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WO/2008/059371A2 |
In a bearing structure of a turbochargcr, a lubrication oil ejected from a lubrication oil supply opening (112) forms fluid layers between a support hole (111) of a center housing (10) and a floating metal member (120) and between a inse...
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WO/2008/055930A1 |
The invention relates to a turbocharger (1) with a turbine part (3) and a flow channel (12), in which several pivotable guide blades (30) are arranged in order to influence the flow. The guide blades (30) are pivotably mounted on a guide...
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WO/2008/055717A1 |
In order to be able to safely absorb the energy in the event of a punctured compressor wheel of an exhaust gas turbocharger, it is advantageous if the screws are as long as possible and embodied as anti-fatigue screws, thereby being able...
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WO/2008/050463A1 |
This invention provides a volatile organic compound-containing waste gas treatment system for treating a volatile organic compound-containing gas using a gas turbine. In order to prevent damage to components of an electric generator due ...
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WO/2008/049444A1 |
A gas flow control arrangement for a fuel cell arrangement having an inlet passage (2 ) and an exhaust passage (13), the arrangement including in the inlet passage ( 2) in the direction of flow, successively, first compressor means (6), ...
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WO/2008/047489A1 |
This invention provides a power supply equipment for a natural gas liquefaction plant, comprising a carburetor (3) for heating LNG with a first cooling water, a condenser (4) for heating the LNG from the carburetor (3) by air, a compress...
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WO/2008/043539A1 |
A compressor, particularly a radial compressor, for a turbocharger comprises a compressor impeller (1), which is rotatably received in a compressor housing, wherein cooling fluid flows through a part (6) of the compressor housing adjacen...
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WO/2008/041478A1 |
A method and device for starting and stopping a gas turbine, which enable stable ignition of fuel gas by eliminating inconvenience that the fuel gas does not ignite normally due to purge gas (nitrogen gas) remaining in fuel gas piping. T...
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WO/2008/038497A1 |
A gas turbine in which fuel is supplied by a combustor (12) to compressed air, compressed by a compressor (11), and combusted and rotational power is obtained by supplying the produced combustion gas to a turbine (13). The gas turbine ha...
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WO/2008/039216A2 |
The present disclosure includes a turbocharger (18). The turbocharger may include a titanium-aluminide turbine (26) and a shaft (30). A single joint (34) connects the turbine to the shaft. The joint may include an alloy comprising at lea...
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WO/2008/034861A1 |
Electrical energy and hot gas that can be used for the production of plaster products are generated by means of a heat and power generating system (2) in an installation (1) for producing plaster products. Energy supplied in the form of ...
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WO/2008/036862A2 |
A variable-nozzle turbocharger includes a cartridge (50) containing a variable vane mechanism connected between the center housing (20) and the turbine housing (24). The cartridge (50) comprises an annular nozzle ring (38) supporting an ...
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WO/2008/028666A1 |
The invention relates to a method for operating an internal combustion engine in the form of a spark-ignition engine (2) having the following method steps: pre-compressing the air supplied to the combustion chambers (15A-15D) of the inte...
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WO/2008/029211A1 |
An lubricating oil from an oil pump (354) that is driven by rotation of an engine (100) is supplied as a refrigerant to a rotor (214) of an assist motor (216) via a pressure valve (240A). The pressure valve (240A) is configured to be clo...
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WO/2008/025749A1 |
The guide apparatus of a turbine has guide vanes (31) which are mounted rotatably in the turbine housing (22, 23). A sealing sleeve (80) is arranged between the turbine housing (22) and the guide-vane stem (32). The additional axial comp...
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WO/2008/025754A1 |
The invention relates to a waste gate actuator (14) for an exhaust gas turbocharger (1), comprising an actuator housing and an actuator cover (19), an element for actuating the waste gate valve and electronic components for controlling t...
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WO/2008/023986A1 |
The invention relates to a method for increasing the energy and cost effectiveness of a gas power plant or thermal power plant, and for energy and cost effective CO2 capturing from flue gas with CO2 enriched content. The plant comprises ...
