CONTROL SYSTEM FOR CONTROLLING A LANDING GEAR DRIVE SYSTEM

A control system for controlling a landing gear drive system for driving rotation of an aircraft wheel is disclosed having a control panel with a controller having a forward motion setting and a zero speed setting, a control unit for receiving a control input from the controller, and for providing a...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser:	ROMANA, Louis Emmanuel
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CONTROLLING COSMONAUTICS ELECTRIC EQUIPMENT OR PROPULSION OF ELECTRICALLY-PROPELLEDVEHICLES ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES, IN GENERAL HELICOPTERS MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES PERFORMING OPERATIONS PHYSICS REGULATING SIGNALLING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRAFFIC CONTROL SYSTEMS TRANSPORTING VEHICLES IN GENERAL
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Beschreibung
Zusammenfassung:	A control system for controlling a landing gear drive system for driving rotation of an aircraft wheel is disclosed having a control panel with a controller having a forward motion setting and a zero speed setting, a control unit for receiving a control input from the controller, and for providing a torque command to be applied to the wheel, and a speed sensor for sensing an aircraft taxi speed and for providing an indication of the aircraft taxi speed to the control unit. When the controller is moved from the forward motion setting to the zero speed setting, the control unit provides a torque command to the drive system to provide zero forwards driving torque to the wheel, and a braking command to apply a braking torque to the wheel.