| Document |
Document Title |
|
WO/2009/082275A1 |
The invention relates to a gas turbine engine comprising a first flow passage (1), and main combustion means (4) in the first flow passage (1). The engine further comprises a second flow passage (11), and first catalytic combustion means...
|
|
WO/2009/080994A2 |
Cogeneration or trigeneration process using an adiabatic compressor/gas turbine assembly combined with a gasifier or with at least one catalytic steam reforming unit, characterized in that said process employs at least first and second H...
|
|
WO/2009/076062A2 |
A variable nozzle for a turbocharger (10) has a nozzle ring (138) supporting an array of vanes (134) that are variable in setting angle. The nozzle ring (138) is rotationally oriented and fixed in position by a plurality of circumferenti...
|
|
WO/2009/073406A2 |
A rotary mechanically reciprocated sliding vane air pump is integrated with pulse driven boundary layer gas turbines on a single shaft. The shaft is slotted and is aligned with a slotted rotor that mechanically drives a reciprocating sli...
|
|
WO/2009/068048A1 |
The invention relates to a drive device (1) having compression modification in the form of a thermal rotary engine (2) with internal combustion, particularly a thermal jet engine such as a turbine or the like, having a stator (8) compris...
|
|
WO/2009/069426A1 |
A combustion burner (10A) comprising a fuel nozzle (110), a burner tube forming an air passage between the fuel nozzle (110), swirler vanes (130) arranged at a plurality of positions along the circumferential direction on the outer circu...
|
|
WO/2009/069443A1 |
Provided is a composite-type coal gasification power plant facility in which the power generation efficiency can be prevented from being lowered even if a low-grade coal having relatively high moisture content is used. The power plant fa...
|
|
WO/2009/059364A1 |
A method of extracting more energy from a stream of gas possibly from an exhaust of an internal combustion engine with constrained back pressure resulting at its inlet where the gas stream will be directed Into a turbine there being a pa...
|
|
WO/2009/052622A1 |
Method to provide fugitive gases to an engine. A source of fugitive gases is directed to the air intake of the engine. A fugitive gas pipe supplies the fugitive gases to the air intake and a vent allows the fugitive gases to vent to atmo...
|
|
WO/2009/041617A1 |
A working fluid containing CO2 comprised of a molecule with a small ratio of specific heat as a main component is expanded in a gas turbine (4). An exhaust gas having a high temperature can be obtained, even if a pressure changes between...
|
|
WO/2009/040112A2 |
The invention refers to a power supplying device or system for aeronautics, having a hydrocarbon supply (400) for supplying an engine (400) with hydrocarbon fuel and a hydrogen supply (100) having a fuel reformer (120) for producing hydr...
|
|
WO/2009/039611A2 |
A method for generating energy from sulphur combustion without causing harmful emissions to the environment entails steps of evaporating liquid sulphur to generate sulphur dioxide gas and sulphur vapor, combusting the sulphur vapor with ...
|
|
WO/2009/036458A1 |
A novel method of combing the CTL fuel plant and IGCC electrical plant by sharing the systems of coal intake, coal preparation, gas separation, and water units is described herein. This configuration allows for the combined facility to o...
|
|
WO/2009/036455A2 |
|
|
WO/2009/031945A2 |
The invention relates to gas turbine plants. The oil systems of a gas turbine engine and of actuating units are designed in the form of individual adjustable flow circuits each of which comprises fuel-oil heat exchangers (10, 11), the co...
|
|
WO/2009/032253A1 |
The part load method controls delivery of diluent fluid, fuel fluid, and oxidant fluid in thermodynamic cycles using diluent, to increase the Turbine Inlet Temperature (TIT) and thermal efficiency in part load operation above that obtain...
|
|
WO/2009/022103A2 |
There is described a gas turbine engine (10) comprising a gas inlet (12), a compressor (14), a combustion chamber (16), and a gas outlet (20) at or near the periphery of the combustion chamber. The gas inlet (12) is located at or near an...
