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Matches 701 - 750 out of 8,405

Document Document Title
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...  
WO/2011/084551A3
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...  
WO/2011/079997A1
A turbine and a method for converting energy are provided, wherein an angular position φ33 of an exit (33) of a cooling duct (25) in the casing depends on angular positions φ21 of a downstream edge (21) of a guide vane (17) and on an a...  
WO/2011/082232A1
The present invention provides in one embodiment of the present invention a surge margin power recuperation system. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for recuperating power from ...  
WO/2011/061764A1
The application relates to a method and a system for storing renewable energy and recycling carbon oxides as renewable fuel.  
WO/2011/061299A1
In a process according to the invention for the emission-free generation of energy and/or hydrocarbons and other products by utilizing carbon-containing materials, in a first process stage (P1) carbon-containing materials are supplied an...  
WO/2011/061079A1
A method and an apparatus' for converting energy into electricity using a gaseous working fluid and an evaporative fluid, the method comprises pressuring the working fluid (20) in a compressor (1), heating the high-pressure working fluid...  
WO/2011/054698A1
The invention relates to a chemical reactor (2) of a technical plant, in particular a power plant system, comprising a gas-tight wall forming a gas channel (5), wherein heat exchanger surfaces that are permeable with a first fluid and at...  
WO/2011/056928A3
A micro gas turbine engine for use in a turbo heater or co-generation application is described. The micro gas turbine engine includes a fuel delivery system which minimizes the development of deposits in the air-fuel passageway. To this ...  
WO/2011/056928A2
A micro gas turbine engine for use in a turbo heater or co-generation application is described. The micro gas turbine engine includes a fuel delivery system which minimizes the development of deposits in the air-fuel passageway. To this ...  
WO/2011/056341A1
The present application provides an integrated gasification combined cycle system (230). The integrated gasification combined cycle system may include a gas turbine engine (110), a syngas system (115) for producing a syngas (190) for the...  
WO/2011/055575A1
Provided is a turbine wheel which is provided with a plurality of vanes and which is shaped into a scallop shape obtained by notching a backboard-side portion between the suction surface of each vane and the pressure surface of the adjac...  
WO/2011/056928A4
A micro gas turbine engine for use in a turbo heater or co-generation application is described. The micro gas turbine engine includes a fuel delivery system which minimizes the development of deposits in the air-fuel passageway. To this ...  
WO/2011/054803A1
A method for centrifugal separation of condensed CO2 from a flue gas comprises: - combusting a mixture of fuel and oxygen enriched air in a combustion chamber (26) to generate heat and flue gas (27); - splitting the flue gas (27) into a ...  
WO/2011/056303A3
An air compression and expansion system having a combined motor-generator unit and a single drive shaft coupled to compressors and expanders is disclosed. The system includes a motor-generator unit, a drive shaft connected to the motor-g...  
WO/2011/053138A1
A method for generating electrical energy, wherein a carbonaceous fuel is gasified to a combustible gas, the combustible gas is combusted to drive an apparatus chosen from a gas turbine and a gas engine, and relatively hot exhaust gas fr...  
WO/2011/045363A1
The present invention relates to a device for filtering the intake air of an internal combustion engine, including at least one filtering element (8) having an inlet for air being treated, a first clean air outlet toward the engine and a...  
WO/2011/045047A3
The invention relates to a Rankine cycle (RC) or an organic Rankine cycle (ORC) for utilising the waste heat from biomass combustion for generating electricity as well as to a corresponding system. In order to achieve an improvement of t...  
WO/2011/039059A1
The invention relates to a method for operating an IGCC power plant process having integrated CO2 separation. A process gas containing H2 and CO2 is separated into technically pure hydrogen and a fraction rich in CO2 by means of pressure...  
WO/2011/037597A1
An annular combustion (22) chamber and a transient plasma system (42) in communication with the annular combustion chamber (22) to sustain a spinning detonation wave. This system (42) is also called as "nanosecond pulsed plasma" system a...  
WO/2011/038188A1
A gas turbine engine having an adaptive core (10) capable of maintaining a substantially constant core pressure ratio while having a variable flow rate is disclosed. In one aspect, the adaptive core composes a front block compressor (30)...  
WO/2011/038196A1
A method of operating a compressor in an adaptive core engine is disclosed. The method comprises the steps of operating a front block compressor (30) to increase pressure of a fluid to a first pressure ratio in a high-power mode operatio...  
WO/2011/035241A1
Provided herein are systems, methods and equipment that include Integrated Gasification Combined-Cycle technology to retrofit existing plants, that include, e.g., subsystems for separating char fines from syngas after it emerges from an ...  