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WO/2008/019555A1 |
A coal powder-turbine generator includes a gas-steam combined cycle system and a coal powder two-phases combustion system. A combustor (11) of the gas-steam combined cycle system connects with the coal powder two-phases combustion system...
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WO/2008/015291A1 |
In a turbocharger multiple hollow spaces (31) occur resulting from its construction. If such hollow spaces are filled with particles, inexpensive particle vibration damper can be realized. Further, there are advantages with regard to fur...
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WO/2008/014481A1 |
A system and method for integrating gasification processes with membrane oxygen separation, advanced steam conditions, and effective heat recovery. Through the integration of synergistic technologies, a highly efficient Integrated Gasifi...
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WO/2008/009936A1 |
A turbine housing (13) for a radial flow turbine, particularly a turbine used in an exhaust gas turbocharger. The housing has a general volute shape with a substantially annular part extending around the turbine axis and an inlet duct (2...
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WO/2008/006797A1 |
A turbo-machine, having a rotor and a stator, is provided at least partially with a catalytic coating on a fluid flow-carrying part. The catalytic coating (7, 7') comprises at least one oxide of a transition metal, or an oxide of a mixtu...
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WO/2008/003651A1 |
Turbine of an exhaust gas turbocharger comprising a turbine disk (11) with rotor blades (12), a nozzle ring (31) with rotor blades, and a secondary ventilation system for the cooling of turbine components (31, 32, 33) which are exposed t...
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WO/2007/141101A1 |
In a method of operating a gas turbine (GT) with sequential combustion, which comprises at least one compressor (12, 13), a first combustion chamber (14) with a downstream first turbine (15), and a second combustion chamber (16) with a d...
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WO/2007/140835A1 |
Turbocompressor for an internal combustion engine, in particular a compressor for a turbocharger, having an air-collecting passage (1) for combustion air to be compressed, adjoining which are a main inlet passage (2), at least one auxili...
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WO/2007/137924A1 |
A guide device for a diffuser at the compressor wheel outlet of a radial compressor has guide blades (10, 20) with stepped inlet edges (11, 21). The step is realized by recessing the hub-side inlet edge (21). Said meridional stepping div...
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WO/2007/138325A2 |
A turbocharger wastegate valve assembly comprises a first bypass port (30) communicating with a first portion of an exhaust inlet and a first valve member (36) adapted for engaging and sealing a first valve seat surrounding the first byp...
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WO/2007/136731A2 |
A wind turbine system (16) for producing compressed air from wind energy. The wind turbine harvests energy from wind to produce mechanical energy. A compressor (22) receives mechanical energy from the wind turbine to compress air to an e...
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WO/2007/118663A1 |
The invention relates to a turbocharger (1) with variable turbine geometry (VTG) having a turbine housing (2) with an inlet duct (9) for exhaust gases; having a turbine rotor (4) which is rotatably mounted in the turbine housing (2); and...
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WO/2007/115446A1 |
A cascade radial-flow compressor for an aeronautic turbo-jet engine is disclosed. The compressor includes an air inlet (1) provided at the central of an axis, a casing, a movable impeller disc (5), a stationary impeller disc (2); a plura...
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WO/2007/117280A2 |
A turbocharger includes a compressor wheel having back-to-back impellers (i.e., a forward-facing impeller and a rearward-facing impeller) mounted on the same shaft. The two impellers are independently supplied with inlet air via separate...
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WO/2007/111759A2 |
The present invention is a turbocharger unit (10) incorporating variable turbine geometry. The unit (10) has a turbine for receiving exhaust gases from an engine having a turbine wheel (14) located inside a turbine housing (12), and an i...
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WO/2007/107289A1 |
Turbocharger (1) having a cartridge (K) arranged in a turbine casing (2) for the variable turbine geometry; having a bearing housing (3) which is arranged between the turbine casing (2) and a compressor casing of a compressor wheel and i...
