SYSTEM FOR INCREASING CONTROLLABILITY FOR AN AIRCRAFT

SYSTEM FOR INCREASING CONTROLLABILITY FOR AN AIRCRAFT

The system includes deflection transmission means (16) to provide a deflection position of the high-lift device (8) for each setting angle position of an adjustable HTP (2). Preferably, the deflection transmission means (18,20,23) comprise essentially of a mechanical linkage connected between the hi...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: VELA ORGE, PILAR, NAMER, ARNAUD, PASCUAL FUERTES, ANGEL, SIMÓN CALERO, FRANCISCO JAVIER
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:The system includes deflection transmission means (16) to provide a deflection position of the high-lift device (8) for each setting angle position of an adjustable HTP (2). Preferably, the deflection transmission means (18,20,23) comprise essentially of a mechanical linkage connected between the high-lift device (8) and the aircraft (1).