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WO/2013/038001A1 |
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/2013/040323A2 |
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/2013/029914A1 |
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/2013/028164A2 |
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/2013/028167A2 |
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/2013/028169A1 |
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/2013/023725A1 |
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/2013/024231A1 |
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/2013/015899A1 |
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/2013/016704A2 |
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/2013/014176A1 |
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/2013/016703A2 |
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/2013/015883A1 |
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/2013/016705A2 |
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/2013/009636A2 |
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/2013/006957A1 |
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/2013/001238A1 |
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/2012/172405A1 |
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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WO/2012/172235A1 |
Turbine engine (10) comprising a low-pressure compressor (12), a high-pressure compressor (14), a low-pressure turbine (20), a high-pressure turbine (18) and regulating means (30) for regulating the rotational speed of the low-pressure t...
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WO/2012/171094A1 |
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/2012/173651A1 |
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/2012/164228A1 |
The invention relates to a gas turbine engine for propelling an aircraft, comprising: a low‑pressure rotary body (10) having mobile low‑pressure turbine blades (10T), an intermediary rotary body (20) having mobile intermediary turbin...
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WO/2012/165968A1 |
System and method for treating cargo vapors from crude oil and petroleum products tanks (2) to generate electrical power. The system and method comprising the steps: separating the cargo vapors into liquid volatile organic compounds (LVO...
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WO/2012/164371A2 |
In a system and a method for gas turbine flue gas recirculation for recirculating at least a portion of a flue gas generated in gas turbine of a gas turbine power generation system an oxygen feed unit (18) is arranged to bring a recircul...
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WO/2012/161711A1 |
Described herein are gradual oxidation systems that receive and process solid, liquid, or gaseous fuels. The system can include a solid fuel gasifier that extracts and cleans gas fuel from a solid fuel. The system can also include a reac...
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WO/2012/155314A1 |
A hybrid power generation system and method based on classification of solid fuel pyrolysis and semi-coke combustion are provided. The system comprises a pyrolysis device (1) for pyrolysing solid fuel to produce gas, liquid and solid sem...
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WO/2012/156597A1 |
The invention relates to a turbine engine including a detonation chamber and an aircraft provided with such a turbine engine. The chamber (4) of the turbine engine (1) comprises a continuous detonation wave engine (6) provided with an an...
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WO/2012/152447A1 |
The invention is directed to a turbo-engine, particularly internal combustion engine, comprising a housing and therein a bladeless turbine section (30; 42; 67) of the stacked disc- or Tesla-type construction, wherein the turbine section ...
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WO/2012/151606A1 |
A hot-air engine (10) includes a compressor (12), a heating chamber (14), a rotary displacement type working engine (16) and a drive means (22). The compressor (12) has an inlet (12a) and an outlet (12b). The heating chamber (14) has an ...
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WO/2012/151625A1 |
An integrated drying gasification system comprises a gasifier for gasifying carbonaceous fuel to produce hot product gas and an entrained flow dryer which receives the hot product gas to dry the carbonaceous fuel prior to gasification. A...
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WO/2012/148172A2 |
Disclosed is a system for producing syngas and reducing tar using air/steam on a fluidized bed, which includes a gasifier (10) in which a solid fuel is gasified to produce a combustible syngas; a first loop seal (20) connected to the gas...
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WO/2012/147752A1 |
This system is provided with: a fluidized bed drying device (102) in which fluidized gas (107) is fed to a drying chamber to thereby fluidize and dry low-grade coal fed to the drying chamber; a raw-coal fluidized bed bunker (50) for temp...
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WO/2012/146399A1 |
The invention relates to a method (1) and a device (1) for generating electricity from waste gases (3) containing hydrogen sulfide, in particular from the natural gas industry (2). The method according to the invention is characterized i...
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WO/2012/142124A2 |
Crosslinked hydrogel-based transdermal pharmaceutical formulations. The hydrogel transdermal formulations. Transdermal patches are useful for administering a variety of drugs to patients. The transdermal patches here employ crosslinked-h...
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WO/2012/138447A1 |
A burner assembly for combusting fuel in a combustion zone to reduce NOx emissions includes a water spray subassembly including a water outlet configured to direct water at an angle with respect to an axis of the burner assembly, the wat...
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WO/2012/132062A1 |
Disclosed is a method for operating a gas compressor which compresses a gas fuel, a supply condition of which fluctuates, and is provided with a suction flow rate adjustment mechanism, wherein the limit pressure ratio that defines the op...
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WO/2012/134325A1 |
The present application provides a power augmentation system with dynamics damping for a gas turbine engine. The power augmentation system may include a transition piece of a combustor and a steam manifold positioned about the transition...
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WO/2012/128928A1 |
Systems, methods, and apparatus are provided for generating power in combined low emission turbine systems and capturing and recovering carbon dioxide from the exhaust. In one or more embodiments, the exhaust from multiple turbine system...
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WO/2012/128926A2 |
Systems, methods, and apparatus are provided for generating power in low emission turbine systems and separating the exhaust into rich CO2 and lean CO2 streams. In one or more embodiments, the exhaust is separated at an elevated pressure...
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WO/2012/128923A2 |
Systems, methods, and apparatus are provided for controlling the oxidant feed in low emission turbine systems to maintain stoichiometric or substantially stoichiometric combustion conditions. In one or more embodiments, such control is a...
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WO/2012/129579A1 |
This invention relates to an engine. More specifically, the invention relates to a fixed volume, multi-propellant engine (10, 110) capable of operation without any mechanical or electrical means of compression and/or ignition. The engine...
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WO/2012/128925A2 |
Systems, methods, and apparatus are provided for controlling the oxidant feed in low emission turbine systems to maintain stoichiometric or substantially stoichiometric combustion conditions. In one or more embodiments, such control is a...
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WO/2012/123684A1 |
The aim of the invention is to improve the energy efficiency of a turbojet engine by optimizing the rotating speed of the fan and the operability of the engine. To this end, the invention proposes freeing the fan from the exclusive contr...
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WO/2012/120555A1 |
The objective of the present invention is to provide a solar heat utilization gas turbine system with which the effect of disturbances in the weather conditions and the like can be reduced for a gas turbine which sprays water into the in...
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WO/2012/121917A2 |
An integrated power generation system for reducing carbon dioxide emissions is provided. The integrated system comprises a gas turbine having an air inlet, a fuel inlet and an exhaust gas outlet; a steam-assisted gravity drainage (SAGD) ...
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WO/2012/117365A1 |
A fluid machine having an impeller (12; 61) with a plurality of blades and including a fluid inlet room and a fluid outlet room wherein an extra blade wheel (2; 7) rotatably mounted independent of the rotation of the impeller (12; 61) is...
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WO/2012/113104A1 |
A less-combustion high-efficiency engine includes an internal combustion engine (1) and a high-pressure oxidant source (2). An intake gas source of an intake duct (100) of the internal combustion engine is set as an oxygen-free gas sourc...
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WO/2012/113523A1 |
According to the invention, the jet engine (1) includes at least one vaporization duct (5) arranged on the outer wall (2a) of a combustion chamber of the jet engine (1) and extending over the entire length thereof between an ejection val...
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WO/2012/114367A1 |
The purpose of the present invention is to provide a gas turbine system which utilizes solar heat, the gas turbine system being configured so that the release of energy to the outside of the system caused by the intermediate cooling of a...
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WO/2012/112889A2 |
A micro-turbine engine, consisting of at least a compressor, combustor, and turbine, is a complicated fluid flow device that controls the flow rate and thermodynamic properties of a working fluid in order to generate shaft power. Existin...
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