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Matches 651 - 700 out of 8,616

Document Document Title
WO/2013/009636A2
A gas turbine engine having a compressor section using blades on a rotor to deliver a gas at supersonic conditions to a stator. The stator includes one or more of aerodynamic ducts that have converging and diverging portions for decelera...  
WO/2013/006957A1
A methanol indirect combustion combined-cycle power generation apparatus and method. A liquid methanol input stream is evaporated to provide a gaseous methanol stream which is converted to syngas that is combusted in a gas turbine assemb...  
WO/2013/009636A3
A gas turbine engine having a compressor section using blades on a rotor to deliver a gas at supersonic conditions to a stator. The stator includes one or more of aerodynamic ducts that have converging and diverging portions for decelera...  
WO/2013/001238A1
The invention relates to a housing for the accessory relay of a gas turbine having a front side surface and a rear side surface (14) opposite the front surface, in which a peripheral flange (16) contains the housing, and in which at leas...  
WO/2013/003654A3
Engine systems and associated methods, including systems with semi- isothermal compression devices are disclosed. An engine system in accordance with a particular embodiment includes a compressor having a compressor inlet and outlet, a c...  
WO/2012/172405A1
The present invention relates to a system (1) for capturing C02 from a flue gas deriving from combustion of hydrocarbons which has been generated in a gas turbine (12) wherein the system comprises means for recirculating the flue gas (18...  
WO/2012/172235A1
Turbine engine (10) comprising a low-pressure compressor (12), a high-pressure compressor (14), a low-pressure turbine (20), a high-pressure turbine (18) and regulating means (30) for regulating the rotational speed of the low-pressure t...  
WO/2012/171094A1
The present disclosure relates to combustion systems and components for rotary ramjet engines. An injection system, optionally stratified for ease of engine startup, provides an air and fuel mixture to a combustion chamber. An ignition s...  
WO/2012/173651A1
An aircraft engine fuel system 900 is disclosed having a gas turbine engine 101, a turbocharger 910, a compressor bleed air system 930 for providing compressor air (A) from the gas turbine engine 101 to the turbocharger 910, and a fuel d...  
WO/2012/164371A3
In a system and a method for gas turbine flue gas recirculation for recirculating at least a portion of a flue gas generated in a gas turbine of a gas turbine power generation system an oxygen feed unit (18) is arranged to bring a recirc...  
WO/2012/164228A1
The invention relates to a gas turbine engine for propelling an aircraft, comprising: a low‑pressure rotary body (10) having mobile low‑pressure turbine blades (10T), an intermediary rotary body (20) having mobile intermediary turbin...  
WO/2012/165968A1
System and method for treating cargo vapors from crude oil and petroleum products tanks (2) to generate electrical power. The system and method comprising the steps: separating the cargo vapors into liquid volatile organic compounds (LVO...  
WO/2012/164371A2
In a system and a method for gas turbine flue gas recirculation for recirculating at least a portion of a flue gas generated in gas turbine of a gas turbine power generation system an oxygen feed unit (18) is arranged to bring a recircul...  
WO/2012/161711A1
Described herein are gradual oxidation systems that receive and process solid, liquid, or gaseous fuels. The system can include a solid fuel gasifier that extracts and cleans gas fuel from a solid fuel. The system can also include a reac...  
WO/2012/155314A1
A hybrid power generation system and method based on classification of solid fuel pyrolysis and semi-coke combustion are provided. The system comprises a pyrolysis device (1) for pyrolysing solid fuel to produce gas, liquid and solid sem...  
WO/2012/156597A1
The invention relates to a turbine engine including a detonation chamber and an aircraft provided with such a turbine engine. The chamber (4) of the turbine engine (1) comprises a continuous detonation wave engine (6) provided with an an...  
WO/2012/152447A1
The invention is directed to a turbo-engine, particularly internal combustion engine, comprising a housing and therein a bladeless turbine section (30; 42; 67) of the stacked disc- or Tesla-type construction, wherein the turbine section ...  
WO/2012/151606A1
A hot-air engine (10) includes a compressor (12), a heating chamber (14), a rotary displacement type working engine (16) and a drive means (22). The compressor (12) has an inlet (12a) and an outlet (12b). The heating chamber (14) has an ...  
WO/2012/151625A1
An integrated drying gasification system comprises a gasifier for gasifying carbonaceous fuel to produce hot product gas and an entrained flow dryer which receives the hot product gas to dry the carbonaceous fuel prior to gasification. A...  
WO/2012/148172A2
Disclosed is a system for producing syngas and reducing tar using air/steam on a fluidized bed, which includes a gasifier (10) in which a solid fuel is gasified to produce a combustible syngas; a first loop seal (20) connected to the gas...  
WO/2012/148172A3
Disclosed is a system for producing syngas and reducing tar using air/steam on a fluidized bed, which includes a gasifier (10) in which a solid fuel is gasified to produce a combustible syngas; a first loop seal (20) connected to the gas...  
WO/2012/147752A1
This system is provided with: a fluidized bed drying device (102) in which fluidized gas (107) is fed to a drying chamber to thereby fluidize and dry low-grade coal fed to the drying chamber; a raw-coal fluidized bed bunker (50) for temp...  
WO/2012/146399A1
The invention relates to a method (1) and a device (1) for generating electricity from waste gases (3) containing hydrogen sulfide, in particular from the natural gas industry (2). The method according to the invention is characterized i...  
WO/2012/142124A2
Crosslinked hydrogel-based transdermal pharmaceutical formulations. The hydrogel transdermal formulations. Transdermal patches are useful for administering a variety of drugs to patients. The transdermal patches here employ crosslinked-h...  
WO/2012/138447A1
A burner assembly for combusting fuel in a combustion zone to reduce NOx emissions includes a water spray subassembly including a water outlet configured to direct water at an angle with respect to an axis of the burner assembly, the wat...  
WO/2012/132062A1
Disclosed is a method for operating a gas compressor which compresses a gas fuel, a supply condition of which fluctuates, and is provided with a suction flow rate adjustment mechanism, wherein the limit pressure ratio that defines the op...  
WO/2012/131051A3
In order to convert solid fuels into electrical energy by means of allothermal gasification with approximately the same efficiency as is possible for combustible gases suitable for gas turbines, according to the invention at least part o...  
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...  

Matches 651 - 700 out of 8,616