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Matches 101 - 150 out of 8,405

Document Document Title
WO/2016/051758A1
A gas turbine (100) according to the present invention uses hydrogen gas as a fuel, has a fuel injection nozzle (23), and is provided with: a combustor (20), at the interior of which a combustion chamber (24) is formed; a water-vapor sup...  
WO/2016/050006A1
A compression-expansion counter-rotating impeller mechanism, comprising a rotating shaft A and a rotating shaft B alternately disposed in an axial direction; the rotating shaft A is provided with a movable compression vane (3) and a mova...  
WO/2016/046073A1
The invention is directed to an apparatus for expanding a compressed combustion gas comprising a combustor, a turbine rotor and a diffusor. The combustor is comprised of an axially extending space around an axially extending combustor ax...  
WO/2016/037452A1
Disclosed is a counter-rotation impeller mechanism, comprising at least one positive rotating shaft (1) and at least one negative rotating shaft (2), wherein the difference between the numbers of the positive rotating shaft (1) and the n...  
WO/2016/040108A1
The present disclosure relates to systems and methods that provide a low pressure liquid CO2 stream. In particular, the present disclosure provides systems and methods wherein a high pressure CO2 stream, such as a recycle CO2 stream from...  
WO/2016/035297A1
Provided is gas turbine equipment with which it is possible to suppress a decrease in efficiency, deterioration of instruments, damage to instruments, and so forth. Gas turbine equipment according to an embodiment has a combustor, a turb...  
WO/2016/031821A1
This compressed fluid storage power generation device (10) is provided with: a compressor (11) having an electric motor (34) and compressor bodies (22, 24) for compressing a working fluid by being driven by the electric motor (34); a pre...  
WO/2016/029184A9
The present disclosure relates to a power generation system (100), and a related method of power generation, that use closed supercritical fluid cycles (106), and in particular, to a power generation system and related methods where mult...  
WO/2016/029184A1
The present disclosure relates to a power generation system (100), and a related method of power generation, that use closed supercritical fluid cycles (106), and in particular, to a power generation system and related methods where mult...  
WO/2016/023987A1
The invention relates to a method for operating a power plant (1) comprising a gas turbine (2) and an emergency fuel system (11). In a normal operating state, gas (5) is supplied from a supply line (3) to the combustion process (4) of th...  
WO/2016/024447A1
Provided is an integrated coal gasification combined cycle power generation facility (1) equipped with: a gasification furnace (20) that generates combustible gas from pulverized coal; a gas cooler (30); gas turbine equipment (50); an au...  
WO/2016/020607A1
The quick-assist device applies to a free-turbine turbomachine (11) of an aircraft comprising at least a first free-turbine turbomachine (11) provided with a gas generator, combined with an electric machine (12) that can operate as a sta...  
WO/2016/010999A1
Methods and systems for producing DRI utilizing a petroleum refinery bottoms (i.e. heavy fuel oil, vacuum residue, visbreaker tar, asphalt, etc.) or petroleum coke gasifier and a hot gas cleaner. Cooling of the hot synthesis gas generate...  
WO/2016/007509A1
The present disclosure relates to a system and method that provide power generation using predominantly C02as a working fluid. In particular, the present disclosure provides for the use of a portion of the heat of compression from a C02c...  
WO/2016/003935A1
In one embodiment, a system includes a drive train starter system. The drive train starter system includes a generator mechanically coupled to a drive train of a gas turbine system and an exciter system electrically coupled to the genera...  
WO/2016/003932A1
In a gas turbine system (52) having an exhaust gas recirculation system (54) receiving exhaust from the gas turbine system and recycling the exhaust gas back to the gas turbine system, a blower (580) with variable guide vanes (586) is po...  
WO/2016/003925A1
In an embodiment, a method includes flowing an exhaust gas from a turbine of a gas turbine system to an exhaust gas compressor of the gas turbine system via an exhaust recirculation path; evaluating moist flow parameters of the exhaust g...  
