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WO/2018/037441A1 |
A mixed flow turbine wheel equipped with multiple rotor blades provided on the peripheral surface of a hub, said multiple rotor blades being configured such that when viewed in a meridian plane the front edge of each rotor blade includes...
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WO/2018/038875A1 |
A method and aircraft for providing bleed air to environmental control systems of an aircraft using a gas turbine engine, including determining a bleed air demand for the environmental control systems, selectively supplying low pressure ...
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WO/2018/035021A1 |
A turbocharger (20) includes a turbine housing (22) defining a turbine housing interior (24), a turbine wheel (26) disposed within the turbine housing interior (24), a shaft (28) coupled to and rotatable by the turbine wheel (26), a comp...
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WO/2018/026507A1 |
A heat exchanger assembly for a gas turbine engine that includes an outer engine case. The heat exchanger assembly includes at least one cooling channel, the at least one cooling channel is configured to receive a flow of fluid to be coo...
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WO/2018/020399A1 |
A process for cracking a hydrocarbon stream by: combusting fuel in a gas turbine in the presence of compressed air to produce a flue gas, wherein the flue gas drives a turbine to produce electricity in a coupled generator or work to powe...
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WO/2018/019401A1 |
The invention relates to an impeller (10) for a rotor of a turbocharger, comprising blades (12) and a wheel back (16) which adjoins the blades (12) in the axial direction of the impeller (10). The wheel back (16) has a first sub-region (...
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WO/2018/017459A1 |
The present disclosure generally relates to separating solid particles from an airflow in a gas turbine engine. A separator (700) includes a plurality of vortex chambers arranged about a longitudinal axis of the gas turbine engine, each ...
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WO/2018/015027A1 |
The invention relates to a flow machine (10), in particular a radial compressor, comprising a rotor (11) with a rotor blade (12); a stator (13) with, preferably, a guide vane (17), the stator defining at least in sections, the at least o...
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WO/2018/016623A1 |
This twin-shaft gas turbine facility is provided with: a twin-shaft gas turbine (10); an induction motor (22) coupled to a compressor (11) of the twin-shaft gas turbine (10); a secondary battery (23); a first frequency converter (24) whi...
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WO/2018/012100A1 |
A gas turbine equipped with: a low-pressure bleed passage (41), a medium-pressure bleed passage (42), and a high-pressure bleed-passage (43) for supplying compressed air bled from respective bleed chambers (25a, 25b, and 25c) to a turbin...
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WO/2018/005605A1 |
A product may include a bearing housing in which a shaft may be supported by a bearing so that it may rotate. A compressor wheel may be disposed on the shaft. A compressor cover may be connected with the bearing housing, which may form a...
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WO/2018/005610A1 |
A venting system (58) for a turbocharger may include a bearing housing (16). The bearing housing may include an inner member (42). A housing wall (40) may extend from the inner member and may include at least one vent (60) disposed there...
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WO/2017/220529A1 |
The invention relates to a method and a system (100) for storing a storage fluid (1), during which the storage fluid (1) is transferred between a withdrawn state at a lower pressure (p1a) and a stored state at a higher pressure (p1e), an...
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WO/2017/219656A1 |
Disclosed is a gas turbine and pressurized water reactor steam turbine combined circulation system, using a heavy duty gas turbine and a pressurized water reactor steam turbine to form a combined circulation system. Heat of the tail gas ...
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WO/2017/218088A1 |
A fan assembly is provided. The fan assembly includes a fan, a fan casing circumscribing the fan, and a fan casing heating system in thermal communication with the fan casing. The fan includes a hub, and a plurality of fan blades extendi...
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WO/2017/215878A1 |
The invention relates to a turbine (20) having an impeller (23) arranged in a housing (26). The turbine (20) has an inflow region (21) and an outflow region (22) and a working medium flows through said turbine during operation. The worki...
