METHOD AND A CONTROL UNIT FOR CONTROLLING ACTUATION OF A FOLDABLE WING TIP SECTION OF A WING OF AN AIRCRAFT

METHOD AND A CONTROL UNIT FOR CONTROLLING ACTUATION OF A FOLDABLE WING TIP SECTION OF A WING OF AN AIRCRAFT

A method to control folding of a wing tip section about a fixed base wing section by a control system that automatically determines whether: (i) a command signal is received to fold the wing tip section, (ii) a first condition indicating signal indicates that the aircraft is on the ground; (iii) the...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: JEGMINAT, Svenja, DEGE, Saskia, GUILHAMET, Jean, JONES, Aeron Charles, NIENABER, Frank
Format: Patent
Sprache:eng
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:A method to control folding of a wing tip section about a fixed base wing section by a control system that automatically determines whether: (i) a command signal is received to fold the wing tip section, (ii) a first condition indicating signal indicates that the aircraft is on the ground; (iii) the current speed of the aircraft is no greater than a preset maximum speed, and (iv) the aircraft is not at gate in an airport.