|
|
WO/2009/015430A1 |
The present invention is concerned with a power generation process and system (10) comprising gasifying (12) a carbonaceous fuel source to yield a synthesis gas (17); cooling the synthesis gas; removing carbon dioxide from die cooled syn...
|
|
WO/2009/008743A1 |
A circular run gear-piston engine comprising an external combustion chamber (1) connected to a toroidal cylinder (5) via a fluid inlet (7), a fluid outlet (8) for exhaust fluids to depart from the cylinder (5), and an annular gear-piston...
|
|
WO/2009/005146A1 |
A blast furnace gas burning facility of simple arrangement and its operation method, which can be operated at a substantially rated load while preventing a wet type dust collector from freezing even under the conditions that the temperat...
|
|
WO/2009/004307A1 |
This invention relates to the separation of carbon dioxide gas from a substantially particulate free pressurised gaseous stream of steam and carbon dioxide, such as that generated by the oxidation of a fossil feedstock used in the genera...
|
|
WO/2009/002179A1 |
This invention relates to a method and plant for combined electric energy and water production, where the method comprises feeding substantially pure oxygen and a hydrocarbon fuel in a stochiometric ratio to a combustor (5), combusting t...
|
|
WO/2008/155242A1 |
The invention relates to a method for the safe, low NOx emission operation of a gas turbine system having fuel gas that is rich in hydrogen, and a gas turbine system having a device for exhaust gas recirculation into the compressor inlet...
|
|
WO/2008/149731A1 |
A gasifying agent supply passage (A) from an axial flow compressor (21) for increasing the pressure of the gasifying agent to a gasification furnace (2) is branched, and a gasifying agent bypass passage (D) provided with an escape pressu...
|
|
WO/2008/146579A1 |
A combustor (14) is placed next to a turbine (16), on the side opposite a compressor (12). A heat insulation device (20) for reducing the transmission of heat from the high-temperature side to the low-temperature side is provided between...
|
|
WO/2008/145954A2 |
An aircraft (40) comprising a gas turbine engine (10) that exhausts a plume of gases in use, the aircraft comprises an ultrasound generator (50) having an ultrasonic actuator (52) and a waveguide (54) to direct ultrasonic waves at the ex...
|
|
WO/2008/147523A1 |
The present invention provides systems, methods, and apparatus for abating effluent from an electronic device manufacturing system using cogeneration. The invention includes a pump adapted to couple to a processing chamber and adapted to...
|
|
WO/2008/145953A2 |
A method of operating an aircraft (40), and the aircraft. itself, comprising a gas turbine engine (10) that exhausts a plume of gases in use weherein the aircraft comprises an electromagnetic radiation generator (50) and a waveguide (54)...
|
|
WO/2008/141839A2 |
The invention relates to a method for the treatment of raw product gas produced by pressure gasification of solid fuels. After cooling to 15 to 45 °C, the following substances are removed by physisorption with cold oxygenate: in a preli...
|
|
WO/2008/140433A2 |
This invention is particularly relates to the systems producing ventilation, cooling, heat, pressure or void space (vacuum) to energy systems, especially to shaft working power, impulsive driver, electricity power supply, jet drive and v...
|
|
WO/2008/138735A2 |
The invention relates to a method for producing electric energy from solid and liquid fuels (13, 32), wherein the fuels (13, 32) are first subjected to a gasification process (1) at high pressure, and the scrubbed gasification gas is fed...
|
|
WO/2008/135362A1 |
The invention relates to a method for the safe, low NOx emission operation of a gas turbine system having combustion gas rich in hydrogen, and a gas turbine system having a device for water injection into fuels rich in hydrogen into a ga...
|
|
WO/2008/136119A1 |
A gas turbine utilizing cold heat of LNG, comprising a compressor (1), a combustor (2), a turbine (3), and a load, is further provided with a cooling device (6) installed in a system (36) for introducing suction air to the compressor (1)...
