F - Mech Eng,Light,Heat,Weapons – 02 – K
Patent
F - Mech Eng,Light,Heat,Weapons
02
K
F02K 1/70 (2006.01)
Patent
CA 2204824
A dual-flow jet turbine engine thrust reverser has pivoting doors (7) which are integral with the outer wall of the pod in forward thrust and which present obstacles deflecting the efflux in reverse thrust. The upstream portion of each door (7) is lined on its inner face by an upstream panel (22) ensuring smooth efflux in forward thrust. The upstream panel (22) is supported and connected by at least one link (30, 34, 35) to the fixed structure (1) of the reverser and to the door (7).
Un inverseur de poussée de turboréacteur à double flux comporte des portes pivotantes (7) intégrées dans la paroi de nacelle en jet direct et formant des obstacles de déviation de flux en jet inverse. Chaque partie amont de porte (7) est doublée sur sa face interne par un panneau amont (22) assurant un lissage de veine en jet direct. Le panneau amont (22) est supporté et relié par au moins une bielle (30,34,35) à la structure fixe (1) d'inverseur et à la porte (7).
Gonidec Patrick
Rouyer Pascal Gerard
Vauchel Guy Bernard
Goudreau Gage Dubuc
Hispano-Suiza Aerostructures
Societe Hispano-Suiza
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