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WO/2017/213983A1 |
The invention relates to an insert piece for a bypass in a turbine housing having a connecting flange and a tubular portion. The connecting flange is suitable for joining the insert piece with a turbine housing. The tubular portion is de...
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WO/2017/210137A1 |
A hybrid power plant system (100) including a gas turbine system (109) and a coal fired boiler system (103) inputs high oxygen content gas turbine flue gas into the coal fired boiler system, said gas turbine flue gas also including carbo...
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WO/2017/206084A1 |
The invention discloses a regenerative cycle gas turbine system and a combined cooling heating and power system. The regenerative cycle gas turbine system comprises an air compressor, an air regenerator, a combustion chamber, a turbine, ...
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WO/2017/205082A1 |
The invention relates to a connection valve for a multi-flow turbine of an exhaust gas turbocharger and/or a turbine with such a connection valve. The connection valve comprises a housing and a valve body, wherein the valve body is arran...
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WO/2017/205397A1 |
A method includes installing a CHP system to be operated by an operator. The operator becomes qualified as a market participant in a wholesale electricity market. An electrical output generated from the CHP system is connected to a first...
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WO/2017/200940A1 |
A process for retrofitting an industrial gas turbine engine of a power plant where an old industrial engine with a high spool has a new low spool with a low pressure turbine that drives a low pressure compressor using exhaust gas from th...
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WO/2017/199818A1 |
Provided are a carbon-containing solid fuel gasification power generation facility, and a method for regulating a gas for drying this carbon-containing solid fuel, with which it is possible to expand the range of the types of carbon-cont...
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WO/2017/198397A1 |
The present invention relates to a system and a method for storing and releasing heat, which comprises at least two concentric heat storage volumes (TES1, TES2, TES3). The walls (2) defining said storage volumes are configured such that ...
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WO/2017/194253A1 |
The present invention relates to a device for heat exchange between a fluid and heat storage particles (6). The exchange system comprises two volumes (2, 3) for storing the particles, and an exchange zone (4) in which the fluid (F) and s...
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WO/2017/194282A1 |
The invention relates to a steel material (21a) for high-temperature applications as well as to a turbine casing (21) for a turbocharger (1) made of said steel material (21a), the steel material (21a) being characterized by a material co...
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WO/2017/190884A1 |
The invention relates to a turbine housing (21) for a turbocharger (1) of an internal combustion engine, comprising - an annular duct (22) for guiding an exhaust gas mass flow (AM) to a turbine wheel (12) that can be arranged in the turb...
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WO/2017/190940A1 |
The invention relates to a drive system for an aircraft (1) comprising an electrical generator (15) and an internal combustion engine (13) having a gas expansion turbine (25). The generator (15) has a rotor (17) rotatably mounted by mean...
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WO/2017/189566A2 |
A large frame heavy duty industrial gas turbine engine that produces twice the power as conventional single spool industrial engines and operates at full power during a hot day. The engine includes a high spool directly driving an electr...
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WO/2017/187619A1 |
The present invention comprises: a combustor for combusting ammonia as fuel; an ammonia vaporizer for vaporizing the ammonia; an ammonia supply unit for supplying the ammonia in a liquid state; an exhaust heat recovery boiler; a warm-wat...
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WO/2017/189217A1 |
An in-line propeller gearbox of a turboprop gas turbine engine includes a lubricant reservoir disposed spaced radially offset from the engine's central axis of rotation and asymmetrically with respect to the central axis of rotation such...
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WO/2017/189440A1 |
An industrial gas turbine engine with a high spool and a low spool in which low pressure compressed air is supplied to the high pressure compressor, and where a portion of the low pressure compressed air is bled off for use as cooling ai...
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WO/2017/178185A1 |
A turbomachine train (9) with two shaft parts which each have a fixedly attached grooved wheel (5), with a first overrunning clutch (7), with two rotational speed sensors and with a control device. The clutch is designed to couple and de...
