F - Mech Eng,Light,Heat,Weapons – 02 – K
Patent
F - Mech Eng,Light,Heat,Weapons
02
K
F02K 1/70 (2006.01)
Patent
CA 2223564
12 A dual-flow jet turbine engine thrust reverser comprises pivoting doors (7) integrated in forward thrust in the outer wall of the annular duct (15) and constituting flow-deflecting obstacles. A shaped part (21) attached to the fixed reverser structure is positioned in the cavity created below the door in forward thrust and forms a deflector vane improving the direction of the reverse flow.
12 Un inverseur de poussée de turboréacteur à double flux comporte des portes pivotantes (7) intégrées en jet direct dans la paroi extérieure de conduit annulaire (15) et constituant des obstacles de déviation de flux. Une pièce profilée (21) reliée à la structure fixe d'inverseur est disposée dans la cavité créée sous la porte en jet direct et forme une aube déflectrice améliorant l'orientation du flux d'inversion.
Gonidec Patrick
Rouyer Pascal Gerard
Vauchel Guy Bernard
Hispano-Suiza
Hispano-Suiza Aerostructures
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