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Matches 151 - 200 out of 8,618

Document Document Title
WO/2016/128925A1
The present invention relates to a radial centrifugal turbomachine provided with an adjusting device (25) operatively active at the axial inlet (12) of the fixed casing (6) of the turbomachine (1 ). The adjusting device (25) comprises an...  
WO/2016/129030A1
A gas turbine system (1) is equipped with: a two-shaft gas turbine (2) having a gas turbine compressor (10) that takes in and compresses air (A), a combustor (11) that mixes and burns compressed air (CA) generated by the gas turbine comp...  
WO/2016/126980A1
A system includes a turbine combustor having a first volume (76) configured to receive a combustion fluid and to direct the combustion fluid into a combustion chamber (60) and a second volume (92) configured to receive a first flow of an...  
WO/2016/126873A1
A gas turbine system includes a turbine combustor, a turbine, an exhaust gas compressor, an exhaust gas recirculation (EGR) system, a carbon black recovery system, and a carbon black production controller. The carbon black production con...  
WO/2016/126985A1
A system includes a turbine combustor having a first volume (76) configured to receive a combustion fluid and to direct the combustion fluid into a combustion chamber. The turbine combustor includes a second volume (92) configured to rec...  
WO/2016/127187A3
A process for retrofitting an electric power plant that uses two 60 Hertz large frame heavy duty industrial gas turbine engines to drive electric generators and produce electricity, where each of the two industrial engines can produce up...  
WO/2016/113489A1
The invention relates to a device for controlling an auxiliary engine (8) including a gas generator and a free turbine suitable for being connected mechanically to the rotor (12) of a helicopter in order to supply same with thrust power,...  
WO/2016/108477A1
Provided are a high-voltage application-type combustor and a method for applying an electric field by means of the same combustor, the high-voltage application-type combustor comprising: a premix chamber (410) arranged on an upper end of...  
WO/2016/109730A1
A system includes an exhaust gas recirculation (EGR) gas turbine system which includes a combustor configured to receive and combust a fuel with an oxidant and a turbine driven by combustion products from the combustor and a turbine driv...  
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...  
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...  
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...  
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...  
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 (...  
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...  
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...  
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 (...  
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...  
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 ...  
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...  
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...  

Matches 151 - 200 out of 8,618