Electrical augmentation of a gas turbine engine
AssigneeSikorsky Aircraft Corporation
InventorsFrederick L. Bourne, Mark Denton Bystry, Jr., Joseph Lawrence Simonetti
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AssigneeSikorsky Aircraft Corporation
InventorsFrederick L. Bourne, Mark Denton Bystry, Jr., Joseph Lawrence Simonetti
Estimating the term…
One aspect is an electrical augmentation system for a gas turbine engine. The electrical augmentation system includes an electric motor operably coupled to a shaft of the gas turbine engine, and an energy storage device operable to provide a temporary increased current source to the electric motor. The electrical augmentation system includes a control system having a torque demand anticipation circuit operable to determine an anticipated torque increase condition for the gas turbine engine. Based on the anticipated torque increase condition, the torque demand anticipation circuit commands a temporary torque increase by the electric motor using the energy storage device.
An electrical augmentation system for a gas turbine engine, the electrical augmentation system comprising:
A method of electrical augmentation for a gas turbine engine, the method comprising:
A gas turbine engine comprising:
Dependencies are inferred from the claim text.