Nacela compreendendo uma primeira capota e uma segunda capota

The invention relates to a nacelle (1) that comprises a first cowling (7) and a second cowling (9) capable of covering in particular the area (15) located around the casing of the fan (19) of a turbojet engine (3). The nacelle further includes an intermediate cowling (23) attached to said first cowl...

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Bibliographische Detailangaben
Hauptverfasser:	GÉRARD CLERE, ANDRÉ BAILLARD, JEAN-PHILIPPE JORET
Format:	Patent
Sprache:	por
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 invention relates to a nacelle (1) that comprises a first cowling (7) and a second cowling (9) capable of covering in particular the area (15) located around the casing of the fan (19) of a turbojet engine (3). The nacelle further includes an intermediate cowling (23) attached to said first cowling (7) so as to sandwich a mast (5) holding said turbojet engine (3). The second cowling (9) is mounted onto the intermediate cowling (23) via removable fastening means.