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WO/2007/104535A1 |
The invention relates to a turbocharger (1) having a cartridge (K), which is arranged in a turbine housing (2), for the variable turbine geometry, having a bearing housing (3) which is arranged between the turbine housing (2) and a compr...
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WO/2007/101815A1 |
A method of operating a combined heat and power process of building heating having a heating circuit and a gas turbine building heating system (1) with which in particular said method can be carried out. In particular, it is important th...
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WO/2007/102641A1 |
A synergic hybrid jet turbine power generation system for increasing thermal efficiency by utilizing multistage axial-flow turbines is disclosed. In the power generation system, to utilize working fluid, generated by a pressure generatio...
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WO/2007/103777A2 |
A turbocharger (201), having an axial compressor wheel (203) and an axial turbine wheel (207) mounted on a first shaft (205) supported by a housing, and a radial compressor wheel (211) and a radial turbine wheel (215) mounted on a second...
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WO/2007/096377A1 |
In a method for the predictive control and/or regulation of a building energy system having at least one combined heat and power unit (1), control signals for a control and regulation unit (2) which is associated with the combined heat a...
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WO/2007/096656A1 |
The present invention concerns systems for storing energy and using the stored energy to generate electrical energy or drive a propeller (505). In particular, the present invention provides a method of storing energy comprising: providin...
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WO/2007/093407A1 |
The invention relates to a turbocharger (1) with a variable turbine geometry (VTG), comprising a turbine housing (2) that has a supply channel (9) for exhaust gases, a turbine rotor (4), which is rotatably mounted in the turbine housing ...
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WO/2007/094914A1 |
A system and method for increasing the efficiency and/or power produced by an integrated gasification combined cycle system by increasing the integration between the air separation unit island, the heat recovery steam generator and the r...
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WO/2007/093406A1 |
The invention relates to a turbocharger with a variable turbine geometry. Said turbocharger comprises a blade bearing ring assembly (1) with a blade bearing ring (2) and a disc (3), which can be fixed to the blade bearing ring (2) to cre...
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WO/2007/085045A1 |
An energy transfer system (101) includes a vessel (1) containing a thermally conductive liquid (2). First, second and third conduits (3, 7, 11) having respective first, second and third thermally conductive sections (6, 10, 14) are immer...
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WO/2007/082398A1 |
The invention relates to guide vanes which are arranged in a two or multi-part housing (32, 33). The housing separation takes place in a radial manner in the region of the bearing point (25) of the vane shaft, such that the separation jo...
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WO/2007/073008A2 |
A heat medium supply device (4) where, even if a heat medium has a successive temperature variation, a heat exchanger is prevented from being adversely thermally affected by the variation. The heat medium supply device (4) has a heating ...
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WO/2007/066569A1 |
A combustor (10) has steam cooling piping (11), and steam is caused to flow in steam supply piping (20), the steam cooling piping (11), steam discharge piping (70), in that order, to cool the combustor (10) by the steam. When a gas turbi...
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WO/2007/066117A1 |
A power generating system (10) includes a drive arrangement (12) and a compressor (18) arranged to be driven by the drive arrangement (12) to compress gas, in particular air. The system (10) also includes an underwater storage arrangemen...
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WO/2007/064631A1 |
A turbocharger (10) with a two-stage compressor having first- (24) and second-stage (26) impellers mounted on a common shaft (12) in a back-to-back configuration. The first-stage impeller (24) has a boreless configuration, defining an un...
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WO/2007/063645A1 |
This invention provides a high-efficiency heat cycle apparatus comprising a compressor, a first turbine, a first heat exchanger (7), a second heat exchanger (8), a first pump, and an expander, and a combined heat cycle power generation a...
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WO/2007/056780A1 |
The invention relates to an exhaust gas turbocharger (1) for an internal combustion engine, comprising an exhaust gas turbine, a charge air compressor (10), and at least one charge air duct (2) which adjoins a cooling device (7) for the ...
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