CPC H04L 67/125 (2013.01) [F01D 21/003 (2013.01); F02C 9/00 (2013.01); G07C 5/008 (2013.01); G07C 5/0808 (2013.01); G07C 5/0841 (2013.01); H04B 7/18506 (2013.01); F05D 2220/323 (2013.01); F05D 2260/80 (2013.01); F05D 2270/80 (2013.01); G07C 5/006 (2013.01); H04L 2012/4028 (2013.01)] | 20 Claims |
1. A communication adapter of a gas turbine engine of an aircraft, the communication adapter comprising:
an internal sensor system comprising a plurality of sensors within the communication adapter;
a memory system; and
processing circuitry configured to:
receive a plurality of time series data at the communication adapter from an engine control of the gas turbine engine;
record a plurality of internal sensor data of the internal sensor system;
correlate the time series data with the internal sensor data based on an alignment in time to form an enhanced data set; and
transmit the enhanced data set from the communication adapter to an offboard system.
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