| 摘要 |
A gas turbine with several shroud segments ( 1 ) which enclose rotor blades ( 3 ) of a turbine wheel ( 5 ) as a seal, with the shroud segments ( 1 ) having at least a front and a rear attachment at the radially outward area of stator vane segments ( 7, 12 ), and with each of the stator vane segments ( 7, 12 ) being located at their radially inner area on a control ring ( 9, 10 ), wherein the stator vane segments ( 7, 12 ) are located on the control ring ( 9, 10 ) in a radially adjustable manner.
|
