The turbine has a turbine shaft (12), and an internal housing (16) that surrounds the turbine shaft. The turbine shaft has a thrust compensation piston (30) for partial compensation of a blade thrust exerted on the turbine shaft. A guiding channel (34) for guiding a cooling medium (42) runs in a region within the internal housing in a longitudinal direction of the turbine shaft. The turbine shaft has a ventilator structure (32) in a region of the piston for driving the cooling medium, where the ventilator structure is drivable by rotation of the turbine shaft. An independent claim is also included for a turbine shaft for a turbine of a thermal power plant, comprising a thrust compensation piston.
申请公布号
EP1806476(A1)
申请公布日期
2007.07.11
申请号
EP20060000182
申请日期
2006.01.05
申请人
SIEMENS AKTIENGESELLSCHAFT
发明人
KACHEL, CARMEN-ELISABETH, DR.;KOSTENKO, YEVGEN, DR.;WECHSUNG, MICHAEL;WIEGHARDT, KAI, DR.