Gas turbine engine power plant

Power plants – Reaction motor – Interrelated reaction motors

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Details

60229, 60232, 23926533, F02K 306

Patent

active

043275486

ABSTRACT:
A ducted fan propulsion plant has a reversible-pitch fan driven by a core gas turbine engine and housed in a duct which terminates at its downstream end in an outlet nozzle defined between two semi-cylindrical shells. The shells are mounted for movement hydraulically both axially and angularly to define an increased effective nozzle area for take-off. Upon further rearward axial displacement the shells adopt a reverse-thrust position to define air inlets to the fan when the fan blade pitch is reversed.

REFERENCES:
patent: 2680948 (1954-06-01), Greene
patent: 2840984 (1958-07-01), Laucher
patent: 3820719 (1974-06-01), Clark
patent: 4132068 (1979-01-01), Johnston

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