| 专利名称： | A CERAMIC BLADE GAS TURBINE |
| 公开（告）号： | |
| 公开（公告）日： | 2007-04-12 00:00:00 |
| 申请（专利）号： | WO2006US37967(WO2007041261) |
| 申请日： | 2006-09-27 00:00:00 |
| 发明（设计）人： | DICIC ZORAN (US) |
| (申请)专利权（人）： | DICIC ZORAN (US) |
| 内容： | A rotor assembly A for use in a turbine (10) that has a rotor (12) supported in a turbine compressor casing (32) of the turbine (10) for rotational movement of the rotor (12) about a rotor axis. The rotor assembly A comprises a first gas flow assembly (16) positioned within the turbine compressor casing (32) and around the rotor (12). The first gas flow assembly (16) has a plurality of nozzles (102) that are removeably attached to an inner circumference (114) of the rotor (12), each nozzle (102) having a nozzle inlet (116), a nozzle outlet (118) and a nozzle blade disposed there between. The rotor assembly A further comprises a heat assembly (14) partially positioned within the turbine compressor casing (32) of the rotor (12). The heat assembly (14) directs heated gas into the nozzle inlet (116) wherein the nozzle outlets (118) discharge the heated gas tangentially with respect to the rotor (12) such that the discharged heated gas produces a reactive force on the plurality of nozzles (102) to rotate the rotor (12) about the rotor axis. The rotor assembly A also comprises a second gas flow assembly (18) positioned on the inner circumference (114) of the rotor (12) and positioned adjacent to the first gas flow assembly (16). The second gas flow assembly (18) has a plurality of stationary blades (128) fixedly supported on the heat assembly (14) and having a plurality of rotary blades (130) removeably attached to the inner circumference (114) of the rotor (12). |
发布日期：2007-08-27 15:44:00