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WO/2014/124291A1 |
A turbocharger for use with an internal combustion engine is provided. The turbocharger comprises a differential device (204) having a carrier portion (226), a compressor portion (212), and a turbine portion (210). The compressor portion...
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WO/2014/116626A2 |
A turbine exhaust casing having an outer casing, an inner casing, an annular exhaust gas path defined between outer and inner flow path walls, and a turbine exhaust casing cavity located radially outward and radially inward from the gas ...
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WO/2014/116185A1 |
An offshore facility (100) comprising a floating platform (102); a metal processing apparatus ( 104) disposed on the floating platform; and a power management module (106) adapted to manage and provide a stable power supply to the metal ...
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WO/2014/111649A1 |
The invention relates to a device for storing and releasing fluids at a near-constant pressure, said fluids including a gas and a liquid, which includes a set of substantially identical tanks (1), said tanks including: a portion (G) cont...
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WO/2014/112210A1 |
A power generation system provided with: a gas turbine (11) having a compressor (21) and a combustor (22); a SOFC (13); a first compressed air supply line (26) that supplies compressed air (A1) compressed by the compressor (21) to the co...
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WO/2014/111485A1 |
The subject of the invention is a device for starting a turbopump (1) of a rocket motor (2) of an aircraft comprising a turbine engine for propelling the aircraft and a rocket motor, which comprises a pneumatic supply of compressed air t...
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WO/2014/105325A1 |
A cryogenic fuel system for an aircraft having a turbine engine with a compressor section and a combustion chamber, including a tank for storing cryogenic fuel, a supply line operably coupling the tank to the combustion chamber and a pum...
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WO/2014/105328A1 |
A system for fluid temperature control and actuation control for an aircraft engine fueled by dual fuels, including a first fuel system having a first fuel tank fluidly coupled to the engine, a second fuel system having a second fuel tan...
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WO/2014/103682A1 |
Provided are exhaust gas processing equipment, which is capable of suitably removing sulfur oxides contained in exhaust gas and capable of increasing device durability, and a gas turbine power generation system using same. An exhaust gas...
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WO/2014/104307A1 |
A power generation system (20A) is provided with: a medium circulation circuit (22) for circulating a medium; a circulation pump (23); an evaporator (25) for heating and evaporating the medium by heat energy of a heating medium obtained ...
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WO/2014/102407A1 |
The invention relates to a hybrid plant with a combined solar-gas cycle, and an operating method with two circuits, one air circuit and one steam circuit, the air circuit having a gas turbine with a cooling exchanger with a natural gas s...
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WO/2014/104969A1 |
A method for producing energy including: producing fuel gases from biomass raw material in a main receptacle unit (8), feeding produced fuel gas to a consumer unit (2,3), transferring energy from the consumer unit to at least one energy ...
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WO/2014/096604A1 |
A centrifugal gas compressor or pump comprising a body (211), a wheel (212) rotatably mounted within the body (211) around a wheel axis (A), the wheel (212) comprising a hub (2120), a set of blades (2121) fastened to the hub (2120), the ...
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WO/2014/098524A1 |
According to one specific embodiment of the present invention, disclosed is a circulating fluidized bed gasifier which is capable of increasing a combustion region and providing an improved carbon conversion rate with a heat exchanger in...
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WO/2014/098962A1 |
A method of configuring a plurality of gas turbine engines includes the steps of configuring each of the engines with respective ones of a plurality of propulsors. Each propulsor includes a propulsor turbine and one of a fan and a propel...
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WO/2014/100164A1 |
A vane carrier temperature control system for use in a gas turbine engine includes a first cooling air source, a second cooling air source, and an air temperature control system. The first cooling air source supplies a first portion of v...
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WO/2014/081492A2 |
A combustor liner which reduces cooling flow to a combustion chamber and augments pressure drop split between impingement holes and effusion holes is disclosed. The combustor liner may further include accelerating channels, trip strips, ...
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WO/2014/080758A1 |
The present invention resolves trouble caused by a difference in the temperature of different types of fuel gas. A power generation system (10) for using exhaust fuel gas (L3) emitted from an SOFC (13) as the fuel for the combustor of a ...
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WO/2014/079466A1 |
The invention concerns a power turbine unit (2) comprising a turbine housing (17a, 17b), an exhaust duct (18), a turbine wheel (6) with blades positioned in said exhaust duct (18), a shaft (16) rigidly connected to said turbine wheel (6)...
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WO/2014/080848A1 |
A power generation system and an operation method for the power generation system, that have: a gas turbine (11) having a compressor (21) and a combustor (22); a fuel cell (13); a discharged fuel gas supply line (45) that supplies discha...
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WO/2014/077156A1 |
The invention addresses the problem of providing a power generation system capable of effectively using the heat of the exhaust air discharged from an SOFC and also providing a method for operating the power generation system. The power ...
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WO/2014/008117A9 |
A turbine wheel (10) for a turbocharger includes a hub (12) extending in an axial direction between a nose (14) and a back-wall (22). The hub (12) defines an axis of rotation (28) extending in the axial direction and the back-wall (22) i...
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WO/2014/072615A1 |
The invention relates to an aircraft propelled by a turbojet engine (10) with contrarotating fans, the turbojet engine being incorporated into the rear of a fuselage (2) of the aircraft in the continuation thereof and comprising two gas ...
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WO/2014/073975A1 |
The present invention provides a modified Organic Rankine Cycle (ORC) process, for reducing or preventing pump cavitation, wherein an ORC working medium flow is pressurized in a pump, heated in a heat exchanger by the use of a waste heat...
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WO/2014/072619A1 |
The invention relates to a method and to a device for determining, in real time, the flow rate of air collected from an aircraft engine (39) by a system (1) for collecting air from the engine, comprising: acquisition means (33) for acqui...
