CONTROL DEVICE FOR AIRCRAFT

A control device is provided for an aircraft, the aircraft having at least one undercarriage with one or more undercarriage wheels. A control mechanism interacts with the aircraft undercarriage and is configured to turn the undercarriage wheels relative to the longitudinal axis of the aircraft. The...

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Bibliographische Detailangaben
Hauptverfasser:	MEISSNER, UTE, MARITA, HAHN, KLAUS-UWE
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL AVIATION BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OFVEHICLES TRANSPORTING VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES VEHICLES IN GENERAL
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Beschreibung
Zusammenfassung:	A control device is provided for an aircraft, the aircraft having at least one undercarriage with one or more undercarriage wheels. A control mechanism interacts with the aircraft undercarriage and is configured to turn the undercarriage wheels relative to the longitudinal axis of the aircraft. The control device has an alignment unit which is connected to the control mechanism and which is configured to control the turning of the undercarriage wheels by means of the control mechanism during at least one part of the landing or take-off phase of the aircraft in such a way that the running direction of the undercarriage wheels is aligned in the direction of a fixed point which may be a corrected fixed point situated below a fixed point by a compensation angle.