| Document |
Document Title |
|
WO/2005/019622A1 |
A cogeneration system capable of switching a bypass damper surely even when power supply is interrupted at the time of abnormality with no possibility of leaking exhaust gas and can be enlarged in scale at an advantageous cost. An exhaus...
|
|
WO/2005/017321A1 |
A variable nozzle device comprises an annular passage which is formed by two opposing wall members (3, 6; 17, 18, 6) which are separated along a rotational axis. A rotation conversion mechanism (9, 35; 172, 181) for converting a rotation...
|
|
WO2004046524B1 |
A system and method for creating power and pasteurizing water is provided. The system includes a power generation subsystem and a water pasteurization subsystem, which are linked together as follows. The power generation subsystem compri...
|
|
WO/2005/003577A1 |
According to the invention, an axial friction bearing, for the bearing of the rotating shaft of an exhaust gas turbocharger, connected to a lubrication circuit, with at least one essentially planar sliding surface and at least one bearin...
|
|
WO/2005/001974A1 |
A fuel cell/constant pressure turbine/hybrid system which is capable of making effective use of the heat energy of exhaust gas from a constant pressure high temperature type fuel cell, which makes it unnecessary to use a separate protect...
|
|
WO/2004/111412A1 |
Electric power supply equipment capable of maintaining a stable power generation against a variation in fuel gas supply amount and a variation in its fuel gas heating value, comprising a gas engine, a gas turbine, intake devices (6) for ...
|
|
WO/2004/109075A1 |
A method of combustion comprising providing fuel (13) to a turbine combustor (14), supplying air (21) to form a fuel/air mixture having an equivalence ratio greater than 0.55 supplying cooled combustion gases (37) and mixing with the air...
|
|
WO/2004/109076A1 |
The invention relates to a gas turbine (1) comprising at least one turbine (11, 20, 20’), at least one compressor (2, 5) driven by the turbine and a combustion chamber (16) arranged between the compressor and the turbine in the airflow...
|
|
WO/2004/106718A1 |
A method of operating a gas turbine power plant comprising of a first gas turbine group (10), consisting of a compressor (12) and a turbine (13) which are connected mechanically with one another, and a second gas turbine group (20), incl...
|
|
WO/2004/093294A1 |
An electric motor cartridge comprises a first cartridge housing portion (2) and a second cartridge housing portion (3). The cartridge housing portions (2, 3) are coupled together so as to assembly the electric motor cartridge (1) by radi...
|
|
WO/2004/087839A1 |
A fluid catalyst of a fluidized bed gasifier (1) has a tar decomposing function and is equipped in a fluid catalyst holding section (6) for generating thermal decomposition produced gas produced by thermally decomposing the raw material....
|
|
WO/2004/085801A1 |
The inventive power supply unit can be used for thermal electric power plants combusting various coal of different quality. According to said invention, turbine (7) exhaust gases are removed to a gas pipeline (21). A required gas flow ra...
|
|
WO/2004/083729A2 |
The invention relates to a cogeneration method and device using a turbine, such as a gas turbine, comprising a compression section (14), at least one expansion section (18, 52, 96) and a combustion chamber (20). The inventive method comp...
|
|
WO/2004/083606A1 |
A nozzle comprising a passage defined by an inner wall (11) and an outer wall (13) with at least one of opposite portions of said vane (2) extending therein, wherein at least one of opposite portions of said vane (2) is urged towards one...
|
|
WO/2004/081482A1 |
A gas turbine engine (1) and recuperator system (5) includes a bypass valve (100) for the recuperator (50) which is situated in a duct (70) that surrounds the recuperator (50). The valve (100) is adapted to directly open and close an ope...
|
|
WO/2004/074655A1 |
A compound cycle engine (10) comprises a compressor and a turbine section (14, 18), and at least one cycle topping device (16) providing an energy input to the turbine section (18). The compressor section (14) compresses the air accordin...
