Fluid flow reversing apparatus
AssigneeROLLS-ROYCE plc
InventorHenry Tubbs
Life of this patent
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Abstract
In a multi stage ducted fan or ducted propeller gas turbine engine, a fan flow exit path is provided in the cowl between axially adjacent stages of blades. The stage of blades downstream of the exit are each pivotable to attitudes which on continued rotation of the stage, induces a reverse flow of ambient air into the duct via the nozzle. The normal and reversed airflows meet under the exit path and pass therethrough to atmosphere. The need for blocker doors in the duct is obviated and energy is imported to the fan air passing through the exit by both stages of blades.
Claims4
Fluid flow reversing apparatus in the fan duct of a ducted fan gas turbine engine comprising a cowl which defines the outer wall of the fan duct, a fluid flow exit path in the cowl, a first stage of rotatable blades in the duct and upstream of the fluid flow exit path, a second stage of rotatable blades in the duct and downstream of the fluid flow exit path means for covering and uncovering the fluid flow exit path and wherein each of the blades of the second stage of rotatable blades are pivotable about a longitudinal axis thereof to an attitude which on continued rotation of the second stage, induces a reversed flow of ambient air via the duct nozzle, in opposition to the flow induced by the first stage of rotatable blades, which flows meet radially inwardly of the fan flow exit path and passes therethrough when it is uncovered.
Dependencies are inferred from the claim text.