| Document |
Document Title |
|
WO/2006/038944A1 |
An exemplary bore (248) for a shaft of a turbomachine includes a longitudinal axis extending generally from an inner end to an outer end of the bore, an. outer seat disposed proximate to the outer end of the bore at an outer seat radius ...
|
|
WO/2006/038903A1 |
A turbocharger (10) comprises a turbine mounted on a rotatable shaft (12) for rotation about an axis of the shaft and a compressor comprising a compressor wheel mounted on the shaft (12), the compressor wheel comprising a first-stage imp...
|
|
WO/2006/032827A1 |
An exemplary vane for a variable geometry turbine includes an upper surface that includes a pressure biasing region positionable to substantially coincide with an opening in an adjacent surface that provides high pressure exhaust gas dur...
|
|
WO/2006/033175A1 |
A gas turbine apparatus, a low calorie content gas feeding apparatus capable of feeding a low calorie content gas as a fuel for gas turbine stabilized by suppressing the sudden rise of its calorie content, and a method of suppressing the...
|
|
WO/2006/027610A1 |
An integrated power plant comprising a gas turbine set with a compressor, a combustion chamber and a gas turbine, a waste heat recovery unit (WHRU) arranged downstream of the gas turbine, the heat from the gas turbine flue gases being re...
|
|
WO/2006/024209A1 |
The engine of the invention, which is of a gas-steam type has three modes, i.e. a boiler engine, a turbine engine, and an internal-combustion engine. Combustion is controlled by means of an air-feeding system of the engine which is compo...
|
|
WO/2006/018187A1 |
An exhaust gas turbocharger for an internal combustion engine comprises an exhaust gas turbine (3) in the exhaust gas line (4) and comprises a compressor (5) in the induction tract (6). An inflow channel (13) is mounted up from the turbi...
|
|
WO/2006/019131A1 |
A volatile organic compound is treated to make it harmless and, in addition, the overall energy efficiency in a facility where the treatment of a volatile organic compound is necessary is heightened. A discharge gas containing a volatile...
|
|
WO/2006/018189A1 |
Disclosed is an exhaust turbocharger for an internal combustion engine comprising a compressor in the intake manifold and a turbine in the exhaust manifold thereof, the compressor being connected to the turbine via a torsion-proof shaft....
|
|
WO/2006/015613A1 |
The present application relates to a turbocharger having a compartment (113) which accommodates a vane actuating mechanism (135, 137, 139) for actuating a variable nozzle device. The compartment (113) is communicated by means of a ventil...
|
|
WO/2006/012406A2 |
An organic rankine cycle system is combined with a vapor compression cycle system with the turbine generator of the organic rankine cycle generating the power necessary to operate the motor of the refrigerant compressor. The vapor compre...
|
|
WO/2006/007888A1 |
Disclosed is a compressor in an exhaust gas turbocharger, comprising an attached rotor that is mounted upstream of the compressor wheel and can be displaced between a coupled position with the compressor wheel and a decoupled position. T...
|
|
WO/2006/007963A1 |
The invention relates to a compressor in an exhaust-gas turbocharger for an internal combustion engine. Said compressor comprises a compressor wheel (8) that is rotatably mounted in a compressor intake port (19). A rotor wheel attachment...
|
|
WO/2006/004141A1 |
A heat exchanger packed with a catalyst for reforming DME is installed in the discharge line of a combustion apparatus such as a furnace, an internal combustion engine or electric power generation facilities. A mixed gas from DME and H2O...
|
|
WO/2005/124107A2 |
The invention relates to a turbine wheel in a waste gas turbine, comprising a turbine wheel hub and a plurality of turbine wheel blades which are arranged on the turbine wheel hub and which extend in an axial manner between a turbine whe...
|
|
WO/2005/122389A1 |
The invention relates to a power station, comprising an input shaft run (1), on which a motor (12) and a compressor (11) are arranged and an output shaft run (2), on which a generator (22) and an expansion engine (21) are arranged. The c...
