| 摘要 |
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 ). |
