Wireless engine monitoring system and associated engine wireless sensor network
First Claim
1. A monitoring system for an aircraft engine, comprising:
- a plurality of wireless engine sensors associated with the aircraft engine, each wireless engine sensor configured to sense an engine parameter as engine data and transmit wirelessly the engine data regarding the sensed engine parameter and receive engine data to change the respective operation of the engine parameter sensing;
an engine monitoring module comprising;
a housing mounted at the aircraft engine,a wireless sensor processor and wireless sensor transceiver mounted within the housing and configured to receive the engine data regarding sensed engine parameters from the wireless engine sensors;
a first wireless transceiver carried by the housing,a memory carried by the housing,a processor carried by the housing and coupled to the memory, the wireless sensor processor and wireless sensor transceiver, and the first wireless transceiver and configured to;
collect and store in said memory engine data relating to engine parameters sensed during operation of the aircraft engine by the plurality of wireless engine sensors;
transmit the engine data via the first wireless transceiver over a wireless communications signal into the aircraft,a wireless local area network (LAN) communications unit located within the aircraft and forming a wireless access point and wireless LAN within the aircraft and configured to transmit the engine data via the wireless LAN from the wireless LAN communications unit into the aircraft for further processing and receive and transmit to the engine monitoring module engine data regarding engine parameter sensing for transmission to the wireless engine sensors via the wireless sensor processor and wireless sensor transceiver; and
wherein selected ones of the plurality of wireless engine sensors receive the engine data and change the operation of a respective sensor for a different engine parameter sensing operation.
1 Assignment
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Accused Products
Abstract
A plurality of wireless engine sensors each includes a sensing circuit that senses an engine parameter as engine data. A radio transceiver receives and transmits the engine data regarding the sensed engine parameters. An engine monitoring module includes a housing configured to be mounted at the aircraft engine. A sensor receiver is mounted within the housing and receives the engine data from the wireless engine sensors. A first wireless transmitter is carried by the housing. A memory is carried by the housing and a processor is carried by the housing and coupled to the memory and the first wireless transmitter and configured to collect and store in the memory engine data related to engine parameters sensed during operation of the aircraft engine by the plurality of wireless engine sensors and transmit the engine data via the first wireless transmitter.
97 Citations
24 Claims
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1. A monitoring system for an aircraft engine, comprising:
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a plurality of wireless engine sensors associated with the aircraft engine, each wireless engine sensor configured to sense an engine parameter as engine data and transmit wirelessly the engine data regarding the sensed engine parameter and receive engine data to change the respective operation of the engine parameter sensing; an engine monitoring module comprising; a housing mounted at the aircraft engine, a wireless sensor processor and wireless sensor transceiver mounted within the housing and configured to receive the engine data regarding sensed engine parameters from the wireless engine sensors; a first wireless transceiver carried by the housing, a memory carried by the housing, a processor carried by the housing and coupled to the memory, the wireless sensor processor and wireless sensor transceiver, and the first wireless transceiver and configured to; collect and store in said memory engine data relating to engine parameters sensed during operation of the aircraft engine by the plurality of wireless engine sensors; transmit the engine data via the first wireless transceiver over a wireless communications signal into the aircraft, a wireless local area network (LAN) communications unit located within the aircraft and forming a wireless access point and wireless LAN within the aircraft and configured to transmit the engine data via the wireless LAN from the wireless LAN communications unit into the aircraft for further processing and receive and transmit to the engine monitoring module engine data regarding engine parameter sensing for transmission to the wireless engine sensors via the wireless sensor processor and wireless sensor transceiver; and wherein selected ones of the plurality of wireless engine sensors receive the engine data and change the operation of a respective sensor for a different engine parameter sensing operation. - View Dependent Claims (2, 3, 4, 5, 6)
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7. A monitoring system for an aircraft engine, comprising:
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a plurality of wireless engine sensors associated with the aircraft engine, each wireless engine sensor configured to sense an engine parameter as engine data and transmit wirelessly the engine data regarding the sensed engine parameter and receive engine data to change the respective operation of the engine parameter sensing; an engine monitoring module comprising; a housing mounted at the aircraft engine, a wireless sensor processor and wireless sensor transceiver mounted within the housing and configured to receive the engine data regarding sensed engine parameters from the wireless engine sensors; a first wireless transceiver carried by the housing, a memory carried by the housing, a processor carried by the housing and coupled to the memory, the wireless sensor processor and wireless sensor transceiver, and the first wireless transceiver and configured to; collect and store in said memory engine data relating to engine parameters sensed during operation of the aircraft engine by the plurality of wireless engine sensors and transmit the engine data via the first wireless transceiver over a wireless communications signal into the aircraft; a wireless local area network (LAN) communications unit located within the aircraft and forming a wireless access point and wireless LAN within the aircraft and configured to transmit the engine data via the wireless LAN from the wireless LAN communications unit into the aircraft for further processing and receive and transmit to the engine monitoring module engine data regarding engine parameter sensing to the engine monitoring module and to the wireless engine sensors via the wireless sensor processor and wireless sensor transceiver; and wherein selected ones of the plurality of wireless engine sensors receive the engine data and change the operation of a respective sensor for a different engine parameter sensing operation. - View Dependent Claims (8, 9, 10, 11, 12, 13, 14, 15)
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16. A method of monitoring an aircraft engine, comprising:
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mounting a plurality of wireless engine sensors at the aircraft engine, each wireless engine sensor configured to sense an engine parameter as engine data and transmit the engine data regarding the sensed engine parameter and receive engine data to change the respective operation of the engine parameter sensing; and mounting an engine monitoring module at the aircraft engine, said engine monitoring module comprising a housing mounted at the aircraft engine, a wireless sensor processor and wireless sensor transceiver mounted within the housing and configured to receive engine data regarding sensed engine parameters from the wireless engine sensors, a first wireless transceiver carried by the housing, a memory carried by the housing, a processor carried by the housing and coupled to the memory, the wireless sensor processor and wireless sensor transceiver, and the first wireless transceiver; forming a wireless local area network (LAN) within the aircraft by locating a wireless LAN communications unit comprising a wireless access point and wireless communications unit within the aircraft; collecting and storing in said memory engine data relating to engine parameters sensed during operation of the aircraft engine by the plurality of wireless engine sensors; transmitting the engine data via the first wireless transceiver via the wireless LAN to the wireless communications unit; transmitting the engine data to a location into the aircraft via the wireless LAN for further processing and receiving and transmitting to the engine monitoring module data regarding engine parameter sensing; and transmitting to selected ones of the wireless engine sensors via the wireless sensor processor and wireless sensor engine data for changing the operation of a respective sensor for different engine parameter sensing operation. - View Dependent Claims (17, 18, 19, 20, 21, 22, 23, 24)
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Specification