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WO/2013/069111 |
Provided are a gas turbine electricity generation device, and an operating method therefor, with which the output can be improved by spraying heated water obtained with the heat energy of solar heat, and with which stable operation can b...
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WO/2013/069123 |
A control device for a gas turbine power-generating plant provided with: a compressor (1) for pressurizing the combustion air; an air intake spraying device (3) that sprays sprayed water droplets supplied via a spray flow adjustment valv...
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WO/2013/066432 |
A system for the gradual oxidation of fuel is disclosed. The system includes an oxidizer that has a reaction chamber with an inlet and an outlet. The reaction chamber is configured to receive a fluid comprising an oxidizable fuel through...
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WO/2013/066433 |
A system for the gradual oxidation of fuel is disclosed. The system includes an oxidizer that has a reaction chamber with an inlet and an outlet. The reaction chamber is configured to receive a fluid comprising an oxidizable fuel through...
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WO/2013/067149 |
The present disclosure provides an integrated power generating system and method and liquefied natural gas (LNG) vaporization system and method. More particularly, heat from a CO2 containing stream (15) from the power generating system a...
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WO/2013/065624 |
The present invention is equipped with: a combustor (2) having a fuel injection nozzle (4) that injects hydrogen gas (H) and pure water (W); a water storage tank (12) that stores the pure water (W) supplied to the combustor (2); a gas co...
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WO/2013/060516 |
The present invention relates to a gas turbine (100) comprising a combustion chamber (101) with an exhaust section (102) through which a combustion gas (103) is exhaustable, a plenum chamber (104) and a compressor (105) for generating a ...
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WO/2013/061928 |
This liquefied gas treatment system is provided with: a compression means (2) which compresses outside air; a pressurized combustion means (6) which comprises a furnace (3) into which the compressed outside air is led as jacket air and c...
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WO/2013/061303 |
A method for modifying a gas turbine burner assembly (1), which extends along an axis (A) and comprises a premix main burner (3) and a pilot burner (5), about which the main burner (3) is arranged; the pilot burner (5) comprises a swirle...
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WO/2013/061662 |
The objective of the present invention is to provide a rotary internal combustion engine with which compressed air obtained from the outside is used and the compressor is not driven from the output shaft, thereby eliminating compression ...
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WO/2013/058253 |
The objective of the present invention is to provide a method for controlling a gas-turbine power plant, a gas-turbine power plant, a method for controlling an oven for gasification of a carbon-containing fuel, and an oven for gasificati...
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WO/2013/058209 |
The present invention relates to a lean fuel intake gas turbine which is capable of stable operation avoiding an accidental fire at a catalytic combustor and an explosion in a compressor even when there is a change in fuel concentration....
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WO/2013/056437 |
A turbine engine with multiple working substances comprises a turbine (20) used for transforming energy of working substances to mechanical energy, a first working substance inlet passage, and a second working substance inlet passage. Th...
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WO/2013/058210 |
According to a low-concentration methane gas oxidation system of the present invention, waste heat from a gas turbine engine may be used effectively, and a stable operation may be available by avoiding a burning of a catalyst even in a c...
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WO/2013/059456 |
A method is disclosed to enable the efficient physical packaging of gas turbine engine components to optimize power density, more readily integrate with other equipment and facilitate maintenance. The method illustrates dense packaging o...
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WO/2013/049898 |
The engine with the circular (rotation) movement of the piston 2, where the piston 2 is shaped as a cross, has four branches where is located combustion chamber of mixture in the piston 9. Piston is directly connected to the shaft (crank...
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WO/2013/052442 |
An aero-derivative gas turbine engine having: a gas turbine engine core including a high pressure compressor (65) interconnected with a high pressure turbine (73) by a high pressure shaft (142) in a geometric arrangement appropriate for ...
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WO/2013/052438 |
A casing for a can annular gas turbine engine, including: a compressed air section (40) spanning between a last row of compressor blades (26) and a first row of turbine blades (28), the compressed air section (40) having a plurality of o...
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WO/2013/042500 |
This power conversion system (S) is equipped with: a hydrogen generation device (1) that heats a supplied organic hydride in the presence of a prescribed catalyst and generates hydrogen and a dehydrogenation product of the organic hydrid...
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WO/2013/040679 |
The present disclosure introduces a rotor assembly having a concentric arrangement comprising a rotating turbine portion, a cooling channel and an annular reinforcement wall. The concentric arrangement is configured to rotate around a co...
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WO/2013/043077 |
A gas turbine includes a plurality of combustors within an outer turbine shell, arranged about a rotor of the gas turbine, each combustor having a combustion chamber defined by a liner with an end cover at a forward end supporting at lea...
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WO/2013/043754 |
An energy storage system utilizing compressed gas as a storage medium, may include one or more turbines configured to convert energy in gas expansion and compression processes. One or more axial and centrifugal turbines may be used to st...
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WO/2013/038001 |
For coupling the gas turbine process to the indirect gasification of solid fuels, particularly by means of steam, and to avoid the use of heat pipes (26) that must be operated using dangerous liquid alkali-metals, a second combustion cha...
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WO/2013/040323 |
A gas turbine engine includes a compressor for compressing air from an environment; a combustor for receiving the compressed air from the compressor, mixing the compressed air with fuel, and combusting the fuel; a turbine coupled with th...
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WO/2013/040323 |
A gas turbine engine includes a compressor for compressing air from an environment; a combustor for receiving the compressed air from the compressor, mixing the compressed air with fuel, and combusting the fuel; a turbine coupled with th...
