Turbine engine tip clearance control utilizing electric machine
AssigneeRtx Corporation
InventorsGraham R. Philbrick, Gary Collopy, John P. Virtue, Jr.
Life of this patent
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AssigneeRtx Corporation
InventorsGraham R. Philbrick, Gary Collopy, John P. Virtue, Jr.
Estimating the term…
An operating method is provided during which a command is received to increase thrust generated by a propulsor rotor from a first thrust level to a second thrust level. The propulsor rotor is operatively coupled to an engine core and an electric machine. The engine core includes a flowpath, a compressor section, a combustor section and a turbine section. The engine core is operated in a transient state to increase power output from the engine core to the propulsor rotor from a first power level to a second power level in response to the command. The electric machine is operated to boost the power output from the engine core to the propulsor rotor while the engine core is operating in the transient state. A clearance control system for the engine core is operated based on the operation of the electric machine.
An operating method, comprising:
Dependencies are inferred from the claim text.