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. 15, 2018

Filed:

Jun. 23, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Selaka Bandara Bulumulla, Niskayuna, NY (US);

David Patrick Calder, Baltimore, MD (US);

Michael Joseph Dell'Anno, Clifton Park, NY (US);

Andrew Michael Roach, Aberdeen, MD (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
H01Q 1/28 (2006.01); B64D 29/00 (2006.01); B64D 29/06 (2006.01); G07C 5/00 (2006.01); B64F 5/60 (2017.01); B64C 7/02 (2006.01);
U.S. Cl.
CPC ...
H01Q 1/28 (2013.01); B64C 7/02 (2013.01); B64D 29/00 (2013.01); B64D 29/06 (2013.01); B64F 5/60 (2017.01); G07C 5/008 (2013.01); H01Q 1/286 (2013.01);
Abstract

An engine monitoring system for an aircraft engine having a nacelle extending annularly thereabout and a sensor positioned radially inward therefrom. The system includes an engine control device coupled communicatively to the sensor and configured to receive engine data from the sensor and/or receive instruction data from a transmitter device positioned radially outward from a nacelle radially outward surface. The system also includes a composite panel including at least a portion of the nacelle and a ground plane positioned radially inward from the nacelle radially outward surface, the composite panel including an antenna coupled communicatively to engine control device and a radome positioned radially outward from ground plane. The antenna is configured to at least one of receive engine data from the engine control device and transmit engine data to a receiver device, and receive instruction data from the transmitter device and transmit instruction data to the engine control device.


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