Title:
無線航空機エンジン監視システム
Document Type and Number:
Japanese Patent JP6490149
Kind Code:
B2
Abstract:
An engine monitoring system (100) for an aircraft engine (102) having a nacelle (110) extending annularly thereabout and a sensor (116) positioned radially inward therefrom. The system includes an engine control device (104) coupled communicatively to the sensor and configured to receive engine data from the sensor and/or receive instruction data from a transmitter device (512) positioned radially outward from a nacelle radially outward surface (111). The system also includes a composite panel (208,702,802,902) including at least a portion of the nacelle and a ground plane (602) positioned radially inward from the nacelle radially outward surface, the composite panel including an antenna (502) coupled communicatively to engine control device and a radome (405,504) 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 (510), and receive instruction data from the transmitter device and transmit instruction data to the engine control device.
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Inventors:
Seraca Bandara Blumura
David Patrick Calder
Michael joseph derano
Andrew Michael Roach
David Patrick Calder
Michael joseph derano
Andrew Michael Roach
Application Number:
JP2017115537A
Publication Date:
March 27, 2019
Filing Date:
June 13, 2017
Export Citation:
Assignee:
GENERAL ELECTRIC COMPANY
International Classes:
B64D45/00; B64D47/00; G08C17/02; H01Q1/28; H01Q1/42
Domestic Patent References:
| JP2010209916A | ||||
| JP5055607U | ||||
| JP2005220905A | ||||
| JP2013201794A |
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka