Attachment system of aircraft components

Attachment system of aircraft components

An attachment system for attaching a component (11) such as a vertical tail plane to a fuselage (27) of an aircraft; the component (11) being structured as a box comprising front and rear spars (13, 14), ribs (15) extending from the front spar (13) to the rear spar (14), and a skin (17), and also co...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: PINA LOPEZ JOSE MARIA, SANZ MARTINEZ PABLO TIMOTEO
Format: Patent
Sprache:eng
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:An attachment system for attaching a component (11) such as a vertical tail plane to a fuselage (27) of an aircraft; the component (11) being structured as a box comprising front and rear spars (13, 14), ribs (15) extending from the front spar (13) to the rear spar (14), and a skin (17), and also comprising a plurality of intermediate spars (23) arranged to be attached to fuselage frames (33); the fuselage (27) comprising a skin (31) and frames (33) and also comprising a mounting arrangement suitable for receiving the additional spars (23) and for allowing its attachment to the frames (33).