Ducted fan gas turbine engine
AssigneeROLLS-ROYCE plc
InventorJohn A. Mullins
Life of this patent
Estimating the term…
Abstract
The downstream portions of a ducted fan, gas turbine engine are translatable to open respective gaps and allow the lateral egress of exhaust gas and fan air. The fan air outlet is upstream of the exhaust gas outlet and the translatable fan cowl portion and gas turbine engine casing cooperate to reduce the fan annulus on translation. Exhaust gas passing laterally through its outlet enters any annular space remaining between casing and cowl and prevents the passage of fan air in a downstream direction.
Claims3
A ducted fan gas turbine engine, comprising a core gas generator enclosed in a streamlined casing, a fan at the upstream end thereof, a cowl surrounding the core gas generator and fan in spaced relationship, so as to form an annular fan duct therewith, the fan duct exit nozzle plane being further upstream than the core gas generator exit nozzle plane, the downstream end portions of both the cowl and the casing being adapted for simultaneous translation to open respective gaps therein, the gap so formed in the casing being within the translatable portion of the cowl, the inner wall of the translatable portion of the cowl and the fixed casing portion being shaped so that on translation of said cowl and casing portions in a downstream direction during operation of said engine, said inner wall of the cowl portion and fixed casing portion cooperate to substantially reduce the fan duct annulus downstream of the gap in the cowl and, hot gases passing from the core gas generator via the gap in the casing complete the closure thereof, to prevent fan air from passing therethrough and means for effecting said translation.
Dependencies are inferred from the claim text.