F - Mech Eng,Light,Heat,Weapons – 02 – K
Patent
F - Mech Eng,Light,Heat,Weapons
02
K
F02K 1/56 (2006.01) F02K 1/70 (2006.01)
Patent
CA 2239465
A thrust reverser for a jet turbine engine comprises pivoting hollow doors (3) integrated in forward thrust with the external fairing of the nacelle and constituting in reverse thrust obstacles for deflecting flow to form scoops. A movable deflector (24) is attached to each door (3). When the door opens (3), the deflector (24) is positioned above the outer surface of the outer panel (4) of the door (3) so as to avoid interference between the exhaust flow of the door (3) and the flow deflected outside the door (3).
Un inverseur de poussée de turboréacteur comporte des portes creuses pivotantes (3), intégrées en jet direct dans le capotage extérieur de la nacelle et constituant en jet inversé des obstacles de déviation de flux en formant écopes. Un déflecteur mobile (24) est associé à chaque porte (3). Lors de l'ouverture de la porte (3), le déflecteur (24) se place au-dessus de la surface externe du panneau externe (4) de la porte (3) de manière à éviter l'interférence entre le flux d'échappement de la porte (3) et le flux dévié à l'extérieur de la porte (3).
Gonidec Patrick
Portal Jean Fabrice Marcel
Studer Vincent Joseph Rodolphe
Vauchel Guy Bernard
Goudreau Gage Dubuc
Societe Hispano Suiza Aerostructures
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