Articulated fairing for nacelle members supported by these nacelle members in a closed position

Articulated fairing for nacelle members supported by these nacelle members in a closed position

The assembly (1) has an attachment device (4) including a front aerodynamic structure (24) having a cradle (40) equipped with an aerodynamic fairing (46), where the cradle is pivotally mounted on an air inlet (32) of a turbojet engine (6), and fan cowls are movably mounted on the cradle. The cradle...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: LETAY, BENOIT, TORO, ANDRES, VENET, ADRIEN
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:The assembly (1) has an attachment device (4) including a front aerodynamic structure (24) having a cradle (40) equipped with an aerodynamic fairing (46), where the cradle is pivotally mounted on an air inlet (32) of a turbojet engine (6), and fan cowls are movably mounted on the cradle. The cradle assumes a configuration in which its rear end rests on a bearing surface (60) of a mast when the cowls are in an open position, and the cradle assumes another configuration in which it is devoid of direct mechanical connection with other elements of the mast when the cowls are in a closed position.