|
|
WO/2008/129652A1 |
To provide a gas turbine power generating apparatus which is capable of igniting and starting while stably keeping the pressure balance of an entire system even if the capacity of the apparatus is increased by increasing the difference i...
|
|
WO/2008/124767A2 |
Disclosed is a process to start-up, operate, and shut down a gasifier and an integrated gasification combined cycle complex without flaring while additionally reducing the release of contaminants such as carbon monoxide, hydrogen sulfide...
|
|
WO/2008/119245A1 |
A flywheel engine comprises a housing (23) on which a flywheel shaft (3) attached to at least one flywheel (15) is mounted, ignition system, starting system and fuel system. A gas-mixture chamber (4) is mounted on the flywheel (15). The ...
|
|
WO/2008/113088A1 |
The invention relates to a turboprop engine (1) comprising at least one compressor (2), rotatably arranged on a shaft (11), for compressing air sucked in via air inlets (7), at least one combustion chamber (5) for igniting and combusting...
|
|
WO/2008/105815A2 |
A gas turbine engine having speed an intermediate stage booster configured to provide speed change to a boost compressor. The boost compressor and fan stage are driven by a low pressure turbine; the fan stage rotates with the low pressur...
|
|
WO/2008/097096A1 |
A system and method for the reduction of NOx emissions from a gas turbine system, in which air is provided to the fuel gas line for partial premixing with the fuel gas flow so as for reducing the combustion chamber temperature and flame ...
|
|
WO/2008/097247A2 |
An exhaust system for an aircraft has a primary exhaust duct for communicating exhaust gas from an engine exhaust exit and is configured for movement with the engine. A secondary exhaust duct is in fluid communication with the primary ex...
|
|
WO/2008/091158A1 |
A method for enhancing carbon dioxide capture from flue gases produced in a combustor in a gas power plant or thermal power plant comprising a combustor, an oxygen separation device, one or more turbine plants comprising a turbine unit a...
|
|
WO/2008/089925A2 |
The invention relates to a gas turbine engine, particularly an aircraft engine, comprising a combustion chamber (1) and a gas turbine (2) for generating driving power and/or thrust, a compressor that has at least two stages and encompass...
|
|
WO/2008/089082A1 |
A high-pressure system and method utilizing an input fluid. The system includes a reactor treating a material to produce an effluent having an energy content, a plurality of stages compressing the input fluid in a stepwise manner providi...
|
|
WO/2008/088225A1 |
A rotating device for producing pressure from a process substance by expansion, which device includes a U-channel structure (120) rotatably arranged on an axis (121,122) including an expansion point (105) arranged at the periphery of the...
|
|
WO/2008/082336A1 |
The invention relates to a power transmission device (2) for a gas turbine engine (1) comprising a low pressure shaft (11) and a high pressure shaft (10), wherein the high pressure shaft (10) is arranged concentric to the low pressure sh...
|
|
WO/2008/082335A1 |
The invention relates to a power transmission device (2) for a gas turbine engine comprising a low pressure shaft (11) and a high pressure shaft (10), wherein the high pressure shaft (10) is arranged concentric to the low pressure shaft ...
|
|
WO/2008/082334A1 |
A gas turbine engine with a power transmission device (2) comprising: a first turbine shaft (11) of said gas turbine engine (1); a power output shaft (24); a gear mechanism (14) arranged to provide a variable gear change between said fir...
|
|
WO/2008/075022A1 |
The present invention relates to the processing of biomass, particularly but not exclusively poultry litter, to generate energy. A method is presented for generating power from biomass comprising a gasification process (44) involving the...
|
|
WO/2008/074099A1 |
A process for improving the performance, power output and/or rating of a gas turbine which is mechanically coupled to and drives a compressor producing compressed air, the process including the following steps: (a) humidifying all or a p...
|
|
WO/2008/068596A2 |
A method and a system (1) for the gasification of biomasses for the production of combustible gas are described. The system comprises a fixed-bed gasifier (10) in which the biomass undergoes a controlled combustion in oxygen deficiency, ...
|
