Turbine with exhaust vortex disrupter and annular recuperator
Number of patents in Portfolio can not be more than 2000
United States of America Patent
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-
Oct 21, 2003
Grant Date -
Jul 17, 2003
app pub date -
Oct 15, 2001
filing date -
Nov 2, 2000
priority date (Note) -
Expired
status (Latency Note)
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Abstract
In a turbine engine with an annular recuperator surrounding the turbine, exhaust gas is directed from the turbine to the recuperator by a generally curved exhaust dome. A vortex disrupter structure extends from the exhaust dome to a point distal of the turbine to evenly distribute the exhaust gas entering the recuperator and sustain diffusion of the exhaust gas to increase the expansion ratio across the turbine.
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