DISPOSICION DE INTERFAZ ENTRE DOS COMPONENTES DE UNA ESTRUCTURA DE UNA AERONAVE

DISPOSICION DE INTERFAZ ENTRE DOS COMPONENTES DE UNA ESTRUCTURA DE UNA AERONAVE

Interface arrangement between a first component (11) and a second component (21) of an aircraft structure having an aerodynamic contour, such as a wing skin and a wing leading edge panel, the first component (11) having a joggle so that it includes a first area (13) which surface (15) belongs to the...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: OUTON HERNANDEZ, IGNACIO, RODRIGO CABALLERO, NURIA, PINA LOPEZ, JOSE MARIA
Format: Patent
Sprache:spa
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:Interface arrangement between a first component (11) and a second component (21) of an aircraft structure having an aerodynamic contour, such as a wing skin and a wing leading edge panel, the first component (11) having a joggle so that it includes a first area (13) which surface (15) belongs to the aircraft aerodynamic contour and a second area (17) where the joint with the second component (21) takes place, the second component (21) having a surface (23) belonging to the aircraft aerodynamic contour, in which the second component (21) includes a chamfer-shaped ending (29) that extends beyond the overlapping area (27) where the joint with the first component (11) takes place so that the gaps (26, 28) between the first component (11) and the second component (21) are minimized.