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:
May. 31, 2016

Filed:

Dec. 13, 2013
Applicants:

David Wayne Leadingham, Bradenton, FL (US);

Drew Robert Johnson, Palmetto, FL (US);

Randy John Fette, Santa Rosa, CA (US);

Ralph Emerson Welch, Bradenton, FL (US);

Inventors:

David Wayne Leadingham, Bradenton, FL (US);

Drew Robert Johnson, Palmetto, FL (US);

Randy John Fette, Santa Rosa, CA (US);

Ralph Emerson Welch, Bradenton, FL (US);

Assignee:

Illinois Tool Works, Inc., Glenview, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
H01R 13/66 (2006.01); H01R 13/648 (2006.01); B64F 1/36 (2006.01); B64F 1/34 (2006.01);
U.S. Cl.
CPC ...
H01R 13/648 (2013.01); B64F 1/34 (2013.01); B64F 1/36 (2013.01);
Abstract

An aircraft ground power connector for use in an aircraft ground power support system providing electrical power from a ground power unit through a ground power cable to the ground power receptacle of a parked aircraft. The axis of the portion of the connector housing which engages the aircraft ground power receptacle is angled relative to the axis of the portion of the housing which receives the ground power cable to minimize mechanical stress on the aircraft ground power receptacle when the connector is installed therein and to render the connector easier to insert and remove from the aircraft receptacle. Additionally, the ground power connector includes a capacitor connected to an electrical circuit within the connector supplying do voltage to the aircraft ground power receptacle to mitigate momentary voltage drops at the receptacle resulting from momentary surges in current demand by the aircraft.


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