|
|
WO/2005/119029A1 |
A refrigeration cycle is integrated into a combined cycle power plant to form a triple cycle power plant in which gas turbine generator inlet air is chilled and dehydrated to increase the mass flow of the inlet air, and in which duct fir...
|
|
WO/2005/119030A1 |
The inventive turbine comprises a cooled turbine wheel. The hub (11) of the turbine wheel is cooled by means of a cooling channel (50) that is configured in the neighbouring turbine housing (22). The lower material temperatures thus achi...
|
|
WO/2005/119031A1 |
The absorber silencer of the compressor of an exhaust gas turbocharger is mounted in the area of the flow duct downstream from the compressor wheel. The absorption silencer can be mounted in front of or after the guiding device or as an ...
|
|
WO/2005/108757A2 |
A turbocharger (24) comprising a turbine (28), director (2), and compressor (34). The turbine (28) may be formed as a turbine wheel (68) surrounded by at least two scrolls (26). The at least two scrolls (26) may direct exhaust gases supp...
|
|
WO/2005/108863A1 |
A feedwater heater (14) for an HRSG (A) is provided with a monitoring unit (B) for detecting the presence of condensation in the feedwater heater. The monitoring unit includes a dielectric band (50) around one of the tubes (26) of the fe...
|
|
WO/2005/108758A1 |
The offered high-temperature GAES is designed as a stabilising element in high-power electric energy systems to ensure qualitative, economical and reliable functioning of these systems. It relates to energy accumulation equipment in whic...
|
|
WO/2005/106213A1 |
A variable geometry turbocharger assembly (90) employing the present invention includes a center housing (92), a compressor housing attached to one side of the center housing, and a turbine housing (94) attached to another side of the ce...
|
|
WO/2005/106224A1 |
A process for producing electrical power including the step of: a) combusting a stoichiometric amount of a reactant in air in the presence of atomized water to obtain a gaseous mixture having a terminal temperature less than a maximum op...
|
|
WO/2005/098218A1 |
A gearbox (30, 130) for rotating a propeller in a selected one of a first or second direction provided. The second direction being opposite with respect to the first direction. The gearbox includes common gas turbine gear components sele...
|
|
WO/2005/095772A1 |
A turbocharger (50) includes a foil bearing assembly (100) mounted in a center housing (90) between a compressor (60) and a turbine (70) of the turbocharger (50). The bearing assembly (100) forms a unit installable into the center housin...
|
|
WO/2005/089257A2 |
A combined heat and AC power generating system is disclosed having black start capability for the full time, simultaneous production of both electricity and heat. Heat generated within the system is captured and used for heating applicat...
|
|
WO/2005/090755A1 |
The invention relates to a gas turbine, comprising a turbine and a compressor (10) provided with a compressor housing (14), and to a method for the operation thereof. The compressor (10) is tapped in order to cool the turbine by means of...
|
|
WO/2005/088122A1 |
Because the efficiency of the thermal energy storage technology is inherently restricted, its beneficial use is limited to very particular economic boundary conditions, i.e. a large difference between the value of electricity going into ...
|
|
WO/2005/088103A1 |
The invention relates to a device (1) for heating an air flow (4, 5) supplied to a compressor (2) of a stationary gas turbine (3). Said device (1) comprises an exhaust gas recirculation line (5), the supply end (6) thereof being connecte...
|
|
WO/2005/088123A1 |
The invention relates to a device for the conversion of heat energy into another energy form (14, 6) provided with at least one heat input and pressure reservoir module, each comprising a heat input transmitting device (1) and a pressure...
|
|
WO/2005/083238A1 |
The invention relates to a power plant comprising a conventional steam turbo set, a high temperature turbo set and a carbon-fired boiler (1) which is fired by a fluidised bed. The high temperature turbo set is arranged, in particular, in...
|
|
WO/2005/083269A2 |
Compressor wheel (16) and techniques for manufacturing such a wheel are provided. The wheel may include a hub (21) with a counterbore (36) internally treated to impart residual compressive stresses. for enhanced endurance to stress-induc...
