Method and arrangement for providing a gas turbine, and engine-braking therefore
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United States of America Patent
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Apr 26, 2005
Grant Date -
Jun 3, 2004
app pub date -
Oct 6, 2003
filing date -
Apr 6, 2001
priority date (Note) -
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Abstract
Method and arrangement for providing a gas turbine (1) having a first compressor (2), a combustion chamber (16) and a first turbine (11), the turbine being adapted to drive the compressor via a first shaft (10a, 10b). The gas turbine also has a bleed valve (12) arranged upstream of the first turbine for conducting part of a gas compressed by the compressor past it during engine braking. The invention also relates to a method for engine-braking a gas turbine.
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