GAS TURBINE ARRANGEMENT AND METHOD FOR RETROFITTING SAME
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.
1 . A gas turbine arrangement comprising:
a compressor, a combustion chamber and a turbine connected to one another; and
a casing housing the compressor,
wherein the casing includes flanges connectable to pipes providing secondary air to at least one of the combustion chamber and the turbine,
wherein the flanges define passages having an asymmetric cross section.
2 . The gas turbine arrangement as claimed in claim 1 , wherein the asymmetric cross section is an oval cross section.
3 . A method for retrofitting a gas turbine arrangement including a compressor, a combustion chamber and a turbine connected to one another, and a casing housing the compressor, the casing having at least one flange defining passages having a symmetrical cross section, the at least one flange being connected to pipes providing secondary air to at least one of the combustion chamber and the turbine, wherein the method comprises:
replacing the at least one flange defining passages having the symmetrical cross section with at least one flange defining passages having an asymmetrical cross section.
4 . The method as claimed in claim 3 , wherein the replacing of the at least one flange comprises replacing the at least one flange having the symmetrical cross section with at least one flange defining passages having an asymmetrical cross section which is an oval cross section.
5 . The method as claimed in claim 3 , wherein the replacing comprises cutting a part of the casing having the at least one flange defining passages having the symmetrical cross section and connecting the at least one flange defining passages having the asymmetrical cross section to the part of the casing from which the at least one flange defining passages having the symmetrical cross section was cut.
6 . The method as claimed in claim 5 , wherein the connecting comprises welding the at least one flange defining passages having the asymmetrical cross section to the part of the casing from which the at least one flange defining passages having the symmetrical cross section was cut.
7 . The method as claimed in claim 3 , wherein the replacing comprises removing a portion of the casing including the at least one flange defining passages having the symmetrical cross section, and affixing the at least one flange defining passages having the asymmetrical cross section to the casing.
8 . The method as claimed in claim 7 , wherein the at least one flange defining passages having the asymmetrical cross section is affixed to the casing by means of a removable connection mechanism.
9 . The method as claimed in claim 7 , wherein the removable connection mechanism includes a bolt.