Thrust reverser for jet turbine engine with doors held...

F - Mech Eng,Light,Heat,Weapons – 02 – K

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F02K 1/70 (2006.01) F02K 1/76 (2006.01)

Patent

CA 2223529

Un inverseur de poussée de turboréacteur à double flux comporte des portes (7) intégrées en jet direct dans la paroi extérieure du conduit annulaire (15) et pivotant sous l'action d'un vérin de commande (8) pour constituer des obstacles de déviation du flux d'inversion. Deux verrous primaires (20a, 20b) solidaires de la structure fixe amont d'inverseur et disposés de part et d'autre de la ligne centrale de porte (7) sont simultanément en contact avec la porte (7) en configuration de vol et retiennent ladite porte (7) sans désafleurement par rapport aux lignes externes et internes de nacelle.

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