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WO/2017/036431A1 |
The equipment for increase of output and improvement of efficiency of a gas turbine includes a primary compressor (101) with an impeller for input medium compressing, a combustion chamber (102) for heating the compressed input media and ...
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WO/2017/040022A1 |
The present invention relates to a turbocharger comprising a bearing housing, a turbine housing which is connected to the bearing housing, and a cartridge. The cartridge comprises a blade bearing ring and a disk, wherein a plurality of b...
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WO/2017/039640A1 |
Systems, methods and apparatus for connection of a multi-stage turbocharger to a heat exchanger are disclosed. The multi-stage turbocharger includes at least first and second compressors with respective first and second outlets. A plumbi...
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WO/2017/040635A1 |
The present disclosure relates to systems and methods useful for power production. In particular, a power production cycle utilizing CO2 as a working fluid may be combined with a second cycle wherein a compressed CO2 stream from the powe...
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WO/2017/029007A1 |
The invention relates to a method for coupling a first sub-shaft, which has a first turbomachine and a generator connected to a mains supply, to a second sub-shaft, which has a second turbomachine, by means of an overrunning clutch, with...
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WO/2017/029437A1 |
The present invention is a system, method and computer program for operating a land- or marine-based multi-spool gas turbine system for generating electrical power to supply a load, wherein the system comprises a multi-spool gas turbine ...
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WO/2017/025746A1 |
A hybrid combustion turbine power generation system (330) comprises a gas turbine (11/12/14) integrated with an ACAES via fluid connection(s) (32) between the compressor (11) and turbine (14), to allow air to be extracted from, and injec...
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WO/2017/018154A1 |
A water feeding system (50) is provided with: a first water feeding line (51) through which first feed water flows; a second water feeding line (52) through which second feed water having a lower pressure than the first feed water flows;...
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WO/2017/015343A1 |
A system and related method for providing a highly reactive fuel to a combustor of a gas turbine are disclosed herein. The system includes a fuel supply system that is in fluid communication with a fuel supply. The fuel supply system inc...
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WO/2017/013362A1 |
The invention relates to an aircraft propulsion assembly, including a turbine engine comprising at least one gas generator (2a, 2b) configured to generate a main flow, which is supplied by a central jet (4) to at least one power turbine ...
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WO/2017/005470A1 |
The invention relates to an exhaust-gas turbocharger (1) for an internal combustion engine (2) having an intake duct (3) for air and having an exhaust duct (5) and having a turbine (6) arranged in the exhaust duct and having a compressor...
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WO/2017/001029A1 |
The invention relates to an engine structure (200) forming an adapter for connecting a turbocharger unit (100) to a cylinder block (22) of an internal combustion engine (10). The engine structure (200) comprises a set of attachment means...
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WO/2016/203980A1 |
This compressed air energy storage power generation device 2 is provided with: motors 26a, 26b which are driven by fluctuating input power; a compressor 4 which is mechanically connected to the motors 26a, 26b, and which compresses air; ...
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WO/2016/203979A1 |
This compressed air energy storage power generation device 2 is provided with: an expansion-side heat medium temperature sensor 40 for measuring the temperature of a heat medium supplied to an expansion-side heat exchanger 16; an expansi...
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WO/2016/202711A1 |
In order for charge air (L) to be conducted with the lowest possible losses in pressure in a turbocharger (2) that comprises a blow-off valve (20), a flow-guiding element (28) in an inlet region (14) is designed such that neutral zones a...
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WO/2016/195968A1 |
Apparatus, systems, and methods store energy by liquefying a gas such as air, for example, and then recover the energy by regasifying the liquid and combusting or otherwise reacting the gas with a fuel to drive a heat engine. The process...
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WO/2016/193724A1 |
A micro-CHP gas boiler comprises a heat exchanger having a combustion space surrounded by a water flowpath, and a gas turbine assembly which is installed in the combustion space. The gas turbine assembly includes a generator surrounded b...