|
|
WO/2004/074641A1 |
In a station for stepping up the pressure in a natural gas or other fuel gas pipeline, the waste heat discharged from a gas turbine is utilized to generate steam by a waste heat recovery boiler. This steam is passed to a steam turbine to...
|
|
WO/2004/072450A1 |
The invention relates to a production method and to an assembly for a gas turbine system having a low output, which can be used as a shaft output gas turbine, a hot gas generator or as an air supplier. The aim of the invention is to prov...
|
|
WO/2004/072451A1 |
A pulse detonation engine system (1) for driving a turbine is comprises a detonation generator section (5) including a detonation tube (7) having a tubular hollow section for permitting detonation to be generated therein during combustio...
|
|
WO/2004/073134A2 |
Backup energy systems utilizing compressed air storage (CAS) systems and bridging energy systems to supply backup power to a load are provided. During a power failure, the bridging energy system provides backup power to the load at least...
|
|
WO/2004/072452A1 |
Combined thermal and compressed air storage systems are provided that utilize an exhaustless heater, such as a thermal storage unit, to provide power with enhanced efficiency. Compressed air is heated by the thermal storage unit prior to...
|
|
WO/2004/067918A2 |
An integrated steam-ammonia power cycle is disclosed which achieves a close match to a glide heat source such as exhaust from a gas turbine, and which also eliminates sub-atmospheric pressure operation. With reference to Figure 1, the ex...
|
|
WO/2004/065215A1 |
A system and method for an engine bleed flow-sharing control system is disclosed. For a multi-engine bleed system, one (10) of the engines is selected as the master channel (15) such that the bleed air supply pressure of the control syst...
|
|
WO2004046523A9 |
A low or no pollution power generation system is provided. The system has an air separator to collect oxygen. A gas generator is provided with inputs for the oxygen and a hydrocarbon fuel. The fuel and oxygen are combusted within the gas...
|
|
WO/2004/053295A1 |
A system for providing back-up electrical power in the event of failure of the utility electrical supply, which comprises a vessel (11) adapted to contain a volume of compressed gas supplied by a compressor (10), a solenoid valve (14) to...
|
|
WO/2004/054029A1 |
The invention relates to anode exhaust gas treatment methods for solid oxide fuel cell power plants with CO2 capture, in which the unreacted fuel in the anode exhaust (301) is recovered and recycled, while the resulting exhaust stream (3...
|
|
WO/2004/044386A2 |
An combined ornganic rankine and vapor compression cycle evaporator (14) cools gas turbine inlet air and the cycle’s boiler (17) receives heat from turbine exhaust. A common condenser (71) may be used for both the rankine and vapor com...
|
|
WO/2004/044102A1 |
A slurry production and storage system utilizing waste heat, characterized in that it comprises a reactor (102) in a subcritical water for forming a solid waste slurry fuel (110) from a solid waste (109), an internal combustion engine (1...
|
|
WO/2004/042200A1 |
It is disclosed a method of operating a gas turbine power plant and gas turbine power plant wherein hydrogen (6) for the combusting process is produced by feeding natural gas (14) mixed with steam (15) through a membrane/partial oxidatio...
|
|
WO/2004/031669A1 |
A reduced carbon dioxide emission system and method for providing power for refrigerant compression and shared electrical power for a light hydrocarbon gas liquefaction process.
|
|
WO2003087564B1 |
This invention relates to improved combustion methods and systems of Water Combustion Technology, WCT, based upon the chemistry of Water (H2O) incorporating Hydrogen (H2) and Oxygen (O2), as well as H2O as fuel. The WCT described in this...
|
|
WO/2004/031668A1 |
A system and method for the production of liquified light hydrocarbon gases by a system and a process that produces a liquified gas product more efficiently and with reduced emissions of carbon dioxide (CO2) to the atmosphere.
|
|
WO/2004/031667A2 |
A reduced carbon dioxide emissions system and method for providing power for refrigerant compression and shared electrical power for a light hydrocarbon gas liquefaction process.
|
|
WO/2004/031670A1 |
Disclosed are methods for efficiently and economically designing, constructing, or operating a light hydrocarbon gas liquefaction process for the liquefaction of selected quantities of light hydrocarbon gas. The method includes a light h...
