Gas turbine arrangement
View Patent ↗A gas turbine arrangement with heat accumulation segments ( 3 ) which are arranged, opposite moving blades, on a casing of the gas turbine, and with guide vanes ( 1 ) which are arranged adjacently to the heat accumulation segments ( 3 ) over the circumference between the casing of the gas turbine and the rotor, the moving blades and the guide vanes ( 1 ) being arranged in a hot-gas duct ( 5 ) of the gas turbine. At least one sealing element ( 4 ) arranged over the circumference is present between the guide vanes ( 1 ) and the heat accumulation segments ( 3 ) and can be separated from the hot-gas duct ( 5 ) by means of a protective shield ( 6 ).
1. A gas turbine arrangement, comprising:
a gas turbine casing defining a circumference;
a gas turbine rotor defining a circumference;
moving blades arranged over the rotor circumference;
a carrier arranged over the casing circumference;
a turbine hot-gas duct;
guide vanes arranged over the circumference of the casing;
heat accumulation segments arranged on the carrier opposite the moving blades and adjacent to the guide vanes;
at least one sealing element arranged between the guide vanes and the heat accumulation segments; and
a protective shield arranged between the at least one sealing element and the hot-gas duct, separating the at least one sealing element from the hot-gas duct.
2. The gas turbine arrangement as claimed in claim 1 , wherein the rotor defines an radially outward direction and the at least one sealing element has a W-shape oriented in the rotor radially outward direction.
3. The gas turbine arrangement as claimed in claim 1 , wherein the sealing element, the protective shield, or both, are segmented over the circumference.
4. The gas turbine arrangement as claimed in claim 3 , wherein the sealing element, the protective shield, or both, comprises between four to eight segments.
5. The gas turbine arrangement as claimed in claim 1 , wherein the heat accumulation segment comprises a step; and
wherein the sealing element and the protective shield are arranged in or on the step of the heat accumulation segment.
6. The gas turbine arrangement as claimed in claim 5 , wherein the protective shield has an L-shape.
7. The gas turbine arrangement as claimed in claim 6 , wherein the protective shield is arranged horizontally on the step.
8. The gas turbine arrangement as claimed in claim 1 , wherein the sealing element, the protective shield, or both, comprise a nickel- or cobalt-based superalloy.
9. The gas turbine arrangement as claimed in claim 1 , further comprising:
a metallic coating which coats the sealing element, the protective shield, or both.