WO/2016/000850A1
The invention relates to a method for operating an integrated power plant with formic acid, comprising several steps. First, formic acid is produced catalytically from a solid fuel at low temperatures in a first reactor. Subsequently, th...  
WO/2015/199693A1
A transition duct system (100) for routing a gas flow from a combustor (102) to the first stage of a turbine section in a combustion turbine engine, wherein the transition duct system includes one or more converging flow joint inserts (1...  
WO/2015/199690A1
A method of operating an axial stage combustion system in a gas turbine engine (12) including an EGR system (14) that extracts a portion of exhaust gas produced by the gas turbine engine (12) to a second axial stage of a combustor (18). ...  
WO/2015/197949A1
The invention relates to a turbojet engine comprising a shaft of a fan (12) driven by a turbine shaft (16) via a device (20) that reduces the rotational speed, characterized in that it comprises an uncoupling means (28) interposed betwee...  
WO/2015/199694A1
A transition duct system (100) for routing a gas flow from a combustor (102) to the first stage (104) of a turbine section (106) in a combustion turbine engine (108), wherein the transition duct system (100) includes one or more convergi...  
WO/2015/195871A1
A turbine apparatus (10) has amain shaft (16), a first set of blades (12) mounted to the main shaft, a second set of blades (14), and a barrel (18) affixed to a periphery of the second set of blades. The barrel (18) is rotatably mounted ...  
WO/2015/191100A1
A power generation plant has two internal combustion engines (ICE) coupled in a compound configuration to operate electrical generators. A first ICE is a piston/cylinder engine producing high temperature and high pressure exhaust. The ex...  
WO/2015/191039A1
A gas turbine engine (10) having a rotor centering cooling system (12) for cooling struts (14) within an exhaust diffuser (16) and turbine case to reduce tip rub during hot restarts is disclosed. In particular, the rotor centering coolin...  
WO/2015/185384A1
A method (100, 200) manages a gas turbine assembly during start up or shut down, the gas turbine assembly (10) including a twin shaft gas turbine (5) comprising an input shaft (13) and an output shaft (21) and a speed sensor (40) for mea...  
WO/2015/181519A1
A combustion engine comprising a radial compressor in flow communication via a flow passage with an annular compressor-combustor array radially outward of the radial compressor. Both the radial compressor and compressor-combustor are co-...  
WO/2015/180935A1
The present invention relates to a method for operating a gas turbine engine unit (10) comprising a gas turbine engine (12, 12a, 12b, 12c) with at least a compressor section (14) and a turbine section (16), wherein the compressor section...  
WO/2015/180540A1
A combustion gas turbine relates to the field of automobile industry. The combustion gas turbine uses a combustion gas turbine technology in which a closed waste-gas circulation and an opened combustion-gas circulation coexist. The combu...  
WO/2015/181938A1
 A gas turbine composite power generation device having a gas turbine (2A), a power generator (3) for generating power through the drive force of a turbine (1), a first control device (20A) for controlling the output of the gas turbine...  
WO/2015/177296A1
The invention relates to a device and a method for treating a gas flow. Combustible components are separated from a first gas flow by means of an absorption process using a liquid medium in an absorption device; the components dissolved ...  
WO/2015/172899A1
The invention relates to a method for operating a burner (16), wherein a fuel (84) and an oxidizing working medium (86) are fed into the burner (16), the fuel (84) and the working medium (86) are introduced into a combustion volume (14) ...  
WO/2015/174246A1
By using a combustion exhaust gas (18) from a power turbine (16), a high-pressure secondary compressed air (12C) is subjected to heat exchange in a first heat exchange unit (19A) of an exhaust heat recovery device (19), and by using resu...  
WO/2015/161972A1
The invention relates to a method for exhaust gas aftertreatment, in which an exhaust gas to be aftertreated, which is produced during a combustion process, is treated with a reducing agent. The invention further relates to a combustion ...  
