element to a connector element designed to connect directly with a wire harness or other connection with an aircraft source of electric power. This electric connector design facilitates disconnection and reconnection when removal and remounting of the drive wheel is required.


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