Gas turbine exhaust device including a jet diffuser

Power plants – Combustion products used as motive fluid – With exhaust treatment

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F02C 700

Patent

active

047488050

ABSTRACT:
A gas turbine exhaust device installed at the outlet from the guide vane stage (5) of the turbine and upstream from an exhaust duct (10), said device comprising a jet diffuser (20) having orifices (25) perforated therethrough, with the axis of the diffuser being the same as the axis of the turbine.

REFERENCES:
patent: 3185252 (1965-05-01), Lemmerman
patent: 3195678 (1965-07-01), Morgan et al.
patent: 3688865 (1972-09-01), Smith
patent: 3692140 (1972-09-01), Smith
patent: 4180141 (1979-12-01), Judd

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