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US 2024/0275239 A1Published application
Power system
AssigneeHamilton Sundstrand Corporation
InventorDavid James Tate
Life of this patent
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Abstract
A power system for an aircraft comprises: a motor-generator component; a shaft, wherein the motor-generator component is connectable to the shaft, the shaft connectable to an additional component of the aircraft to for torque transfer with the additional component; and a de-coupler operable to disconnect the motor-generator component from the shaft, wherein the motor-generator component is located between the de-coupler and the additional component in use.
Claims15
A power system for an aircraft, the power system comprising:
- a motor-generator component;
- a shaft, wherein the motor-generator component is connectable to the shaft, the shaft connectable to an additional component of the aircraft to for torque transfer with the additional component;
- and
- a de-coupler operable to disconnect the motor-generator component from the shaft, wherein the motor-generator component is located between the de-coupler and the additional component in use.
1 more element
Dependencies are inferred from the claim text.