ANTI-TORQUE SYSTEM FOR A HELICOPTER AND METHOD FOR CONTROLLING AN ANTI-TORQUE SYSTEM FOR A HELICOPTER

An anti-torque system (10) for a helicopter (1) is described that comprises: an electric power supply unit (15); at least one first rotor (17), operatively connected to an electric power supply unit (15) and operable by the electric power supply unit (15) so as to rotate with a first variable angula...

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Bibliographic Details
Main Authors BOTTASSO, Luigi Maria, BRUNETTI, Massimo, WELLER, Gary, GOH, Chee Su
Format Patent
LanguageEnglish
French
German
Published 26.06.2019
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:An anti-torque system (10) for a helicopter (1) is described that comprises: an electric power supply unit (15); at least one first rotor (17), operatively connected to an electric power supply unit (15) and operable by the electric power supply unit (15) so as to rotate with a first variable angular speed; and at least one second rotor (25) operatively connected to electric power supply unit (15) and operable by the electric power supply unit (15) so as to rotate with a second variable angular speed.
Bibliography:Application Number: EP20170210094