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Matches 1 - 50 out of 8,614

Document Document Title
WO/2018/142191A1
The present invention relates to a method for optimising continuous combustion systems that reduces fuel consumption, exhaust gas and particulate emissions. The operation principle is based on the introduction of small amounts of hydroge...  
WO/2018/143168A1
This combustion device (C) uses fuel air to combust a fuel within a combustion chamber (N), wherein the combustion device comprises a reducing agent injection device for injecting a reducing agent toward a flame within the combustion cha...  
WO/2018/143310A1
This hydrogen/oxygen equivalent combustion turbine system comprises a high-pressure steam turbine (2), a low-pressure steam turbine (3), and a heater (5) between the two turbines. The heater (5) has a combustion unit (53) that burns equi...  
WO/2018/138291A1
The present disclosure is directed to a shaft assembly (95) for a turbine engine (10), the shaft assembly (95) defining an axial direction and a radial direction, wherein the turbine engine (10) includes a fan or propeller assembly (14) ...  
WO/2018/134720A1
Here is described a process to transform energy in chemical form in fuels into electric power through a thermal process., It combines advantages of the traditional internal combustion engine and the steam engine by producing supercritica...  
WO/2018/128880A1
Processes for generating electric power are provided. The processes involve combining a supercritical water stream with a pressurized, heated hydrocarbon-based composition in a mixing device to create a combined feed stream. The combined...  
WO/2018/128791A1
A gas turbine engine defines a radial direction and an axial centerline. The gas turbine engine includes a core turbine engine that defines a core inlet. The core inlet is oriented with respect to the axial centerline and positioned alon...  
WO/2018/119920A1
An LNG gas turbine (10), comprising a combustion chamber (12), a turbine (14), and an air compressor (16). The air compressor (16) is drivingly connected to the turbine (14); the combustion chamber (12) comprises a combustion chamber inl...  
WO/2018/123922A1
Provided is a nozzle capable of providing a spray of a fine particle diameter while suppressing occurrence of coarse particles. This single-fluid nozzle having a J-shaped collision frame integrally provided to an outer surface of a spray...  
WO/2018/119921A1
An LNG gas turbine with inter-stage cooling, comprising a combustion chamber, a turbine, and an air compressor; the air compressor is communicated with the combustion chamber to provide compressed air to the combustion chamber; the turbi...  
WO/2018/119577A1
A gas turbine, comprising a combustion chamber (12), a turbine (14), and a compressor (16), and further comprising an injection-driven dual-working medium compressor (10). The injection-driven dual-working medium compressor supplies fuel...  
WO/2018/117874A1
Sweep-based gas separation processes are used for reducing carbon dioxide emissions from gas power plants. The invention involves at least two compression steps, a combustion step, a carbon dioxide capture step, a power generation step a...  
WO/2018/110460A1
Provided is a transition duct 30 that forms an annular gas flow channel 40 through which a main flow gas flows from a high-pressure turbine to a low-pressure turbine, wherein the gas flow channel 40 has an inner peripheral flow channel s...  
WO/2018/110474A1
Disclosed is a starting device (1) that drives a compressor-side rotary shaft (11) of a two-shaft gas turbine engine (GT) at the time of startup of the gas turbine engine, the starting device comprising: a starter motor (15) serving as a...  
WO/2018/106528A1
A waste heat recovery system including a drive unit, the drive unit having a drive shaft, a compressor, the compressor operably coupled to the drive shaft, wherein operation of the drive unit drives the compressor, and a waste heat recov...  
WO/2018/105166A1
The invention provides a means of utilizing electrical energy by electrolyzing deep sea water to generate hydrogen gas and oxygen gas which are allowed to rise to the sea surface because the gases have a specific gravity of lower than 1,...  
WO/2018/100368A1
A method of extending the useful life of an aged selective catalytic reduction (SCR) catalyst bed, which catalyses the conversion of oxides of nitrogen (NOx) to dinitrogen (N2) in the presence of a nitrogenous reductant, in the exhaust g...  
WO/2018/094536A1
The present disclosure generally relates to rotary turbomachinery methods and integrated processes requiring high-energy efficiency. In one embodiment, the present invention relates to rim-rotor configurations enabling long-term survival...  
WO/2018/093429A1
A multistage radial microturbine device comprising at least three compressor stages and at least three turbine stages.  
WO/2018/087694A1
The present disclosure relates to systems and methods useful for power production. In particular, a power production cycle, comprising a first combustor (102) and a turbine (103), utilizing CO2 as a working fluid may be configured for si...  
WO/2018/088184A1
The gas turbine plant is provided with a gas turbine (10), a heating device (60), a decomposition gas line (70), and a decomposition gas compressor (85). The heating device (60) heats ammonia so that the ammonia is pyrolyzed and decompos...  
WO/2018/085046A1
A power transmission system (210) for a turbine (200) or a compressor has a housing (220), a first shaft rotatably mounted so as to be rotatable in one direction in the housing, a barrel (202) rotatably mounted so as to be rotatable in a...  
WO/2018/076926A1
An engine driven by gunpowder, relating to the technical field of engines and comprising an engine, a gas storing bag (3), a draft fan (6) and a gunpowder burner; the engine comprises an engine housing (1) which is provided therein with ...  