|
|
WO/2004/029432A2 |
A gas turbine engine. The engine is based on the use of a gas turbine driven rotor having a compression ramp traveling at a local supersonic inlet velocity (based on the combination of inlet gas velocity and tangential speed of the ramp)...
|
|
WO/2004/029418A1 |
A device for handling and recovering of kinetic energy in a fluid is presented which basically features a bladed impeller (11). The impeller is operated by an electric engine (12) and acts as a centrifugal blower yielding energy to the a...
|
|
WO/2004/027219A1 |
Variable geometry turbochargers (10) comprise a turbine housing (12) having an exhaust gas inlet (14) and outlet (16), a volute connected to the inlet, and a nozzle wall (24) adjacent the volute. A turbine wheel (17) is carried within th...
|
|
WO/2004/022926A1 |
A turbocharger comprises a variable nozzle device and an exhaust housing being mechanically and/or thermally decoupled from the variable nozzle device. Additional optional advantageous features are provided, including various axial and r...
|
|
WO/2004/022948A1 |
A jet or turbine motor that includes a radial or diagonal compressor containing at least one rotating part pivoted in the fixed part of the jet or turbine motor when a synchronous electromotor containing a mutually cooperating stator and...
|
|
WO/2004/018856A1 |
A power quality system (10) has a gas turbine unit (20) with at least one turbine stage. The gas turbine unit comprises a first gas turbine shaft (30), a first compressor stage (40), a first turbine stage (50), a first generator/motor (6...
|
|
WO/2004/018855A1 |
A power quality system (10) has two separate turbine units, a first turbine unit (20) with a first turbine shaft (30) and a second turbine unit (40) with a second turbine shaft (50). The first turbine unit comprises a first compressor st...
|
|
WO/2004/011789A1 |
A microturbine engine operable to combust a flow of VOCs without a combustor. The microturbine engine comprising a compressor (15) having an inlet (52), the inlet receiving a mixture of air and VOCs, the compressor operable to produce a ...
|
|
WO/2004/009961A1 |
The invention relates to an exhaust gas turbocharger for an internal combustion engine, said turbocharger comprising an exhaust gas turbine in the exhaust gas system and a compressor in the induction tract. A regulatable throttle device ...
|
|
WO/2004/005685A1 |
The invention relates to a storage power station (S), for example an air storage plant, comprising a compressor unit (V), a turbine unit (T), and a storage volume (100). Said storage power station is operated according to a special mode ...
|
|
WO/2004/003362A1 |
A power fluctuation suppressing method wherein by-product gas produced in a plant is used as a fuel for a high-efficiency combined cycle power generation facility so as to generate power, the calorific value is increased while using, as ...
|
|
WO/2003/102401A1 |
An integrated-cycle power system and method, comprising thermal transfer assembly (600), recuperating heat exchanger assembly (300), heat integrator (400), thermal conduit assembly and gas turbine (700). The thermal transfer assembly rec...
|
|
WO/2003/100233A1 |
A highly supercharged gas-turbine generation system include a gas turbine power plant that is supercharged to a high inlet pressure, preferably over about 1.15 pressure ratio and preferably includes a transmission system with refrigerate...
|
|
WO/2003/100221A1 |
The invention relates to an exhaust-gas turbine for a turbocharger whose turbine wheel is rotationally mounted inside a turbine housing having a spiral intake port (13), to which an annular space (8) surrounding the turbine wheel is conn...
|
|
WO/2003/097394A2 |
A power generating system is integrally provided with a gas turbine engine (GT) and a solid electrolyte type fuel cell (FC). A compressor wheel (17), a turbine wheel (18), a heat exchanger (20) and a burner (27) of the gas turbine engine...
|
|
WO/2003/095812A1 |
The invention relates to a variable exhaust-gas turbocharger of an internal combustion engine and a compressor, each of which has at least one variable actuating element in the induction region. The exhaust gas turbocharger is configured...
|
