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WO/2016/098156A1 |
This gas turbine power generation system 100 includes: a two-shaft gas turbine 1; a power generator 2 that is driven by the two-shaft gas turbine 1 and that generates power; an electric motor 3 that is driven by power generated by the po...
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WO/2016/098220A1 |
The gas turbine power generation system of the present invention repeats either the supply or absorption of power, in addition to generating power. The gas turbine power generation system is provided with a first rotation shaft, a compre...
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WO/2016/098266A1 |
A gas turbine power generation system having an improved function to stabilize the power system is disclosed. The gas turbine power generation system has a dual-shaft gas turbine, an electric generator mechanically connected to a low pre...
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WO/2016/091604A1 |
The method allows to control a test apparatus for a gas turbine engine; WI values of one or more tentative fuel gas mixtures are predicted by calculations and the predicted WI values are used for setting the composition of a fuel gas mix...
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WO/2016/079223A1 |
The invention relates to a thermal energy machine (1), in particular a gas turbine (2), comprising a compressor (3) for compressing an air mass flow (5) flowing along the machine longitudinal central axis (6) in an axial flow direction (...
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WO/2016/064785A1 |
A co-generation process for a regenerator in an FCC system having a reactor and a regenerator includes the steps of introducing flue gas from the regenerator into a heating unit at a first location of the heating unit, and introducing an...
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WO/2016/057112A1 |
A centrifugal compressor diffuser (42) includes a plurality of diffuser flow passages (22) extending through an annular diffuser housing (20) and circumferentially bounded by diffuser vanes (23) and axially bounded by forward and aft wal...
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WO/2016/056180A1 |
A fuel injecting device (36) for a combustor (12) has a pilot burner (40) and a main burner (4). The main burner (4) has at least one first fuel injection port (41a) to supply a first fuel to an upstream section of a combustion chamber (...
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WO/2016/056580A1 |
Provided is a turbine stator blade cooling structure that can suppress the use of compressed air. Also provided is a gas turbine engine that is provided with the turbine stator blade cooling structure. A turbine blade cooling structure t...
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WO/2016/056579A1 |
Provided is a combustor that has an efficient cooling structure. Also provided is a gas turbine engine that is provided with the combustor. A combustor that is for a gas turbine and that is provided with a combustion cylinder and with a ...
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WO/2016/055278A1 |
A (micro) gas turbine arrangement has a gas turbine device (12) with a combustion chamber system (28), a turbine (30) driven by an exhaust gas stream (32) from the combustion chamber system, and a compressor (22) for supplying the combus...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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). ...
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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...
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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...
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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 ...
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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...
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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...
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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...
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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-...
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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...
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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...
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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 (2...
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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 ...
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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) ...
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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...
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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 ...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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