GAS TURBINE ARRANGEMENT AND METHOD FOR RETROFITTING SAME
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United States of America Patent
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Issued Date -
Jan 26, 2012
app pub date -
Jul 8, 2011
filing date -
Jul 22, 2010
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Abstract
A gas turbine arrangement includes a compressor, a combustion chamber and a turbine connected to one another. A casing housing the compressor has flanges connectable to pipes providing secondary air to at least one of the combustion chamber and the turbine. The flanges define passages having an asymmetric cross section. A method for retrofitting a gas turbine arrangement is also provided.
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