DEVICE FOR CONTROLLING AIR INTAKE FLAPS USING A MULTILAYER PIEZOELECTRIC ACTUATOR

An electric actuator for inlet guide vanes of a gas turbine engine, the electric actuator including a fixed portion secured to a stationary portion of the engine and a movable portion that is mechanically connected to the inlet guide vanes, stationary electromagnets distributed at regular intervals...

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Bibliographic Details
Main Authors KLONOWSKI, Thomas, MOUTAUX, Antoine, VONFELT, Jean-Julien, Camille
Format Patent
LanguageEnglish
French
German
Published 17.07.2019
Subjects
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Summary:An electric actuator for inlet guide vanes of a gas turbine engine, the electric actuator including a fixed portion secured to a stationary portion of the engine and a movable portion that is mechanically connected to the inlet guide vanes, stationary electromagnets distributed at regular intervals around the periphery of the movable portion and fastened to the fixed portion, and movable electromagnets arranged between the stationary electromagnets, each movable electromagnet being secured on either side to first and second piezoelectric elements, the movable electromagnets and the first and second piezoelectric elements having a degree of freedom of movement relative to the movable portion and having inside faces forming a common line of contact that is tangential to the movable portion.
Bibliography:Application Number: EP20170768490