Nacelle thrust reverser and nacelle equipped with at least one reverser
Nacelle thrust reverser and nacelle equipped with at least one reverser
- Neue Suche nach: CARUEL PIERRE
- Neue Suche nach: CARUEL PIERRE
The present invention relates to a turbojet engine nacelle thrust reverser and to a nacelle equipped with at least one thrust reverser as aforementioned, said thrust reverser comprising: at least one outer cowl (2), produced as two half-cowls (3) articulated on hinges (5), capable of translational movement from a position referred to as the closed position into at least one position referred to as open, first actuating means (8) for actuating the translational movement of the downstream frame (18), second actuating means (9) for actuating the rotation of each half-cowl (3), locking/unlocking means (7) that lock/unlock the half-cowls (3) relative to one another, thrust reversal means (13) comprising at least cascades of deflection veins (14) supported at their upstream end (15) by an upstream frame (16) and at their downstream end (17) by a downstream frame (18); and enclosed in a shroud (19) formed by a fan casing (20) and a fan cowl (11), means (21) of connection between the downstream frame (18) and the external cowl (2).
Dokumentinformationen
Nacelle thrust reverser and nacelle equipped with at least one reverser
2015-08-19
Patent
Elektronische Ressource
Englisch
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