WO/2015/156889A2
A mid-turbine frame (MTF") for a jet engine is disclosed and comprises a duct that extends between a high pressure turbine ("HPT") and a low pressure turbine ("LPT"), the duct comprising a plurality of segments that together form an oute...  
WO/2015/155142A1
The invention relates to a gas turbine (100) assembly comprising a first shaft (101), a first compressor (102) and a first turbine (103) mounted on the first shaft, a combustor (104) between the first compressor (102) and the first turbi...  
WO/2015/155818A1
This floating liquefied-gas production facility (1) is equipped with: a gas turbine unit (20); a liquefaction facility (90) that has a primary refrigeration compressor (40) driven by the gas turbine unit (20), and cools natural gas; a dr...  
WO/2015/155450A1
The invention concerns a device for assisting a propulsion system of a single-engine helicopter comprising an engine linked to a power transmission unit (15) suitable for rotating a rotor of the helicopter, characterised in that it compr...  
WO/2015/149447A1
Provided is a thermodynamic cycle method and system for a semi-closed constant pressure internal combustion in a prime motor. The cycle process thereof comprises a multi-stage compression interstage cooling process, a counter-flow heat e...  
WO/2015/149448A1
Provided is a method and system for a semi-closed timing constant volume thermodynamic cycle in a prime motor. The cycle thereof comprises 6 processes: a multi-stage compression interstage cooling process, a counter-flow heat exchange pr...  
WO/2015/147938A3
A combustor wall assembly has a heat shield and a supporting shell with a cooling cavity defined therebetween. A grommet generally includes a wall defining a dilution hole isolated from the cooling cavity, and a flange projecting radiall...  
WO/2015/145041A1
The invention relates to a method for detecting a failure of a first turbine engine, referred to as faulty engine (4), of a twin-engine helicopter and for operating a second turbine engine, referred to as sound engine (5), each engine (4...  
WO/2015/145043A1
The invention relates to a turboshaft engine comprising a gas generator (5) designed to be rotated and a free turbine (6) rotated by the gases from the gas generator (5). The turboshaft engine is characterised in that it comprises a devi...  
WO/2015/147974A1
A system, including: a recirculated exhaust gas conditioning loop that routes exhaust gas from a heat recovery steam generator to a turbine compressor inlet, wherein the recirculated exhaust gas conditioning loop includes an exhaust gas ...  
WO/2015/148855A1
An engine, a biomass powder energy conversion and/or generation system, hybrid turbine engines, and methods of manufacturing and using the same are disclosed. The engine includes a housing having an inner wall and an outer wall, a centra...  
WO/2015/147938A2
A combustor wall assembly has a heat shield and a supporting shell with a cooling cavity defined therebetween. A grommet generally includes a wall defining a dilution hole isolated from the cooling cavity, and a flange projecting radiall...  
WO/2015/145077A1
Assistance device (100) for a free turbine turbomachine (TAG1) of an aircraft comprising at least two free turbine turbomachines (TAG1, TAG2), the device comprising an electric starter machine (D1) for providing prolonged assistance to t...  
WO/2015/146170A1
[Problem] To control the temperature of dehydrogenation to an appropriate range to enable efficient and stable hydrogen generation when exhaust gas of power generation is used as a heat source for the dehydrogenation. [Solution] A hydrog...  
WO/2015/145076A1
Assistance device (100) for an aircraft free turbine turbomachine (TAG1), the device comprising means (K11, CVS1) for electrically powering a coil (SU) of a rotary starter machine (GD1), referred to as first coil, in order to provide a f...  
WO/2015/145045A1
The invention relates to a turboshaft engine comprising a gas generator (5) designed to be rotated and a free turbine (6) rotated by the gases from the gas generator. The turboshaft engine is characterised in that it comprises a device (...  

Matches 101 - 150 out of 8,405