WIRELESS ENGINE MONITORING SYSTEM WITH MULTIPLE HOP AIRCRAFT COMMUNICATIONS CAPABILITY AND ON-BOARD PROCESSING OF ENGINE DATA
First Claim
1. A monitoring system for an aircraft engine, comprising:
- an engine monitoring module comprising;
a housing configured to be mounted at the aircraft engine,a first wireless transmitter carried by the housing,a memory carried by the housing,a processor carried by the housing and coupled to the memory and the first wireless transmitter and configured to;
collect and store in said memory engine data relating to at least one engine parameter sensed during operation of the aircraft engine by a plurality of engine sensors and transmit the engine data via the first wireless transmitter;
a wireless receiver located within the aircraft and configured to receive the engine data transmitted from the first wireless transmitter; and
a second wireless transmitter located within the aircraft and operatively connected to the wireless receiver and configured to transmit the engine data.
1 Assignment
0 Petitions
Accused Products
Abstract
An engine monitoring module includes a housing configured to be mounted at the aircraft engine and a first wireless transmitter 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 relating to at least one engine parameter sensed during operation of the aircraft engine by a plurality of engine sensors that transmit the engine data via the first wireless transmitter. A wireless receiver is located within the aircraft and configured to receive the engine data transmitted from the first wireless transmitter. A second wireless transmitter is located within the aircraft and operatively connected to the wireless receiver and configured to receive and transmit the engine data.
40 Citations
29 Claims
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1. A monitoring system for an aircraft engine, comprising:
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an engine monitoring module comprising; a housing configured to be mounted at the aircraft engine, a first wireless transmitter carried by the housing, a memory carried by the housing, a processor carried by the housing and coupled to the memory and the first wireless transmitter and configured to; collect and store in said memory engine data relating to at least one engine parameter sensed during operation of the aircraft engine by a plurality of engine sensors and transmit the engine data via the first wireless transmitter; a wireless receiver located within the aircraft and configured to receive the engine data transmitted from the first wireless transmitter; and a second wireless transmitter located within the aircraft and operatively connected to the wireless receiver and configured to transmit the engine data. - View Dependent Claims (2, 3, 4, 5)
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6. A monitoring system for an aircraft engine, comprising:
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an engine monitoring module comprising; a housing configured to be mounted at the aircraft engine, a first wireless transmitter carried by the housing, a memory carried by the housing, a processor carried by the housing and coupled to the memory and the first wireless transmitter and configured to; collect and store in said memory engine data relating to at least one engine parameter sensed during operation of the aircraft engine by a plurality of engine sensors and transmit the engine data via the first wireless transmitter; and a wireless receiver located within the aircraft and configured to receive the engine data transmitted from the first wireless transmitter, and further comprising a processor located within the aircraft and configured to receive the engine data from the wireless receiver during the flight of the aircraft and process the engine data and determine engine operating parameters. - View Dependent Claims (7, 8, 9, 10, 11, 12, 13)
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14. A method of monitoring an aircraft engine, comprising:
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mounting an engine monitoring module at the aircraft engine, said engine monitoring module comprising a housing that is mounted at the aircraft engine, a first wireless transmitter carried by the housing, a memory carried by the housing, and a processor coupled to the memory and the first wireless transmitter; collecting and storing in the memory engine data relating to at least one engine parameter sensed during operation of the aircraft engine by a plurality of engine sensors; transmitting the engine data via the first wireless transmitter to a wireless receiver located within the aircraft; and transmitting the engine data via a second wireless transmitter located within the aircraft. - View Dependent Claims (15, 16, 17, 18, 19)
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20. A method of monitoring an aircraft engine, comprising:
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mounting an engine monitoring module at the aircraft engine, said engine monitoring module comprising a housing that is mounted at the aircraft engine, a first wireless transmitter carried by the housing, a memory carried by the housing, and a processor coupled to the memory and the first wireless transmitter; collecting and storing in the memory engine data relating to at least one engine parameter sensed during operation of the aircraft engine by a plurality of engine sensors; transmitting the engine data via the first wireless transmitter to a wireless receiver located within the aircraft having a processor connected thereto; and processing the engine data during the flight of the aircraft to determine engine operating parameters. - View Dependent Claims (21, 22, 23, 24, 25, 26, 27, 28, 29)
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Specification