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, SIMON CALERO, FCO. JAVIER
Format: Patent
Sprache:eng ; spa
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). Sistema de aumento de controlabilidad para una aeronave. El sistema incorpora medios (16) de transmisión de deflexión para proporcionar una posición de deflexión de un dispositivo (8) hipersustentador móvil, instalado en el HTP (2) móvil de una aeronave (1), para cada posición del ángulo de calado del HTP (2). Preferiblemente, los medios (16) de transmisión de deflexión (18, 20, 23) consisten esencialmente en una ligadura mecánica conectada entre el dispositivo (8) hipersustentador y la aeronave (1).