Abstract: A supercritical heat recovery steam generator includes a duct defining an interior area and having a gas inlet and a gas outlet. The duct is configured to convey gas from the gas inlet to the gas outlet. A portion of the duct between the gas inlet and the gas outlet defines an exhaust gas flow segment of the interior area. A supercritical evaporator is disposed in the interior area and a reheater is disposed in the interior area. The reheater and the supercritical evaporator are disposed in the exhaust gas flow segment, adjacent to each other with respect to the flow of the exhaust gas.

Abstract: Disclosed herein is a once-through evaporator comprising an inlet manifold; one or more inlet headers in fluid communication with the inlet manifold; one or more tube stacks, where each tube stack comprises one or more substantially horizontal evaporator tubes; the one or more tube stacks being in fluid communication with the one or more inlet headers; where one or more tube stacks are used for a start-up of the once-through evaporator; one or more outlet headers in fluid communication with one or more tube stacks; a separator in fluid communication with the one or more outlet headers; a first flow control device in fluid communication with the separator and at least one of the tube stacks used for startup; a second flow control device in fluid communication with a superheater to bypass the separator and at least one of the tube stacks used for startup; and a controller for controlling the actuation of the first and second flow control devices in response to a parameter of the evaporator.

Abstract: A method for filtration of harmful gas effluents from a nuclear power plant including the steps of providing a gas effluent from a nuclear power plant, the effluent including a mixture of gases; filtering the harmful, notably radioactive elements from the gas effluent by membrane separation through at least one membrane, the membrane separation being achieved by sifting, sorption and/or diffusion; storing the filtered harmful elements in storage reservoirs, and discharging the processed gas effluent to the atmosphere.

Abstract: A gas treatment system including a heat exchanger having a first side and a second side separated from one another. The first side defines a first inlet and a first outlet and the second side defines a second inlet and a second outlet. A direct contact cooler is in fluid communication with the first outlet, a direct contact heater is in fluid communication with the first inlet and/or a gas polisher is in fluid communication with the first inlet and the first outlet. The gas treatment system includes an ammonia polishing system in fluid communication with the second inlet and/or the second outlet.

Abstract: A membrane for a method for filtration of gas effluents from an industrial installation including a wall having an internal surface and an external surface, the wall having pores of variable dimensions in the radial direction and in the longitudinal direction of the wall.

Abstract: A method and gas turbine are provided for the reliable purging of an exhaust gas recirculation line of the gas turbine with exhaust gas recirculation without the use of additional blow-off fans. A blow-off flow of the compressor is used for the purging of the exhaust gas recirculation line. The gas turbine can include at least one purging line which connects a compressor blow-off point to the exhaust gas recirculation line.

Abstract: A CO2 removal system includes an absorber for removing CO2 from flue gas. The CO2 removal system includes a regenerator in communication with the absorber. The regenerator separates CO2 from the ionic solution and supplies regenerated ionic solution to the absorber. The CO2 removal system includes a carbon dioxide water wash system in communication with the regenerator. The carbon dioxide water wash system receives a mixture of carbon dioxide and ammonia from the regenerator and separates the ammonia from the CO2. The CO2 removal system includes an ammonia water wash system in communication with the absorber and the carbon dioxide water wash system. The ammonia water wash system removes ammonia from the flue gas. The CO2 removal system includes a membrane separator in communication with the ammonia water wash system, the regenerator and/or the carbon dioxide water wash system.

Abstract: A method for filtration of harmful gas effluents from an industrial installation including the steps of providing a gas effluent from an industrial installation, the gas effluent including a mixture of gases; filtering the harmful, elements from the gas effluent by membrane separation through a plurality of membranes, the membrane separation being achieved by sifting, sorption and/or diffusion, each membrane being adapted for filtering a specific harmful element; sorting the filtered harmful elements and storing them in separate storage reservoirs, and discharging the processed gas effluent to the atmosphere.

Abstract: A method for operating a gas turbine, which is optionally operated with a gaseous fuel (A) having a gaseous mass flow ({dot over (m)}gas)and/or with an oil fuel (B) having an oil mass flow ({dot over (m)}oil), wherein a change between an operating mode with gaseous fuel (A) and an operating mode with oil fuel (B) is undertaken during load operation of the gas turbine, and wherein a water addition of a water mass flow ({dot over (m)}H2O) is provided at least in the operating mode with oil fuel (B). The ratio (?norm) of the added water mass flow ({dot over (m)}H2O) to the fuel mass flow during the change between operating modes is determined according to ? norm = m . H 2 ? O · LHV norm m . gas · LHV gas + m . oil · LHV oil .

Abstract: A high-pressure compressor (12), in particular in a gas turbine (10), has a compressor rotor (17) which is surrounded by a stator (18, 19) thereby forming a main flow channel (25) and which is delimited at the compressor outlet by an end face (30) substantially extending in the radial direction, along which end face cooling air (21) is conveyed in the radial direction for the purpose of cooling. A prolonged service life is achieved in that the end face (30) is provided with a first system (23, 24) for improving the heat transfer between the cooling air (21) and the end face (30).