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WO/2013/029914 |
The invention relates to a mixing unit (1) for mixing water with steam in a bypass station, wherein a plurality of Laval nozzles (5, 5a, 5b,...) are arranged in the mixing unit (1), which Laval nozzles (5, 5a, 5b,...) are displaced axial...
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WO/2013/028169 |
A combustion device used in gas turbine engines to produce propulsion or rotate a shaft for power generation includes a can-annular combustor with a system of fuel and air inlet passages and nozzles that results in an optimal combustion ...
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WO/2013/028164 |
A combustion device used in gas turbine engines to produce propulsion or rotate a shaft for power generation includes an annular combustor with a system of fuel and air inlet passages and nozzles that results in a staged combustion of pr...
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WO/2013/028167 |
A combustion device used in gas turbine engines to produce propulsion or rotate a shaft for power generation includes a can-annular combustor with a system of fuel and air inlet passages and nozzles that results in an optimal combustion ...
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WO/2013/023725 |
The invention relates to a method for feeding back exhaust gas from a gas turbine with a downstream waste heat boiler, wherein this exhaust gas is metered into the air inflow stream of a gas turbine, with the result that the temperature ...
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WO/2013/025612 |
A method for operating an electrical energy storage system is described. Electrical energy is supplied to electrolyze first water to produce hydrogen and oxygen. A turbine is operated from the hydrogen and the oxygen to combine the hydro...
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WO/2013/024231 |
A method of determining the performance of at least one propeller of a turbomachine in an incident air stream (V) comprising an axial component (Vz) and a tangential component (V), said propeller being modelled by a generalized theoretic...
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WO/2013/016704 |
A system configured for the production of at least one product selected from the group consisting of syngas, Fischer-Tropsch synthesis products, power, and chemicals, the system comprising a dual fluidized bed gasification apparatus and ...
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WO/2013/016705 |
A system configured for the production of at least one product selected from the group consisting of syngas, Fischer-Tropsch synthesis products, power, and chemicals, the system comprising a dual fluidized bed gasification apparatus and ...
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WO/2013/016703 |
A system configured for the production of at least one product selected from the group consisting of syngas, Fischer-Tropsch synthesis products, power, and chemicals, the system comprising a dual fluidized bed gasification apparatus and ...
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WO/2013/016703 |
A system configured for the production of at least one product selected from the group consisting of syngas, Fischer-Tropsch synthesis products, power, and chemicals, the system comprising a dual fluidized bed gasification apparatus and ...
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WO/2013/015883 |
A cost-effective solution for the disposal of solvent deasphalting process bottoms that include spent solid adsorbent material containing ash-producing constituents, asphalt and process reject materials is provided by introducing them in...
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WO/2013/015899 |
A process for the production of a synthesis gas containing hydrogen and carbon monoxide utilizes ground coke having a predetermined ash content in combination with a refinery residual hydrocarbon oil feedstream for gasification in the co...
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WO/2013/016704 |
A system configured for the production of at least one product selected from the group consisting of syngas, Fischer-Tropsch synthesis products, power, and chemicals, the system comprising a dual fluidized bed gasification apparatus and ...
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WO/2013/014176 |
The invention relates to a method for running up a stationary gas turbine (10) comprising at least one combustion chamber (14), the burners of which comprise a pilot burner and a main burner and by which various types of fuel are introdu...
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WO/2013/016705 |
A system configured for the production of at least one product selected from the group consisting of syngas, Fischer-Tropsch synthesis products, power, and chemicals, the system comprising a dual fluidized bed gasification apparatus and ...
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WO/2013/009636 |
A gas turbine engine having a compressor section using blades on a rotor to deliver a gas at supersonic conditions to a stator. The stator includes one or more of aerodynamic ducts that have converging and diverging portions for decelera...
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WO/2013/006957 |
A methanol indirect combustion combined-cycle power generation apparatus and method. A liquid methanol input stream is evaporated to provide a gaseous methanol stream which is converted to syngas that is combusted in a gas turbine assemb...
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WO/2013/009631 |
A gas turbine engine with a compressor rotor having compressor impulse blades that delivers gas at supersonic conditions to a stator. The stator includes a one or more aerodynamic ducts that each have a converging portion and a diverging...
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WO/2013/009636 |
A gas turbine engine having a compressor section using blades on a rotor to deliver a gas at supersonic conditions to a stator. The stator includes one or more of aerodynamic ducts that have converging and diverging portions for decelera...
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WO/2013/001238 |
The invention relates to a housing for the accessory relay of a gas turbine having a front side surface and a rear side surface (14) opposite the front surface, in which a peripheral flange (16) contains the housing, and in which at leas...
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WO/2013/003654 |
Engine systems and associated methods, including systems with semi- isothermal compression devices are disclosed. An engine system in accordance with a particular embodiment includes a compressor having a compressor inlet and outlet, a c...
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WO/2012/173651 |
An aircraft engine fuel system 900 is disclosed having a gas turbine engine 101, a turbocharger 910, a compressor bleed air system 930 for providing compressor air (A) from the gas turbine engine 101 to the turbocharger 910, and a fuel d...
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WO/2012/171094 |
The present disclosure relates to combustion systems and components for rotary ramjet engines. An injection system, optionally stratified for ease of engine startup, provides an air and fuel mixture to a combustion chamber. An ignition s...
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WO/2012/172405 |
The present invention relates to a system (1) for capturing C02 from a flue gas deriving from combustion of hydrocarbons which has been generated in a gas turbine (12) wherein the system comprises means for recirculating the flue gas (18...
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