Abstract: An electrical turbo-machine includes a stator (101), a rotor (102), and a turbine section (110) driven with a working flow containing vaporizable material, for example water, in vaporized form. The rotor includes cooling channels (106-109) for conducting, through the rotor, a cooling flow containing the vaporizable material in liquid form. The rotor is arranged to conduct the cooling flow through an area where an impeller or impellers (111-114) of the turbine section are directly connected to the rotor and conduct the cooling flow to a same room to which the working flow comes out from the turbine section. The above-presented cooling system facilitates constructing the electrical turbo-machine as a hermetic structure in a power plant where bearings of the electrical turbo-machine are lubricated by the vaporizable material, a supply pump is directly connected to the rotor, and the vaporizable material in gaseous form fills the gas spaces of the stator.

Abstract: A gas turbine arrangement, including a gas generator section (A), a power turbine section (B), and a generator section (C) coupled on a common shaft (10). The power turbine has its bearing block (12) provided with a copper cooling cup (9), which possesses a high thermal conductivity and conveys heat flux away from the side and block of the bearing and which has a design that enables the effect of a penetrating airflow.

Abstract: An electrical turbo-machine includes a stator (101), a rotor (102), and a turbine section (110) driven with a working flow containing vaporizable material, for example water, in vaporized form. The rotor includes cooling channels (106-109) for conducting, through the rotor, a cooling flow containing the vaporizable material in liquid form. The rotor is arranged to conduct the cooling flow through an area where an impeller or impellers (111-114) of the turbine section are directly connected to the rotor and conduct the cooling flow to a same room to which the working flow comes out from the turbine section. The above-presented cooling system facilitates constructing the electrical turbo-machine as a hermetic structure in a power plant where bearings of the electrical turbo-machine are lubricated by the vaporizable material, a supply pump is directly connected to the rotor, and the vaporizable material in gaseous form fills the gas spaces of the stator.

Abstract: A gas turbine arrangement, including a gas generator section (A), a power turbine section (B), and a generator section (C) coupled on a common shaft (10). The power turbine has its bearing block (12) provided with a copper cooling cup (9), which possesses a high thermal conductivity and conveys heat flux away from the side and block of the bearing and which has a design that enables the effect of a penetrating airflow.

Abstract: The invention relates to a lead-in structure for coupling of a turbo generator in a circulating process of a circulating medium. The turbo generator includes a turbine and a generator as well as possibly also a feed pump enclosed in a common casing structure. The casing structure also includes at least a first duct for hot, steam-like circulating medium entering the turbine, a second duct for circulating medium exiting the turbine, and a third duct for cooled liquid circulating medium, which, for example, enters the feed pump. The third duct includes an annular channel that is placed, preferably concentrically, around the second duct, which includes an annular channel. The first duct includes an annular channel that is placed, preferably concentrically, between the second duct and the annular channel of the third duct.

Abstract: The invention relates to a lead-in structure for coupling of a turbo generator in a circulating process of a circulating medium. The turbo generator includes a turbine and a generator as well as possibly also a feed pump enclosed in a common casing structure. The casing structure also includes at least a first duct for hot, steam-like circulating medium entering the turbine, a second duct for circulating medium exiting the turbine, and a third duct for cooled liquid circulating medium, which, for example, enters the feed pump. The third duct includes an annular channel that is placed, preferably concentrically, around the second duct, which includes an annular channel. The first duct includes an annular channel that is placed, preferably concentrically, between the second duct and the annular channel of the third duct.

Abstract: The invention relates to a method for generating over-pressure gas by means of a kinetic compressor which is coupled to a high-speed electric machine located on the same shaft with the compressor and comprising a rotor whose rotational speed is over 20,000 rpm. The compressor is provided with at least two stages. The shaft of the rotor is mounted on a magnetic and/or gas bearings, and the high-speed electric machine is placed centrally on the shaft with respect to the compressor stage of the compressor. The rotor is mounted on a magnetic bearing at least in the axial direction, and the ends of the rotor are used at least partly as counter surfaces for the axial magnetic bearing.

Abstract: A method is provided for improving the efficiency of a small-size power plant based on an ORC process. The plant comprises at least one energy converter unit, with a power range below 500 kW, and at least one burner for combustion of fuel for producing energy for the energy converter unit. The energy converter unit includes a high-speed machine which comprises first and second turbines and a generator mounted on a common rotor having rotational speed exceeding 8000 rpm. An ORC medium is vaporized in a vaporizer by utilizing energy derived from the combustion of the fuel in the burner, and then expanded in the first turbine of the high-speed machine to produce electric energy. The ORC medium leaving the first turbine is then reheated by a superheater of the vaporizer utilizing energy derived from the combustion of the fuel in the burner.

Abstract: The present invention is directed to a method for operating a hermetic, small-size power plant in which a primary circulation is conducted in a main line connecting a high-speed machine including at least a turbine and a generator installed on a joint rotor, a vaporizer and a condenser. Fluid lubrication of bearings of the rotor during the continuing operation is effected by fluid medium passing through the condenser and along the main line of the primary circulation. The vaporizer is connected to the high-speed machine through medium flow paths defining a circulating medium circuit bypassing the condenser and at least partly bypassing the main line of the primary circulation to secure passage of circulating medium accumulated in the vaporizer for lubrication of the bearings of the rotor during stopping of the primary circulation.

Abstract: The invention concerns an energy converter, comprising a boiler, a turbine (11), a condenser, a feed pump (16) and a generator (17) and, if required, a recuperator and a pre-feeding pump. The thermal energy to be supplied to the boiler has been arranged to maintain a Rankine process driving the generator (17) and thus to produce electricity. The turbine (11), the generator (17) and the feed pump (16) have a joint rotor shaft (36). The rotor (36) is rotatably carried with gas-dynamic bearings (24) utilizing the circulating fluid's vapor. The lower surface of the rotor (21) of the turbine (11) has been disposed to serve as one abutment surface of a gas-static thrust bearing (22). The gas-dynamic bearings (24) are bearings of tilting pad type.