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Matches 701 - 750 out of 8,554

Document Document Title
WO/2012/031783A2
A gaseous hydrocarbon stream (10) is cooled against a first refrigerant and a second refrigerant, to produce a liquefied hydrocarbon stream (20). The first refrigerant is cycled in a first refrigerant circuit (100), comprising compressin...  
WO/2012/031782A1
A gaseous hydrocarbon stream (10) is cooled against a first refrigerant and a second refrigerant, to produce a liquefied hydrocarbon stream (20). The first refrigerant is cycled in a first refrigerant circuit (100), comprising compressin...  
WO/2012/032557A1
A gas turbine power generation system capable of efficiently and continuously supplying both electric power and service water is provided. A gas turbine power generation system is provided with a gas turbine (1) for driving a power gener...  
WO/2012/033564A1
Disclosed herein are screw shaft turbine compressors having (i) a compressor section, (ii) a turbine section, (iii) a combustion section coupling to the compressor section and the turbine section, and (iv) a grooved shaft. The grooved sh...  
WO/2012/032516A3
An energy generation system and method are presented for use in operating a heat engine. The energy generation method comprises: reducing a CO2 gas into CO and O2 gases; reacting said CO and O2 gases, thus combusting the CO gas, and yiel...  
WO/2012/028430A1
The invention relates to a method for reliably flushing the exhaust gas recirculation line (8) of a gas turbine (14) having exhaust gas recirculation, without using additional blow-out fans, and to a gas turbine (14) for carrying out the...  
WO/2012/031297A2
A system of dense packaging of turbomachinery in a gas turbine engine by means of close-coupling of components and by the ability to rotate various engine components with respect to other engine components is disclosed. In addition, spoo...  
WO/2012/024898A1
A small temperature rise low-entropy mixed-fuel engine includes a combustion chamber, an expansive agent source (2) and a fuel source (3). The fuel source (3) is in communication with the combustion chamber through a fuel input control m...  
WO/2012/018457A1
Provided are more efficient techniques for operating gas turbine systems. In one embodiment a gas turbine system comprises an oxidant system, a fuel system, a control system, and a number of combustors adapted to receive and combust an o...  
WO/2012/018458A1
The present techniques are directed to a combustor for a gas turbine. For example, an embodiment provides a spool piece for the combustor. The spool piece includes an oxidant injection port configured for injection of an oxidant proximat...  
WO/2012/014401A1
A gas turbine (1) comprises: multiple stage compressors (2, 3); a combustor (4) for injecting a fuel into air compressed by the compressors and combusting the fuel; and a turbine (5) driven by the combustion gas from the combustor. In th...  
WO/2012/013289A3
The invention relates to a method and device for storing electrical energy (1), wherein hydrogen (3) and oxygen (4) are produced from water (2) by electrolysis (E), are introduced into a storage apparatus (H, O), and are stored separatel...  
WO/2012/009575A3
In some implementations, a system may include a compressor, a heat exchanger and an ITM. The compressor is configured to receive an air stream and compress the air stream to generate a pressurized stream. The heat exchanger is configured...  
WO/2012/009575A2
In some implementations, a system may include a compressor, a heat exchanger and an ITM. The compressor is configured to receive an air stream and compress the air stream to generate a pressurized stream. The heat exchanger is configured...  
WO/2012/008013A1
A desalination device operated by a membrane method and a concentration device operated by a vaporization method are used in combination to thereby stably concentrate water containing a salt, such as accompanying water, at a low equipmen...  
WO/2012/005619A1
The gas turbine engine with two-way air feed includes a shaft 1, active rotor 2 of the gas turbine on two side of it rotors 8,17 of first and second centrifugal compressors with vanes 3,6 are installed; between them an internal guiding d...  
WO/2012/001684A2
In today's lifestyle it is not always practical to be able to prepare foodstuff on a freshly prepared basis. Therefore partial cooking of foodstuff and preparation for heating and completion of cooking is used. An apparatus, a container ...  
WO/2012/003078A1
Methods and systems for low emission power generation in hydrocarbon recovery processes are provided. One system includes a gas turbine system configured to stoichiometrically combust a compressed oxidant and a fuel in the presence of a ...  
WO/2012/001334A1
The invention relates to a device for protecting against the overspeed of a free turbine (6) of a turbine engine which comprises a gas generator including at least one compressor (1), a combustion chamber (3), at least one linked turbine...  
WO/2012/003079A1
Methods and systems for low emission power generation in hydrocarbon recovery processes are provided. One system includes a gas turbine system configured to stoichiometrically combust a compressed oxidant derived from enriched air and a ...  
WO/2011/163289A3
Emissions and combustion dynamics of a turbine engine are managed through a combustor system that injects water (4) into the primary fuel flow (3) and supplies a secondary water stream (8A, 8B) to the flame zone of the combustor through ...  
WO/2011/162960A3
The present techniques provide systems and methods for recovering energy from flare gases in chemical plants and refineries. The systems use an engine to burn a portion of gas diverted from the flare system. The engine may be a reciproca...  
WO/2011/163192A3
A system includes a fluidization device (18) including a flow passage (34) configured to convey a flow of solid fuel particles (36) in a downstream direction, and a body (44) disposed within the flow passage (34). The body (44) is config...  
WO/2011/157418A1
The present invention relates to a gas turbine combustion chamber arrangement having an annular combustion chamber (1), having a diffuser element (2) which is arranged upstream of the annular combustion chamber (1) in the flow direction ...  
WO/2011/157943A1
The invention relates to a turbine engine (100) for a helicopter (200), said helicopter comprising a main gearbox, a rotor (204), and a speed-reducing device (206) that is placed entirely within the main gearbox (202) of the helicopter w...  