WO/2011/033244A1
The invention relates to a free-turbine turboshaft engine including, on the one hand, a gas generator comprising at least one compressor (1) supplied with air, a combustion chamber (5) receiving the compressed air at the output of said c...  
WO/2011/033204A1
The invention relates to a turbine engine with contra-rotating upstream and downstream non-ducted propellers (12, 14) including a power turbine which is mounted axially between the two propellers (12, 14) and which includes an outer roto...  
WO/2011/035257A1
An exemplary adiabatic calcium looping system includes a first fixed-bed reactor having a fixed sorbent bed holding a calcium-based sorbent, and a second fixed-bed reactor having a fixed sorbent bed holding a calcium-based sorbent. The e...  
WO/2011/031983A2
A method for improving interpenetration, mixing, and combustion between a fuel and oxidizer reactant mixture and combustion product gases in engines having a combustor includes the step of providing an engine having a combustor in which ...  
WO/2011/031983A3
A method for improving interpenetration, mixing, and combustion between a fuel and oxidizer reactant mixture and combustion product gases in engines having a combustor includes the step of providing an engine having a combustor in which ...  
WO/2011/029128A1
A turbine apparatus (20) is disclosed which comprises a container (27) for storing a solid fuel (21), a compressor (42) for compressing air, and a combustion chamber (26) for combusting the fuel (21) in the presence of compressed air fro...  
WO/2011/026732A1
The invention relates to a gas turbine group substantially made of a compressor unit consisting of at least one compressor (1), of at least one generator (5), of at least one combustion chamber (2), and of at least one turbine (3) has at...  
WO/2011/026636A3
The invention relates to a method for operating a micro gas turbine arrangement as well as to a micro gas turbine arrangement for converting biomass into energy according to the preamble of claims 1 and 9. In order to further increase ef...  
WO/2011/026982A1
The method for switching over a gas turbine burner operation from liquid fuel (21) to gas fuel (22, 23) and vice-versa, with the burner (1) comprising nozzles (6) for feeding a premixed gas fuel, nozzles (8) for injecting a pilot gas fue...  
WO/2011/020768A1
The invention relates in particular to a method for converting thermal energy from carbonaceous raw materials into mechanical work, having at least one first (4) and one second (6) device for storing and releasing thermal energy connecte...  
WO/2011/020767A1
The invention relates in particular to a method for converting thermal energy from carbonaceous raw materials into mechanical work, having at least one first (4) and one second (6) device for storing and releasing thermal energy connecte...  
WO/2011/020695A1
The gas turbine (1) comprises a compressor (2) that compresses an oxidiser containing flow and supplies it to at least a combustion chamber (3, 7), wherein a fuel is injected and a mixture formed; the mixture is then combusted generating...  
WO/2011/016945A3
Secondary air flow is provided for a ducted fan having an engine core driving a fan blisk. The fan blisk incorporates a set of thrust fan blades extending from an outer hub and a set of integral secondary flow blades extending intermedia...  
WO/2011/008576A3
A combined cycle power generation system (10) includes a steam turbine (14, 16, 18), a combustion system (12) including a compressor (24), a combustion chamber (26), a gas turbine (28), and a HRSG (20) to generate steam with energy from ...  
WO/2011/007303A4
A system and method for enhancing the performance of a gas turbine engine or a diesel engine, the system comprising: an air control valve (32) for diverting a portion of compressed air from the air compressor section; a monitoring and co...  
WO/2011/007303A1
A system and method for enhancing the performance of a gas turbine engine or a diesel engine, the system comprising: an air control valve (32) for diverting a portion of compressed air from the air compressor section; a monitoring and co...  
WO/2011/005858A3
Systems, apparatuses and methods ("utilities") for use in "internally" cooling the compressor of a gas turbine engine so as to approximate isothermal compression and thereby increase the power and/or efficiency of the engine. In one arra...  
WO/2011/005858A2
Systems, apparatuses and methods ("utilities") for use in "internally" cooling the compressor of a gas turbine engine so as to approximate isothermal compression and thereby increase the power and/or efficiency of the engine. In one arra...  
WO/2011/001311A3
A new gas turbine-fuel cell Hybrid Cycle is proposed. The fuel cell advantageously operates close or under atmospheric pressure and is fully integrated with the gas turbine that is based on an Inverted Brayton-Joule Cycle. The idea of th...  
WO/2011/000548A3
The invention relates to a method for operating a power plant using a gas turbine system (1), comprising at least one compressor section (2), a combustion chamber (3), and at least one turbine (4), wherein the gas fed to the combustion c...  
WO/2010/142573A3
The invention relates to a device (8) for damping the noise in a flow channel (5) of a gas turbine. The device is characterized by supply elements (18, 19, 21) for supplying the recirculated exhaust gases (14) to the intake air flow (16)...  

Matches 701 - 750 out of 8,405