ACTUATOR ARRANGEMENT AND WING ASSEMBLY FOR AN AIRCRAFT

ACTUATOR ARRANGEMENT AND WING ASSEMBLY FOR AN AIRCRAFT

In order to improve aerodynamic properties of an aircraft (10) and reduce drag and weight, the invention proposes an actuator arrangement (20). In this arrangement, the high-lift device support (22) that supports and guides movement of a high-lift device (24), such as a flap, is in axial alignment w...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Andreani, Luc, Lorenz, Florian
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:In order to improve aerodynamic properties of an aircraft (10) and reduce drag and weight, the invention proposes an actuator arrangement (20). In this arrangement, the high-lift device support (22) that supports and guides movement of a high-lift device (24), such as a flap, is in axial alignment with a control actuator assembly (46) that controls one or more control surfaces (40). With this a single support fairing (30) is sufficient for covering both the track member (26) and the control actuator assembly (46), thereby allowing for reduced drag and weight.