WO/2011/154280A1
The invention relates to gas turbine engines, especially a turbojet or turbofan for an aircraft. The gas turbine engine comprising a combustion section and an exhaust section produces an exhaust gas. The emission products can be reduced ...  
WO/2011/154528A1
The invention relates to a method (30) for starting or stopping a gas turbine (1) including a combustion chamber (6) supplied, according to one or more feed controls, with a gas fuel that can comprise one or more given different gases, e...  
WO/2011/156203A2
A method of optimizing operation of a furnace to control emission within a system. Each furnace zone inside of the furnace is associated with at least one exhaust zone. A signal indicative of an amount of byproduct exiting the furnace th...  
WO/2011/149924A2
A method for utilizing landfill gas is disclosed herein. The method includes the step of collecting landfill gas. The method also includes the step of fueling a turbine engine that is at least part of a power generation system with the l...  
WO/2011/149914A1
A process for the clean-up of a crude syngas stream having widely varying composition and particulate load. The process includes quenching the crude syngas stream with a liquid stream to cool the syngas stream and remove particulates, ta...  
WO/2011/146096A2
A gas turbine engine having a ramburner is disclosed. The ramburner is disposed downstream of a gas turbine engine combustor and receives an engine exhaust flow from the gas turbine engine combustor. The ramburner also accepts a bypass a...  
WO/2011/145690A1
Disclosed is a gasification power generation plant provided with a gasification furnace (101) which has a fluid passage (131) allowing circulation of fluid to be heat-exchanged with the inside of the furnace and which gasifies fuel to ge...  
WO/2011/139309A2
The present invention provides in one embodiment a unique gas turbine engine. Another embodiment is a unique gas turbine engine combustion system. Still another embodiment is a unique gas turbine engine combustor. Other embodiments inclu...  
WO/2011/136832A2
One embodiment of the present invention is an integrated aero-engine flowpath structure. Another embodiment is a method of manufacturing integrated aero-engine flowpath structure. Other embodiments include apparatuses, systems, devices, ...  
WO/2011/136832A3
One embodiment of the present invention is an integrated aero-engine flowpath structure. Another embodiment is a method of manufacturing integrated aero-engine flowpath structure. Other embodiments include apparatuses, systems, devices, ...  
WO/2011/130002A1
A splitter (148) is provided for improving a pressure recovery of a compressor discharge casing (CDC) (114) of a gas turbine engine. The CDC includes an annular wall (142) that extends generally axially along at least a portion of the CD...  
WO/2011/125976A1
Provided are a heat engine which emits no carbon dioxide and no nitrogen oxide and achieves the simplification of the structure thereof, and a power generation system using the heat engine. The heat engine is characterized by being an in...  
WO/2011/122594A1
Disclosed is an integrated coal gasification combined cycle power generation plant, wherein combustion gas is combusted by a combustor (17) after being gasified in a gasification furnace (9) to which coal is led. The exhaust, emitted by ...  
WO/2011/121355A3
A gas turbine engine arrangement comprising a first engine section (2), the first engine section (2) comprising a first compressor (4) and a first turbine (6) mounted on a first shaft (8), the gas turbine engine arrangement further compr...  
WO/2011/118372A1
Provided is a lean-fuel intake gas turbine which has no pressure loss in the exhaust gas line that may lead to a drop in engine output and can be reduced in size of the gas turbine. The lean-fuel intake gas turbine includes a compressor ...  
WO/2011/112146A1
A gas turbine power generation plant including: a solid fuel gasifier (5) for the production of a fuel gas stream, an arrangement for fuel gas treatment, a combustor (4) for receiving the fuel gas stream and for the production of a flue ...  
WO/2011/109008A1
An oxy-combustor is provided to combust oxygen with gaseous low heating value fuel. A compressor upstream of the combustor compresses the fuel. The combustor produces a drive gas including steam and carbon dioxide as well as other non-co...  
WO/2011/106073A2
One embodiment of the present invention is a vane assembly for a gas turbine engine. Another embodiment of the present invention is a damper seal that may be employed in conjunction with a vane assembly of a gas turbine engine. Other emb...  
WO/2011/104685A2
The engine comprises: a stator (2) including an inlet opening (1) intended to admit a compressed gaseous oxidant flow, and an exhaust opening (6) intended to discharge burnt gases; and a rotor (3) mounted in the stator (2) in a fluid-tig...  
WO/2011/104685A3
The engine comprises: a stator (2) including a stator inlet opening (1) intended to admit a compressed gaseous oxidant flow, and a stator exhaust opening (6) intended to discharge burnt gases; and a rotor (3) mounted in the stator (2) in...  
WO/2011/101711A1
An engine (10) and a method of operating the engine are provided. The engine (10) includes a gas turbine (20) and fan (40) that rotate together to provide an exhaust gas flow stream, which flows over a free turbine (46) that is connected...  
WO/2011/097121A3
A turbine engine assembly for a generator including a turbine engine having a compressor section (12), a combustor section (30) and a turbine section (14). An air bleed line is in communication with the combustor section for receiving co...  
WO/2011/091424A1
An interface for a pressurized fluidized bed combustion facility is disclosed that enables future addition of carbon dioxide capture technology to capture facility flue gas emissions. The interface includes a gas to water pressurized hea...  
WO/2011/083137A1
The invention relates to a contra-rotating propeller system for an aircraft turbine engine, including a free power turbine including a first rotor and a second rotor contra-rotating relative to said first rotor, a first contra-rotating p...  
WO/2011/084551A2
A recuperative gas turbine generator comprised of a combustor and a turbine driven by the combustor as well as a compressor and a drive shaft linking the turbine and the compressor along a common rotational drive axis. At least one elect...  

Matches 701 - 750 out of 8,554