Method and apparatus for increasing the pressure of cooling fluid within a gas turbine engine
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United States of America Patent
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Jun 5, 2007
Grant Date -
Dec 8, 2005
app pub date -
Jun 8, 2004
filing date -
Jun 8, 2004
priority date (Note) -
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Abstract
A system located with the housing of a gas turbine engine for increasing the pressure of working fluid from the compressor that will be utilized to cool a component. In one form the system includes a pump rotatable with a turbine component to increase the pressure of the working fluid.
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