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Matches 651 - 700 out of 8,554

Document Document Title
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...  
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...  
WO/2012/128813A3
Control system and method for controlling an integrated gasification combined cycle (IGCC) plant are provided. The system may include a controller coupled to a dynamic model of the plant to process a prediction of plant performance and d...  
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...  
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...  
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...  
WO/2012/128926A3
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...  
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...  
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...  
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...  
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) ...  
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...  
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...  
WO/2012/116285A3
A wave apparatus (21) comprising a wave rotor(61) further comprising a plurality of channels (95) each being elongated from an internal end (97) to an external end (99), each of the channels (95) having a constricted width dimension clos...  
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...  
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...  
WO/2012/112889A3
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...  
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...  
WO/2012/105053A1
Provided is a control device for a gas turbine power generation plant, the control device comprising: a compressor (1) pressurizing combustion air; an intake air sprayer (3) spraying a droplet of spray water supplied through a spray flow...  
WO/2012/104180A1
Liquid fuel assist ignition system (1) for providing a fuel -air mixture to a gas turbine in its start-up phase, comprising a high pressure tank (2), a vacuum pump (3) connected to the high pressure tank (2), a liquid fuel inlet (4) conn...  
WO/2012/100393A1
Disclosed is a critical low-entropy mixed combustion circulating thermal power system, comprising a working mechanism (1), a continuous combustion chamber (2), a liquid oxidant source (3), and a fuel source (4). The liquid oxidant source...  
WO/2012/101087A1
The invention pertains to fluegas recirculation in gas turbines, and specifically to an intake section (2) upstream of the inlet of a compressor (1) of a gas turbine unit (1-7) with fluegas recirculation, comprising at least one section ...  
WO/2012/103112A2
An apparatus for igniting a fuel mixture by applying EM energy is disclosed. The apparatus may include a radiating element configured to apply EM energy to the fuel mixture at a plurality of Modulation Space Elements (MSEs), and a proces...  
WO/2012/096940A1
Systems and methods for improving the operation of a combustion device using a low heating value fuel that includes providing a supply of a low heating value fuel, introducing an oxidizing agent that includes an enriched oxygen source in...  
WO/2012/092222A1
One embodiment of the present invention is a unique gas turbine engine. Another embodiment is a unique reheat system for a gas turbine engine. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations f...  
WO/2012/088566A1
The invention relates to a gas turbine engine that will find application in the mechanical engineering and in particular in the manufacturing of small-scale engines for vehicles and electricity generation. The gas turbine engine includes...  
WO/2012/092495A1
One embodiment of the present invention is a unique engine Another embodiment of the present invention is a unique combustion system, Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for engine...  
WO/2012/092216A1
A device capable of collecting a condensate from a working fluid is disclosed. The condensate can take the form of a liquid and can be injected into a flow path of an engine. In one form the engine is a gas turbine engine and the liquid ...  
WO/2012/079694A3
Invention relates to methods for operating a small gas turbine assembly and a small gas turbine assembly itself, comprising at least one compressor/compressor stage (1 - 4) and at least one turbine or turbine stage (10 - 11), in which co...  
WO/2012/079694A8
Invention relates to methods for operating a small gas turbine assembly and a small gas turbine assembly itself, comprising at least one compressor/compressor stage and at least one turbine or turbine stage, in which compressor and turbi...  
WO/2012/080633A1
The invention relates to a method for improving the acceleration efficiency of a gas generator of a gas turbine by reducing the take-up of electric power, in particular during the transition phases, in order to conserve a sufficiently la...  
WO/2012/074061A1
An energy recovery device (10) comprises a heat exchanger (14) which carries out the heat exchange between low-pressure condensed water (12) supplied from a regenerative superheater (11) and supply water (13) and a compressor (17) which ...  
WO/2012/071166A3
One or more heat exchangers (8) mounted in a duct (3) have heat transfer cooling passages (9) therein and a variable geometry flow restrictor (2) is integral with each of the heat exchangers (8). An annular slide valve (102) axially tran...  
WO/2012/064363A2
The power plant combusts a hydrocarbon fuel with oxygen to produce high temperature high pressure products of combustion. These products of combustion are routed through an expander to generate power. The products of combustion are subst...  
WO/2012/064363A3
The power plant combusts a hydrocarbon fuel with oxygen to produce high temperature high pressure products of combustion. These products of combustion are routed through an expander to generate power. The products of combustion are subst...  
WO/2012/064536A2
A turbine engine, such as for example a jet engine or turbojet, that is fueled by particulate fuel, such as cornstarch or other similar particulate products, that burn under deflagration conditions. The engine is modified from a standard...  
WO/2012/060739A1
The invention relates to gas turbine technology used to produce work and generate electrical power or as a drive for vehicles or gas pipeline compressor stations. According to the invention, in the method for operating a gas turbine unit...  
WO/2012/051997A2
The invention relates to a turbine wheel arrangement for a gas turbine comprising two successive turbine wheels (18, 20) rotating in opposite directions, wherein the first turbine wheel (18) comprises flow channels (42) of a Laval cross-...  
WO/2012/054079A3
An electricity generating assembly includes a first turbine having a first plurality of fan blades and a second turbine having a second plurality of fan blades. A first rotor is connected to the first turbine and rotatable with the first...  
WO/2012/052687A1
The aim of the present invention is to enable the cover of a centrifugal compressor to be moved such that the clearance between the cover and the blades of the compressor impeller remains substantially constant and as low as possible. To...  
WO/2012/051997A3
The invention relates to a turbine wheel arrangement for a gas turbine comprising two successive turbine wheels (18, 20) rotating in opposite directions, wherein the first turbine wheel (18) comprises flow channels (42) of a Laval cross-...  
WO/2012/051783A1
A jet engine with parallel combustion chambers is provided, which includes a power turbine duct (1), a jet-propelment duct (2), an intake duct (3), an air compressor (4) and a power turbine (5). The air compressor (4) is arranged in the ...  
WO/2012/051315A3
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/2012/051315A2
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/2012/045028A1
A dual fuel propulsion system 100 is disclosed including a gas turbine engine 101 capable of generating a propulsive thrust using a cryogenic liquid fuel 1 12. A method of operating an aircraft engine 101 is disclosed using a selected pr...  
WO/2012/042628A1
The purpose is to improve the output and the power generation efficiency utilizing hot water produced with a solar heat or a thermal energy of a combustion exhaust gas. This gas turbine power generation device (100) comprises: a compress...  
WO/2012/040214A9
The present disclosure provides methods, assemblies, and systems for power production that can allow for increased efficiency and lower cost components arising from the control, reduction, or elimination of turbine blade mechanical erosi...  
WO/2012/040214A1
The present disclosure provides methods, assemblies, and systems for power production that can allow for increased efficiency and lower cost components arising from the control, reduction, or elimination of turbine blade mechanical erosi...  
WO/2012/040195A3
A method of power production using a high pressure / low pressure ratio Brayton Power cycle with predominantly N2 mixed with CO2 and H2O combustion products as the working fluid is provided. The high pressure can be in the range 80 bar t...  
WO/2012/039890A1
A method and system are disclosed for co-production of olefins and electric power. The method includes determining a separation level, separating a hydrocarbon feed into a light fraction stream and a heavy fraction stream based on the de...  

Matches 651 - 700 out of 8,554