Gas turbine exhaust diffuser
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United States of America Patent
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Jul 19, 2011
Grant Date -
Oct 28, 2010
app pub date -
Aug 4, 2006
filing date -
Aug 4, 2005
priority date (Note) -
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Abstract
A gas turbine including an exhaust diffuser with a flow splitter located between the inner wall and outer wall defining the exhaust gas flow path. In one aspect the flow splitter being moveable independent of the walls defining the exhaust gas flow path to allow for differing thermal movement between the components. In one form a structural member extends from a wall and is coupled to the flow splitter. The wall can have an opening for the through which the structural member is allowed to pass. In some forms a plurality of structural members can be coupled to the flow splitter. In other forms the flow splitter can be independently movable relative to the wall.
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