An aircraft turbojet engine nacelle includes a rear section without a lower bifurcation, the rear section including a thrust reverser system, and the thrust reverser system including a movable cowl. The nacelle includes a guide system including a movable portion and a fixed portion, the movable portion being secured in translation to the movable cowl and cooperating with the fixed portion and the fixed portion being fixed relative to the nacelle. The guide system is disposed proximate to a position called the “6 O'clock” position. In one form, the length of the fixed portion of the guide system is larger than or equal to 50% of the length of the movable portion.
NACELLE DE TURBORÉACTEUR D'AÉRONEF, ENSEMBLE PROPULSIF ET AÉRONEF COMPORTANT UNE TELLE NACELLE
AIRCRAFT TURBOPROP NACELLE, PROPELLER ASSEMBLY AND AIRCRAFT COMPRISING SUCH A NACELLE
FLUGZEUGSTRIEBWERKSGONDEL, ANTRIEBSANORDNUNG UND FLUGZEUG BEINHALTEND SOLCHE GONDEL
2020-07-15
Patent
Elektronische Ressource
Französisch
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