Abstract: An actuating device is provided for the rotation of a turbine shaft train and includes a principal turning gear electrically operated and an auxiliary turning gear hydraulically operated. Also provided is a turbine-generator set for the generation of electricity including the actuating device.

Abstract: A rotary regenerative heat exchanger has a structure in which a rotor accommodating a heat storage body such as a heat transfer element is rotated inside a housing, the heat storage body is heated by means of a high-temperature heating fluid such as exhaust gas and stores the heat, and low-temperature fluid to be heated such as combustion air is heated by the heat stored in the heat storage body; and a sector plate for dividing the flow passages for the abovementioned two kinds of fluids, namely the heating fluid and the fluid to be heated, flowing through the inside of the rotor is provided at the upper end face of the rotor with a slight gap therebetween, and a static seal is disposed on both sides of the gap between the sector plate and the external structure of the heat exchanger, a suction pipe being provided in the external structure in such a way as to suction dust material such as ash which accumulates or is agitated on the sector plate.

Abstract: In a method for operating a combined cycle power plant (10), which has a gas turbine installation (11) and a water-steam cycle (21) connected to the gas turbine installation (11) by a waste heat steam generator (24) and has at least one steam turbine (23), the gas turbine installation (11) includes a compressor (13), a combustion chamber (14), and a turbine (16). To cool the turbine (16), air compressed at the compressor (13) is removed, cooled in at least one cooler (18, 19) flowed through by water, thus generating steam, and introduced into the turbine (16). At least with the gas turbine installation (11) running, prior to or during the start-up of the water-steam cycle (21), waste heat, which is contained in the steam generated in the at least one cooler (18, 19), is used to good effect for pre-heating the installation inside the combined cycle power plant (10).

Abstract: A Rogowski coil assembly (1) for measurement of high frequency electrical currents includes coil segments (3) disposed in series with retrospective impedance influence reduction coupling.

Abstract: The bend of the invention makes it possible to provide a great number of different direction changes in the configuration of gas-insulated high-voltage lines. The bend mainly uses an angled ferrule (11). associated with two angular rings (12), placed between the angled ferrule (11) and a straight section (13) of the line, each angular ring (12) forming a change of direction defined by a determined angular offset angle (?) between said two joining surfaces. Thus, the use of an angled ferrule (11), in combination with one or two angular rings (12) makes it possible to obtain the four angular offsets of 70°, 80°, 100°, 110°. These same angular rings (12), used with an angled ferrule having an angle of 140° makes it possible to obtain the angles of 120°, 130°, 150°, and 160°. Use for constructing gas-insulated high-voltage lines.

Abstract: A slip ring includes a first element and a second element movable relative to each other, a chamber between the first and second elements, a metal or alloy in the chamber. The metal or alloy is liquid or becomes liquid under operating conditions. A passage is connected to the chamber between the first and second element. An outer chamber is connected to the passages. The outer chamber is filled with a sealing fluid for the chamber.

Abstract: A solar tower (1) has a solar radiation receiver (4) and a gas turbine engine (2). The gas turbine engine (2) is vertically arranged within the tower and includes, in downward flow series: a compressor (3) for compressing ambient air (15) drawn through at least one air inlet at an upper end of the tower, a heating arrangement (4) for heating compressed air from the compressor, the solar radiation receiver includes at least part of the heating arrangement, and a turbine (5) for extracting work from the heated compressed air. The gas turbine engine (2) is integrally formed with the solar tower (1) and the gas heating arrangement of the gas turbine engine (2) is integrally formed with the solar radiation receiver (4).

Abstract: A converter has converting groups with a first stage connected to input lines thereof and a second stage connected to output lines. The first and second stages have positive and negative branches that are connected together.

Abstract: A method is provided for reconditioning a turbomachine vane cover plate, by a forming apparatus. The vane having a mounting portion, an airfoil extending radially outward therefrom and a vane head connected to the airfoil. The vane also having a cover plate connected to the vane head, bulged in a direction opposite to the root. In a first analysis step, dimensions of the vane in relation to the cover plate are determined in respect of predefined reference points. If, thereafter, forming of the cover plate seems necessary and possible based on comparison of measurement values from the analysis step with predefined dimension values, the bulged cover plate is formed, at least essentially pressed smooth, by pressing by the forming apparatus in a forming step. After the forming step, the cover plate is re-treated in one or more follow-up steps. An apparatus is also provided for carrying out the method.

Abstract: An exhaust gas housing for a gas turbine, in which an annular gas passage, through which exhaust gas discharges from the gas turbine to the outside, is formed by a concentric inner casing and an outer casing which concentrically encompasses the inner casing at a distance, wherein the inner casing and the outer casing are interconnected by a plurality of radial struts which extend through the gas passage and have in each case a leading edge and a trailing edge with regard to the exhaust gas flowing through the gas passage, and wherein the struts, the outer casing and the inner casing are equipped in each case with a heat-resistant lining towards the gas passage, wherein the lining of the struts is at least partially mechanically decoupled from the lining of the inner casing and/or of the outer casing for reducing thermal stresses on the periphery of the struts.