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WO/2017/174287A1 |
The invention relates to a turbocharger (1) for an internal combustion engine, having a bearing housing (2) in which a shaft (3) is rotatably mounted, having a turbine housing (15), which is fixed mechanically to the bearing housing (2),...
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WO/2017/176186A1 |
The present invention relates to a turbine arrangement driven by exhaust gases from a combustion engine (2). The turbine arrangement comprises a turbine housing (7), a turbine wheel (6) rotatably arranged in the turbine housing (7), a fi...
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WO/2017/170477A1 |
A gas turbine (1) has: a compressor (2) for generating compressed air; a wheel casing (5) into which the compressed air is introduced; a combustor (3) for generating combustion gas; a turbine (4) driven by the combustion gas; a combustor...
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WO/2017/165768A1 |
A turbocharger turbine section (20) is disclosed. The turbine may include a first swing vane (28) rotatably coupled with a first pin (30) that may include a first leading edge, a first trailing edge, a first exhaust side edge extending b...
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WO/2017/163275A1 |
[Problem] To supply power efficiently via a variable-speed drive device in an intake air cooling system used in a gas turbine for supplying motive power to a refrigerant compressor in a natural gas liquefaction plant. [Solution] An intak...
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WO/2017/165598A1 |
The invention relates generally to electrical power systems or steam generator systems including generating capacity of a coal plant where specific emissions and power is improved with an alternately fueled engine driving one or more air...
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WO/2017/163499A1 |
This fuel cell system is provided with: a fuel cell which generates electric power by receiving a supply of an anode gas and a supply of a cathode gas; a compressor which supplies the cathode gas to the fuel cell; a turbine which produce...
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WO/2017/162401A1 |
The invention relates to a micro-gas turbine plant (1) comprising a combustion chamber (30) for generating exhaust gas by combustion of fuel supplied to the combustion chamber (30), a turbine (40) arranged in an exhaust gas line (50) dow...
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WO/2017/165261A1 |
The invention relates to an oil sealing unit for a turbocharger used for sealing a passage from a bearing housing to a compressor housing having an end wall, wherein the end wall serves to delimit an oil expansion chamber in the directio...
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WO/2017/160154A1 |
A process for generating power using a gas turbine, comprising the steps of: (i) vaporising and pre-heating liquid ammonia to produce pre-heated ammonia gas; (ii) introducing the pre-heated ammonia gas into an ammonia-cracking device sui...
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WO/2017/160200A1 |
The present invention relates to a compressor arrangement in an air line (9) supplying charged air to a combustion engine (2). The compressor arrangement comprises a compressor unit (14) comprising a housing (15) including an air intake ...
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WO/2017/159149A1 |
This CAES power generation apparatus 2 is provided with: a motor 14 which is driven by electricity generated using renewable energy; a compressor 16 which is driven by the motor 14; a pressure accumulator tank 20 which stores compressed ...
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WO/2017/159397A1 |
A multistage axial compressor according to the present invention is provided with a rotating shaft to which a plurality of moving blades is attached, a casing that surrounds the rotating shaft and that forms a flow path for a working flu...
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WO/2017/158378A1 |
The turbine arrangement includes a turbine including a turbine housing which defines a turbine cavity within which a turbine wheel is supported for rotation, a turbine inlet upstream of the turbine wheel and a turbine outlet downstream o...
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WO/2017/154459A1 |
A compressed air storage power generation device 2 is provided with a third heat exchanger 30 and fourth heat exchangers 40a, 40b. The third heat exchanger 30 exchanges heat between air exhausted from an expander 24 and a second heat med...
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WO/2017/148630A1 |
The invention relates to a rotor (01) for use in a gas turbine, comprising a plurality of compressor segments (21), a plurality of central segments (31), and a plurality of turbine segments (41); the compressor segments (21) and the turb...
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WO/2017/147810A1 |
Provided is a power generating system using multiple gas channels for power generation, comprising a central control unit (11), and a power generating mechanism electrically connected to the central control unit (11). The power generatin...
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