Self stowing thrust reverser

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

Patent

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Details

F02K 3/02 (2006.01) F02K 1/70 (2006.01)

Patent

CA 2515888

A thrust reverser (36) includes forward and aft louvers (54, 56) pivotally mounted in a compartment (50) defining a flow tunnel (52) through the outer and inner skins (38, 40) of a fan nacelle (16). An aft flap (60) is integrally joined to the aft louver (56) for rotation therewith. A unison link (64) joins together the forward and aft louvers (54, 56). And, an actuator (66) is joined to the louvers for rotation thereof between a stowed position in which the louvers and flap are closed in the nacelle skins and a deployed position in which the louvers and flap are pivoted open from the skins.

L'invention concerne un inverseur de poussée (36) comprenant des persiennes avant et arrière (54, 56) montées pivotantes dans un compartiment (50) définissant un tunnel d'écoulement (52) à travers les revêtements extérieur et intérieur (38, 40) d'une nacelle de soufflante (16). Un volet arrière (60) est raccordé solidaire à la persienne arrière (56), de sorte à tourner avec cette dernière. Une liaison de conjugaison (64) raccorde les persiennes avant et arrière (54, 56). Un actionneur (66) est également raccordé aux persiennes afin de les faire tourner entre une position arrimée, dans laquelle les persiennes et le volet sont fermés dans les revêtements de nacelle, et une position déployée, dans laquelle les persiennes et le volet sont tournés et ouverts dans les revêtements.

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