|
|
WO/2005/083247A1 |
Energy systems providing electrical and heat energy for a single residential house, commercial business or office building. The system is small enough to be stored inside the house or building. The system excess electrical energy may be ...
|
|
WO/2005/071243A1 |
The invention relates to a compressor (1) which is mounted in the intake tract of an internal combustion engine. Said compressor comprises a compressor wheel (2) that is rotatably received in an axial compressor inlet channel (5). Said c...
|
|
WO/2005/064135A2 |
An electric assisted turbocharger has an electric motor (12) with a stator (30) and a rotor (31) that is coupled to a turbocharger shaft (14) carried by a bearing assembly. The stator (30) has a left-hand winding (32) and a right hand-wi...
|
|
WO/2005/063564A2 |
The invention relates to an air guiding flap of an aircraft wherein one surface (28) thereof faces an air duct and is exposed to a prevailing pressure in the air duct and whose opposite surface (30) is exposed to the pressure of the rela...
|
|
WO/2005/064232A1 |
The invention relates to a thermal power plant with sequential combustion and reduced CO2 emissions, said plant having the following components that are connected in series by at least one flow channel (S): a combustion intake air compre...
|
|
WO/2005/063579A1 |
A ram air channel (10) for the supply of ambient air in an aircraft includes a first air inlet (12) and a main flow channel (16) which extends downstream of the first air inlet (12). In order to guarantee that the systems on board the ai...
|
|
WO/2005/056994A1 |
An air-storage plant (1) comprising a storage cavern (5), compressors (2a, 2b) for compressing air, and a turbine (8), which is connected to a generator (G1) via a shaft, is integrated with a steam turbine plant (10) by means of heat exc...
|
|
WO/2005/054645A1 |
The invention relates to a gas turbine, in particular an aircraft engine and to a method for generating electrical energy in a gas turbine. The gas turbine comprises at least one engine core (18), in which a shaft (19) produces a shaft o...
|
|
WO/2005/052341A1 |
Procedure for controlling the useful life of the gas turbines of a plant by means of a production plant (10) equipped with a series of production trains (15) and an auxiliary gas generator group (40). Each production train (15) is in tur...
|
|
WO/2005/045215A1 |
A system for generating accessory power from a gas turbine engine is provided by the present invention. The system includes an electronic control device for monitoring at least one parameter which provides information about an incipient ...
|
|
WO/2005/040581A1 |
A CAES unit comprises an atmospheric burner (11), arranged downstream of the expansion machine (2). The flue gas thus generated flows through a heat exchanger (9). The storage medium, flowing from the reservoir (1) into the heat exchange...
|
|
WO/2005/038972A2 |
A fuel cell (24) comprises a housing (70) with an inlet (72) for an oxygen-containing gas and an outlet (74) for depleted oxygen-containing gas, which are in communication with one another via a number of fuel cell tubes (80) arranged pa...
|
|
WO/2005/033022A1 |
An organic matter such as sewage sludge (101) is treated by gasifying the organic matter into a combustible gas and using the combustible gas as a fuel for a gas engine or a gas turbine to recover power (energy). In a method of treating ...
|
|
WO/2005/031120A1 |
A variable geometry turbocharger includes vanes (50) disposed therein having an inner airfoil surface (68) oriented adjacent a turbine wheel, and an outer airfoil surface (66) oriented opposite and parallel to the inner airfoil surface (...
|
|
WO/2005/028815A2 |
The invention relates to a device for the generation of mechanical or electrical energy using any thermal potential, by means of a flow system that admits a flowing, compressible medium. A diffuser and a heat-exchanger device that is int...
|
|
WO/2005/027302A1 |
Power generating units and compressor units are arranged in an air cell power plant (1,2,3). According to one aspect of the invention, a common network connection transformer (23) with power generating units and compressor units alternat...
|
|
WO/2005/024206A1 |
The invention relates to a power plant comprising a gas turbine group (1) with a heat transfer device (202), e.g. a recuperation device for pre-heating the combustion air, said device being located downstream of the turbine (103) in the ...
|
