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
2015-07-02
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Control panel integration into aircraft throttle control
European Patent Office | 2015
|Aircraft throttle control device including a cam coupling
European Patent Office | 2017
|Automatic throttle control for business and commuter aircraft
Tema Archive | 1990
|