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Matches 1 - 50 out of 8,506

Document Document Title
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...  
WO/2017/222516A1
The present disclosure is directed to systems and processes which prevent fluid droplet impact damage by surface engineering a respective component (2) to exhibit a water receding contact angle ≥ about 120 degrees upon contact with dro...  
WO/2017/212211A1
A radial flow turbine heat engine (2) includes a compressor (6), a recuperator (10), a combustor (12) and a turbine (8). A compressor outlet manifold (14) collects compressed gas from the compressor through a plurality of compressor outl...  
WO/2017/203155A1
The invention relates to an aircraft turbine engine, including at least one rotary body comprising a compressor rotor and a turbine rotor connected to one another by a rotor shaft, the turbine engine being configured to drive a member by...  
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...  
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...  
WO/2017/200665A1
A gas turbine engine includes a core engine, a low pressure turbine, a fan assembly, a gearbox, and a lubrication scavenge pump. The core engine includes a high pressure compressor, a combustor, and a high pressure turbine configured in ...  
WO/2017/196293A1
The present disclosure provides a method for predicting a fluid type, comprising sensing, by a first sensor, mass flow data of a fluid in an engine, wherein the first sensor operates based on a first fluid property; sensing, by a second ...  
WO/2017/195094A1
A mixed flow turbine (1) for the expansion phase of steam thermodynamic cycles of an organic Rankine cycle provided with a first section (A) in which a first expansion of a main flow of working fluid takes place, in a substantially radia...  
WO/2017/193035A1
A gas turbine power generation system includes a core engine and a low pressure compressor. The core engine includes a high pressure compressor, a combustor, and a high pressure turbine configured in a serial flow arrangement. The high p...  
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...  
WO/2017/189566A3
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...  
WO/2017/188052A1
The integrated gasification combined cycle power generation plant comprises: a gasification furnace; a gas turbine which is configured to be drivable by using combustible gas generated by the gasification furnace as fuel; a flow rate con...  
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...  
WO/2017/182980A1
The present disclosure relates to systems and methods wherein a dilute hydrocarbon stream can be oxidized to impart added energy to a power production system. The oxidation can be carried out without substantial combustion of the hydroca...  
WO/2017/170834A1
Provided is a combustor comprising: a nozzle body (16) having a shaft body (24) extending along an axis, the shaft body (24) having a purge air flow passage (29) formed therein so as to extend along the axis to the front end of the shaft...  
WO/2017/170784A1
A combustor (3) for mixing and burning fuel gas, water vapor, and air, and used in a gas turbine, said combustor being equipped with: a fuel injection device (13) having a fuel injection unit (33) that directly injects the fuel gas (H) i...  
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...  
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...  
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...  

Matches 1 - 50 out of 8,506