Gas turbine engine with dynamic data recording
AssigneeRaytheon Technologies Corporation
InventorsWilliam C. Lamberti, Paul Raymond Scheid, Jason E. Posniak
Life of this patent
Estimating the term…
Loading patent…
AssigneeRaytheon Technologies Corporation
InventorsWilliam C. Lamberti, Paul Raymond Scheid, Jason E. Posniak
Estimating the term…
A communication adapter of a gas turbine engine of an aircraft includes a communication interface configured to wirelessly communicate with an offboard system and to communicate with an engine control of the gas turbine engine, a memory system, and processing circuitry. The processing circuitry is configured to receive an engine control dynamic data recording request from the offboard system, confirm an authentication between the communication adapter and the engine control, transfer the engine control dynamic data recording request received at the communication adapter from the offboard system to the engine control based on the authentication, and transmit an update completion confirmation of the engine control from the communication adapter to the offboard system based on a confirmation message from the engine control.
A communication adapter of a gas turbine engine of an aircraft, the communication adapter comprising:
A method comprising:
A gas turbine engine of an aircraft, the gas turbine engine comprising:
Dependencies are inferred from the claim text.