Variable stator vane assembly with magnetic actuation rotor for gas turbine engines
AssigneeRolls-Royce North American Technologies Inc.
InventorsTimothy Unton, Andrew Eifert, Michael Moser
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AssigneeRolls-Royce North American Technologies Inc.
InventorsTimothy Unton, Andrew Eifert, Michael Moser
Estimating the term…
A vane assembly includes a casing, vanes, and an actuator assembly. The vanes are arranged within the casing and are rotatably coupled to the casing for rotation relative thereto and configured to rotate about their pitch axes. The actuator assembly is arranged radially outward of the casing and includes an annular ring surrounding the casing and coupled to the vanes, a magnet arranged on the ring, and a stator spaced apart from the magnet. The ring is configured to rotate the vanes about their pitch axes in response to rotation of the ring about the central axis and the stator is configured to selectively rotate the magnet and ring about the central axis. The stator is configured to create a magnetic field which causes annular movement of the ring via interaction with the magnet.
A vane assembly for a gas turbine engine, the vane assembly comprising
A vane assembly for a gas turbine engine, the vane assembly comprising
17-19. (canceled)
A method, comprising
Dependencies are inferred from the claim text.