A lever control system integrates taxi operation using an electric motor in an aircraft with speed control of a jet engine in the same aircraft. The lever control system provides a smooth transition between the electric motor system used for aircraft taxi operation, and a jet engine system used to fly the aircraft. The lever control system may include a reverse lockout mechanism to prevent unintended reverse taxi movement of the aircraft.
CONTROL PANEL INTEGRATION INTO AIRCRAFT THROTTLE CONTROL
02.07.2015
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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