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WO/2014/073059A1 |
The purpose of the present invention is to provide gas turbine power generation equipment capable of suppressing missteps when an instantaneous voltage drop or other grid accident has occurred, in a local grid having naturally fluctuatin...
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WO/2014/071118A1 |
A system includes a turbine having an exhaust flow path through a plurality of turbine stages, wherein the plurality of turbine stages is driven by combustion products flowing through the exhaust flow path, at least one main combustor di...
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WO/2014/071215A1 |
A system is provided with a turbine combustor having a first diffusion fuel nozzle, wherein the first diffusion fuel nozzle is configured to produce a diffusion flame. The system includes a turbine driven by combustion products from the ...
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WO/2014/071063A1 |
A system includes a turbine combustor (150) that includes a head end portion (166) having a head end chamber, a combustion portion (168) having a combustion chamber disposed downstream from the head end chamber, a cap (331) disposed betw...
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WO/2014/069409A1 |
This power generation system is provided with: a gas turbine (11) having a compressor (21), a combustor (22) and a turbine (23); a first compressed air supply line (26) that supplies compressed air, which has been compressed by the compr...
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WO/2014/065185A1 |
A power generation system having a gas turbine engine that utilizes sunlight is provided with: a compressor (1) for compressing air (A), which is the working medium; a solar heater (3) for heating the air compressed by the compressor usi...
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WO/2014/066515A1 |
A unshrouded vane assembly for an unducted propulsion system includes a plurality of vanes which have non-uniform characteristics configured to generate a desired vane exit swirl angle.
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WO/2014/066503A1 |
An unducted thrust producing system has a rotating element with an axis of rotation and a stationary element. The rotating element includes a plurality of blades each having a blade root proximal to the axis, a blade tip remote from the ...
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WO/2014/021971A9 |
A method of heating a gas by directing X-rays at a mass of hafnium 178 to induce gamma rays. The gamma rays are directed at a heat exchanging apparatus, resulting in a stream of heated gas. This process powers a Hafnium gas turbine engin...
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WO/2014/060961A1 |
The present invention relates to a device for generating electric current comprising a turbine wheel (1), a rotor, a stator mounted around the rotor with facilities for connection to an electrical network, a housing which comprises two c...
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WO/2014/059000A1 |
An engine monitor includes a first tuned modeling unit, a second tuned modeling unit and a monitoring unit. The first tuned modeling unit models dynamics of a first engine by processing first control data with a first engine model to pro...
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WO/2014/056574A1 |
The invention relates to an adjustable stator for an exhaust gas guiding section of a turbine, comprising a contour ring (5) and a bearing ring (4) that are arranged at a spacing from each other in axial direction so as to form an inflow...
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WO/2014/055307A1 |
An apparatus performs a power cycle involving expansion of compressed air utilizing high pressure (HP) and low pressure (LP) air turbines located upstream of a gas turbine. The power cycle involves heating of the compressed air prior to ...
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WO/2014/053421A1 |
The turboexpander and driven turbomachine system comprises: a turboexpander (13) configured for expanding a first fluid and comprising an expander stage with one ex- pander impeller; a first set of moveable inlet guide vanes (23) at the ...
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WO/2014/053662A1 |
An energy storage system is described comprising a closed gas circuit which comprises an expansion chamber 2, a compression chamber 3 coupled to the expansion chamber, a compressor for compressing gas from the expansion chamber as it is ...
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WO/2014/053587A1 |
The invention relates to a process for producing hydrogen and generating power comprising the following steps: (a) subjecting a gaseous hydrocarbon feedstock to an endothermic steam reforming reaction by contacting the hydrocarbon feedst...
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WO/2014/052927A1 |
The present disclosure provides pumped thermal energy storage systems that can be used to store electrical energy. A pumped thermal energy storage system of the present disclosure can store energy by operating as a heat pump or refrigera...
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WO/2014/051661A1 |
An example turbomachine control system includes a Full Authority Digital Electronic Controller and an actuator. The actuator is configured to adjust an effector in response to a command signal communicated from the Full Authority Digital...
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WO/2014/050163A1 |
This gas turbine cooling system (30) is equipped with: a cooler (31) that produces cooling air by cooling compressed air extracted from an air compressor (11); a cooling air compressor (34) that supplies the cooling air to a combustion t...
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WO/2014/044425A1 |
The invention relates to a method for the operation of a gas power plant (1), and to a gas power plant (1) of this type, comprising a gas turbine (10), which is connected to a generator (14) that can also be operated as a motor and which...
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WO/2014/041013A1 |
The invention relates to a method for monitoring at least one exhaust gas turbocharger (ATL) of a large internal combustion engine (BKM), comprising at least one compressor (1a) and one exhaust gas turbine (1b) arranged on the same shaft...
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WO/2014/039288A1 |
A shell air recirculation system for use in a gas turbine engine includes one or more outlet ports located at a bottom wall section of an engine casing wall and one or more inlet ports located at a top wall section of the engine casing w...
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WO/2014/039315A1 |
During full load operation of gas turbine engine operation, a valve system is maintained in a closed position to substantially prevent air from passing through a piping system of a shell air recirculation system. Upon initiation of a tur...
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WO/2014/032830A1 |
The present invention relates to the extension of the range of functions of a so-called IGCC-System (integrated gasification combined cycle system; combined process comprising integrated coal gasification) and a modified IGCC system. By ...
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WO/2014/030011A1 |
A sensor apparatus comprising a housing having an inner perimeter which defines an area through which gas may flow, the housing being provided with a first chamber which extends around the area through which gas may flow, an entrance bei...
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