| 摘要 |
The invention relates to a housing-side structure of a turbomachine, in particular of a gas turbine, comprising an in particular segmented jacket ring (16), which carries an abradable coating for radially outer ends of rotor-side rotor blades of a rotor blade ring, wherein the jacket ring (16) carrying the abradable coating is connected by means of at least one narrow part (18) to a stator-side housing part (19), which is radially outwardly adjacent to the jacket ring (16), and the jacket ring is thermally decoupled from said stator-side housing part. |
