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A thrust reverser for a turbofan engine having an air duct defined radially inwardly by a cowl around a gas turbine and radially outwardly in part by a fan case of the engine includes a bulkhead that is adapted to be mounted on the fan case. A translating sleeve is supported for movement axially bet

A thrust reverser for a turbofan engine having an air duct defined radially inwardly by a cowl around a gas turbine and radially outwardly in part by a fan case of the engine includes a bulkhead that is adapted to be mounted on the fan case. A translating sleeve is supported for movement axially between a closed position adjacent the bulkhead and an open position spaced apart axially to the rear of the bulkhead so as to form a outlet opening for discharge of air from the air duct. A cascade array fixed in the outlet opening has a substantially conical portion, the forward end of which is of a diameter substantially smaller than the diameter of the rearward end.

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1. A thrust reverser for a turbofan engine having an air duct defined radially inwardly by a cowl around a gas turbine and radially outwardly in part by a fan case of the engine, comprising a bulkhead adapted to be mounted on the fan case, a translating sleeve supported for movement axially betw

1. A thrust reverser for a turbofan engine having an air duct defined radially inwardly by a cowl around a gas turbine and radially outwardly in part by a fan case of the engine, comprising a bulkhead adapted to be mounted on the fan case, a translating sleeve supported for movement axially between a closed position adjacent the bulkhead and an open position spaced apart axially to the rear of the bulkhead so as to form an outlet opening for discharge of air from the air duct, and a cascade array fixed in the outlet opening, the cascade array attached to the bulkhead at a location substantially inwardly of the outer perimeter of the bulkhead, the cascade array having a substantially conical portion, wherein the forward end of the conical portion has a diameter substantially smaller than the diameter of the rearward end, and the cascade array being substantially conical throughout its axial extent. 2. The thrust reverser according to claim 1, wherein the translating sleeve has a fixed generally conical inner wall member forming a portion of the outer wall of the duct when the translating sleeve is in the closed position and forming a blocking wall for closing the duct to rearward air flow when the translating sleeve is in the open position. 3. The thrust reverser according to claim 2, wherein the fan case has an outer V-groove and the cascade array is substantially in line with the outer V-groove. 4. A thrust reverser for a turbofan engine having an air duct defined radially inwardly by a cowl around a gas turbine and radially outwardly in part by a fan case of the engine, comprising a bulkhead adapted to be mounted on the fan case, a translating sleeve supported for movement axially between a closed position adjacent the bulkhead and an open position spaced apart axially to the rear of the bulkhead so as to form an outlet opening for discharge of air from the air duct, and a cascade array fixed in the outlet opening, the cascade array having a substantially conical portion, wherein the forward end of the conical portion has a diameter substantially smaller than the diameter of the rearward end, the cascade array being substantially conical throughout its axial extent, and the fan case has an outer V-groove and the cascade array is substantially in line with the outer V-groove. 5. The thrust reverser according to claim 4, wherein the translating sleeve has a fixed generally conical inner wall member forming a portion of the outer wall of the duct when the translating sleeve is in the closed position and forming a blocking wall for closing the duct to rearward air flow when the translating sleeve is in the open position.