초록 ▼

A gas turbine engine comprising a bypass duct defined radially outwardly by a nacelle and radially inwardly by a core engine casing. The nacelle comprises a thrust reverser unit having at least one blocker door rotatably attached to a static part and slidably connected to a translating part. The tra

A gas turbine engine comprising a bypass duct defined radially outwardly by a nacelle and radially inwardly by a core engine casing. The nacelle comprises a thrust reverser unit having at least one blocker door rotatably attached to a static part and slidably connected to a translating part. The translating part is arranged to move between a stowed position and a deployed position and in the deployed position the blocker door spans the bypass duct. In the stowed position the blocker door is stowed inside the translating part and does not form part of an airwash surface of the bypass duct.

대표청구항 ▼

The invention claimed is: 1. A gas turbine engine having a core engine casing, and being surrounded by a nacelle that defines a bypass duct, the bypass duct being defined radially outwardly by the nacelle and radially inwardly by the core engine casing, the nacelle including a thrust reverser unit,

The invention claimed is: 1. A gas turbine engine having a core engine casing, and being surrounded by a nacelle that defines a bypass duct, the bypass duct being defined radially outwardly by the nacelle and radially inwardly by the core engine casing, the nacelle including a thrust reverser unit, the thrust reverser unit comprising:a static part and a translating part;a slider ramp located on the translating part; andat least one blocker door rotatably attached to the static part and in slideable contact with the translating part, the translating part being arranged to move between a stowed position and a deployed position, in the deployed position the blocker door spans the bypass duct, wherein the at least one blocker door is in slideable contact with the slider ramp located on the translating part.