WO/2018/078350A1
A gas turbine engine (1) has a centrifugal compressor (4) and a radial turbine (14) mounted to a turbine shaft (2) for rotation with the shaft about the shaft axis Z. A number of combustion chambers (10) in the air/gas flow path between ...  
WO/2018/075015A1
Turbine fuel provided for large-scale land based turbines used by utilities for producing electricity and desalinated water, and for large mobile engines and turbines in marine and remote applications where only liquid fuels are availabl...  
WO/2018/071738A1
A hydraulic fracturing system that includes a fixed-speed gas turbine assembly (18) having a gas generator and power turbine, both mounted to a semi-trailer. The system further includes a hydraulic pump (28) mounted to the semi-trailer a...  
WO/2018/070394A1
The purpose of the present invention is to provide a furnace wall in which a throat section with a smaller channel diameter than other regions can be formed using all peripheral wall pipes. Provided is a furnace wall comprising: a plural...  
WO/2018/071260A1
A gas turbine engine includes a compressor section and turbine section. The gas turbine engine of the present disclosure is a relatively small gas turbine engine, configured to generate less than 1491 kW (2,000 horsepower) during peak op...  
WO/2018/059885A1
A rotating device for a compressor of a gas turbine is presented. The rotating device, connectible within the compressor, includes a first shaft, a second shaft, rotatable blades, a bearing assembly, an energizable drive and an input por...  
WO/2018/063610A1
A gas turbine engine includes a compressor section and a turbine section. A first spool is rotatable with a first turbine of the turbine section and a first compressor of the compressor section. Additionally, a second spool is rotatable ...  
WO/2018/057523A1
Methods and systems of power generation that integrate SCO2 Bray ton and Rankin steam power cycles with fossil fuel combustion, One such method involves combusting a fuel material with an oxidizer material in a combustor to produce heat ...  
WO/2018/052616A1
A gas turbine engine includes a fan section and a core turbine engine. The fan section includes a fan and a fan shaft, with the fan including a plurality fan blades rotatable with the fan shaft. The core turbine engine includes a turbine...  
WO/2018/050964A1
The gas turbine comprises a compressor (10), a combustor (20), and a turbine (30). The method comprises: compressing air with the compressor and feeding compressed air continuously to the combustor, feeding fuel to the combustor, continu...  
WO/2018/042336A2
The present invention relates to a cryogenic air separation process that provides high pressure oxygen for an oxy-fired combustion of a fuel (e.g., a carbonaceous fuel). The air separation process can be directly integrated into a closed...  
WO/2018/042338A1
The present disclosure relates to systems and methods for power production utilizing an ion transfer membrane (ITM) unit. An air stream and a fuel stream can be passed through the ITM unit so that the fuel is at least partially oxidized ...  
WO/2018/042336A3
The present invention relates to a cryogenic air separation process that provides high pressure oxygen for an oxy-fired combustion of a fuel (e.g., a carbonaceous fuel). The air separation process can be directly integrated into a closed...  
WO/2018/044251A1
The invention relates to a method and a device for thermochemical conversion of municipal solid waste and other carbon-rich feedstock with high content of tars into synthesis gas. Conversion occurs in a two-stage process of pyrolysis (zo...  
WO/2018/044252A1
The invention relates to a method and a device of thermochemical conversion of municipal solid waste and other carbon-rich feedstock with high content of tars into synthesis gas. Conversion occurs in a two-stage process of pyrolysis (zon...  
WO/2018/044558A1
The invention relates to the compression of a pyrolysis product to facilitate light olefin separation. The pyrolysis product is produced in a pyrolysis reaction. A power generator produces a first shaft power and a second shaft power. Th...  
WO/2018/043568A1
This two-shaft gas turbine equipment is provided with: an induction motor (22) which transmits and receives power to and from an external system (1); and a speed reducer (40) which makes the rotational speed of a motor rotor (22r) of the...  
WO/2018/036891A1
The present application provides a selective catalyst reduction system for use with a combustion gas stream of a gas turbine. The selective catalyst reduction system may include an inlet positioned about the gas turbine, a combined ammon...  
WO/2018/038876A3
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 ...  
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 ...  
WO/2018/038876A2
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 ...  
WO/2018/025294A1
This combustor 20 comprises: a combustor liner 61 that is provided in a combustor casing 70; a cylindrical body 80 that partitions the space between the combustor casing 70 and the combustor liner 61; piping 42 that guides combustion gas...  
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...  
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...  
WO/2018/009668A1
A fuel gas blending system for internal combustion engines combines two or more gas streams to achieve a blended fuel gas having a suitable heating value (HV) for a given engine. A relatively high HV gas, for example gas produced from an...  
WO/2018/000799A1
A power device comprises a spiral gas flow passage realizing a combination of axial flow and circumferential flow. The spiral gas flow passage comprises an intake section (9a), an intermediate section (10a), and an exhaust section (11a)....  
WO/2018/003488A1
This gas turbine combustor comprises: a casing which is coupled to a main housing; a liner which has an interior in which a combustion chamber extending in the axial direction is formed, the liner comprising an upstream portion, includin...  

Matches 1 - 50 out of 8,614