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WO/2016/195999A1 |
Apparatus, systems, and methods store energy by liquefying a gas such as air, for example, and then recover the energy by regasifying the cryogenic liquid and combusting or otherwise reacting the gas with a fuel to drive a heat engine. C...
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WO/2016/189188A1 |
A power plant (10) comprising a first turbine-compressor unit (12) provided with a first compressor part (14) and a first turbine part (20); a gas heater unit (24) arranged in fluid connection with the first compressor part (14) and the ...
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WO/2016/189189A1 |
A power plant (10) comprising a first turbine-compressor unit (12) provided with a first compressor part (14) and a first turbine part (20); a gas heater unit (24) arranged in fluid connection with the first compressor part (14) and the ...
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WO/2016/185782A1 |
This thermoacoustic power generation system is equipped with: a turbine 140 including a turbine blade 145 that rotates by self-excited vibration of an operating gas in a thermoacoustic engine, and is provided inside a branch pipe 103 of ...
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WO/2016/184416A1 |
An ultra-high speed turbocharger, comprising a turbine machine (1), a compressor (2), a rotary shaft (3), two radial bearings (4), a thrust bearing (5) and a main housing (6), the radial bearings (4) being groove-type dynamic pressure ga...
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WO/2016/185783A1 |
This thermoacoustic power generation system 100 is equipped with: a thermoacoustic engine 110 provided in a ring-shaped pipe 102; a turbine 140 that is provided in a branch pipe 103, and rotates upon receiving acoustic energy E produced ...
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WO/2016/184417A1 |
A miniature turbocharger, comprising a turbine machine (1), a compressor (2), a rotary shaft (3), two radial bearings (4), a thrust bearing (5) and a main housing (6), the radial bearings (4) being mixed-type dynamic pressure gas radial ...
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WO/2016/186512A1 |
A system and a method for recovering waste heat from an industrial process in pre heating combustion air and fuel is provided. The present invention attains the above-described objective by a plurality of heat exchangers extracting heat ...
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WO/2016/185906A1 |
According to the compressed-air-storing power generation method: a storage value indicating that an amount of air stored in an accumulator tank 12 in a compressed-air-storing power generation device 2 has reached a prescribed intermediat...
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WO/2016/181841A1 |
A compressed air energy storage and power generation device 2 comprising a compressor 10, a pressure accumulation tank 12, and an expander 14. The compressor 10 is driven by a motor 30 using renewable energy and compresses air. The press...
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WO/2016/181884A1 |
A compressed air energy storage and power generation device 2 comprises a compressor 8, a pressure accumulation tank 12, and an expander 14. The compressor 8 is two-stage, is driven by a motor 44 using renewable energy, and compresses ai...
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WO/2016/181883A1 |
A compressed air energy storage and power generation device 2 comprises a motor 46, a compressor 8, a pressure accumulation tank 10, an expander 12, and a generator 44. The motor 46 is driven by a fluctuating input power. The compressor ...
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WO/2016/181798A1 |
Provided is a compressed air storage power generation device 2 comprising a compressor 6, a pressure accumulation tank 8, and an expander 10. The compressor 6 is driven by renewable energy to compress air. The pressure accumulation tank ...
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WO/2016/181069A1 |
The invention relates to a butterfly valve (24) for bleeding a compressor for an aircraft turbine engine, the valve including a valve body (32), a butterfly (36), and a device (42) for controlling the angular position of the butterfly, t...
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WO/2016/177705A1 |
The invention involves a conduit connection assembly comprising a first conduit part (201) and a second conduit part (401), adapted to be assembled to form a conduit connection delimiting a first fluid conducting volume (VI), characteriz...
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WO/2016/178358A1 |
A compressed-air storage power generation method according to the present invention is provided with: a first air-compression step; a first air-storage step; a first air-supply step; a first power-generation step; a first heat-exchange s...
