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Matches 1 - 50 out of 8,618

Document Document Title
WO/2018/187731A1
Re-lithiation methods and systems are disclosed. Example re-lithiation methods include separating lithium depleted active cathode material from a cathode and introducing lithium containing materials. Also disclosed are re-lithiation elec...  
WO/2018/186925A2
The present disclosure is directed to a gas turbine engine defining a longitudinal direction, a radial direction, and a circumferential direction, and an upstream end and a downstream end along the longitudinal direction. The gas turbine...  
WO/2018/180773A1
Provided is a combustion device equipped with: an ammonia supply unit (6) that, by supplying primary reduction ammonia as a nitrogen oxide reducing agent to within a combustor (2) and mixing secondary reduction ammonia with combustion ex...  
WO/2018/181063A1
This combustion device (C) causes the combustion of fuel ammonia and combustion air within a combustion chamber (N), and is equipped with a combustor liner (3a) which forms the combustion chamber, a burner (3c) which is attached to one e...  
WO/2018/180781A1
Provided is a gas turbine (A) using a denitration catalyst and ammonia as a reducing agent for the denitration of combustion gas, wherein the ammonia is supplied, along with cooling air supplied from a compressor (1), to turbine vanes (3...  
WO/2018/180996A1
This combustion device uses compressed combustion air to cause the combustion of fuel ammonia within a combustion chamber, and is equipped with a combustion air cooling unit (6) that cools the combustion air by means of heat exchange wit...  
WO/2018/181030A1
This combustion device (C) is equipped with a compressor (2a) for compressing combustion air, a combustor (2b) for causing the combustion of fuel ammonia and the compressed combustion air, and an ammonia injection unit (3) for injecting ...  
WO/2018/181002A1
This combustion device (C) is provided with a combustor (3) for causing the combustion of fuel ammonia and combustion air within a combustion chamber (N), and the combustor is equipped with a cooling ammonia supply unit (3g) for mixing t...  
WO/2018/180984A1
This combustion device uses combustion air to cause the combustion of fuel ammonia within a combustor (2), and is equipped with a catalyst reduction unit (4) for reducing nitrogen oxides in combustion exhaust gas supplied from the combus...  
WO/2018/178565A1
A device for temporarily increasing power (13) for increasing the power of at least one first turbomachine (5A) and at least one second turbomachine (5B), said device comprising a coolant reservoir (14), a first injection circuit (16A), ...  
WO/2018/173122A1
This combustor 20 comprises a tubular combustor liner 70, and a fuel nozzle 21A that is provided to one end of the combustor liner 70 and that sprays fuel and an oxidant into the combustor liner. The fuel nozzle 21A is provided with a pl...  
WO/2018/173012A1
A micro-combustion device (1) for the generation of electrical power, capable of raising the global performance of the system, with greater compactness and fewer losses by exploiting the principles of a combustion chamber with induced he...  
WO/2018/168747A1
Provided is a combustor nozzle equipped with a nozzle main body (2) extending along an axis, said nozzle main body (2) being equipped with: a first fuel passage (21) formed along the axis (Am) and through which a first fuel (F1) flows; f...  
WO/2018/169578A2
The present disclosure is directed to a method of operating a gas turbine engine with an interdigitated turbine section. The engine includes a fan rotor, an intermediate pressure compressor, a high pressure compressor, a combustion secti...  
WO/2018/167223A1
The installation (10) comprises: – at least one air-cooled heat exchanger (22), the air-cooled heat exchanger (22) comprising a tube bundle capable of accepting a flow (24) that is to be cooled, and a fan capable of causing a flow of a...  
WO/2018/162994A1
The present disclosure relates to systems and methods that are useful for controlling one or more aspects of a power production plant. More particularly, the disclosure relates to power production plants and methods of carrying out a pow...  
WO/2018/164775A1
A combustion section for gas turbine engine includes an inner liner, an outer liner, and a dome attached to the inner liner and to the outer liner. A heat shield is attached to the dome, with the dome, the heat shield, or both define an ...  
WO/2018/156262A1
The present disclosure is directed to a gas turbine engine defining a radial direction, a longitudinal direction, and a circumferential direction, an upstream end and a downstream end along the longitudinal direction, and an axial center...  
WO/2018/156235A1
The present disclosure is directed to a gas turbine engine defining a radial direction, a longitudinal direction, and a circumferential direction, an upstream end and a downstream end along the longitudinal direction, and an axial center...  
WO/2018/155239A1
Provided are a power generation system and a power generation system control method with which an optimum energy efficiency can be obtained by load sharing control without providing a power turbine with a governor. The power generation s...  
WO/2018/147950A3
The present disclosure is directed to a gas turbine engine defining a longitudinal direction, a radial direction, and a circumferential direction, and an upstream end and a downstream end along the longitudinal direction. The gas turbine...  
WO/2018/147950A2
The present disclosure is directed to a gas turbine engine defining a longitudinal direction, a radial direction, and a circumferential direction, and an upstream end and a downstream end along the longitudinal direction. The gas turbine...  
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...  

Matches 1 - 50 out of 8,618