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WO/2016/177430A1 |
The invention involves a conduit connection assembly, characterised in that the assembly comprises a first conduit part (201) and a second conduit part (401), adapted to be assembled to form a conduit connection delimiting a fluid conduc...
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WO/2016/176605A1 |
Turbomachines having one or more flow guiding features designed to increase the performance of the turbomachine (3400, 3700, 4000, 4800). In some examples, flow guiding features are designed and configured to bias a circumferential press...
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WO/2016/169636A1 |
The invention relates to an exhaust turbocharger for an internal combustion engine, in particular of a motor vehicle, comprising a supporting housing (16), which has at least one passage opening (18) for a rotor (10) of the exhaust turbo...
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WO/2016/166774A1 |
The present disclosure relates to a novel gas turbine having applications, for example, in thermal power generation in an environmentally friendly manner. In various embodiments, the present disclosure provides a multiloop gas turbine wi...
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WO/2016/166024A1 |
The invention relates to a method for operating a power plant (1) and to a power plant (1) which can be operated at locations with an insufficient fuel supply. For this purpose, the power plant (1) comprises a gas turbine (2), a gas liqu...
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WO/2016/166095A1 |
The invention relates to a system and a method for compressed gas energy storage and recovery, such as AA-CAES. The system and the method according to the invention implement the constant volume heating Q of the stored compressed gas, wh...
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WO/2016/165724A1 |
The present invention relates to a method for energy storage by way of the conversion into thermal energy and subsequent power generation by means of – a gas turbine set with a compressor (1), an expander (6) and a power generator (8),...
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WO/2016/162105A1 |
The invention relates to a controller for an exhaust gas conductive portion, through which a flow can pass, of a turbocharger. The controller (13) is designed to open and close a bypass channel (11) in the exhaust gas conductive portion ...
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WO/2016/162106A1 |
The invention relates to a regulating device for an exhaust-gas-conducting section of an exhaust-gas turbocharger, wherein the regulating device (19) is designed for guiding a flow of a fluid into a bypass duct (22), which is formed in t...
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WO/2016/156310A1 |
The invention relates to a wastegate valve system for an exhaust-gas turbocharger comprising a housing (30), which forms a valve seat, a valve body (28), and an actuating device, by means of which the valve body (28) can be pressed onto ...
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WO/2016/156739A1 |
The invention relates to a hub (2) of an intermediate casing (1) for a dual-flow turbine engine, said hub (2) comprising: a discharge flow duct (18) extending between an inner shroud (3) and an outer shroud (5) of the hub (2), the discha...
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WO/2016/151199A1 |
The invention concerns land-based gas turbine plants with a two-spool gas turbine arrangement for generating electrical power. The invention comprises two spools. The first spool (10) comprises a first shaft (11), a first compressor (C1)...
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WO/2016/153963A1 |
An engine turbocharger (10) includes a radially oriented oil deflector (50) that incorporates an oil guiding feature (70) to improve control of a continuous turbulent mass of oil being impelled against the deflector by an oil flinger (35...
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WO/2016/154354A1 |
Embodiments of the inventive concept include a manufactured pressure vessel including pressure cells having an impermeable layer containing porous material in which air can permeate, and a big mass layer disposed atop the pressure vessel...
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WO/2016/149727A1 |
Disclosed is a multi-stage turbocharger (2) for an internal combustion engine, said turbocharger comprising an exhaust gas turbine (16) having at least one turbine impeller, and a compressor (1a) having a first compressor stage (3) and a...
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WO/2016/151198A1 |
The invention concerns land-based gas turbine plants with a multi-spool gas turbine arrangement for generating electrical power to supply a load (200). The invention comprises at least three spools (10a-10c). Each of the at least three s...
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WO/2016/148008A1 |
An intake air cooling device (150) is provided with a water supply line (131) and a heat pump device (151). The water supply line (131) sends water to a waste heat recovery boiler (110) which generates vapor utilizing the heat of exhaust...
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