A system includes a hydrogen gas production system and a power generation system. The hydrogen gas production system includes a heated gas supply line configured for flow of a heated gas, a hydrocarbon supply line, a catalytic pyrolysis reactor configured to be in thermal contact with the heated gas of the heated gas supply line and produce a hydrogen containing gas by pyrolyzing a hydrocarbon introduced therein via the hydrocarbon supply line, and a separator configured to extract a hydrogen gas from the hydrogen containing gas discharged from the catalytic pyrolysis reactor. The power generation system includes a heated gas collection line configured to collect the heated gas after the thermal contact with the catalytic pyrolysis reactor and supply the heated gas to the power generation system, and a gas turbine having a combustor configured to bum the hydrogen gas introduced therein from the separator via a hydrogen supply line.
F02C 3/22 - Ensembles fonctionnels de turbines à gaz caractérisés par l'utilisation de produits de combustion comme fluide de travail utilisant un combustible, un oxydant ou un fluide de dilution particulier pour produire les produits de combustion le combustible ou l'oxydant étant gazeux aux température et pression normales
C01B 3/02 - Production d'hydrogène ou de mélanges gazeux contenant de l'hydrogène
F01K 23/02 - Ensembles fonctionnels caractérisés par plus d'une machine motrice fournissant de l'énergie à l'extérieur de l'ensemble, ces machines motrices étant entraînées par des fluides différents les cycles de ces machines motrices étant couplés thermiquement
F02C 6/00 - Ensembles fonctionnels multiples de turbines à gazCombinaisons d'ensembles fonctionnels de turbines à gaz avec d'autres appareilsAdaptations d'ensembles fonctionnels de turbines à gaz à des applications particulières
F02C 7/22 - Systèmes d'alimentation en combustible
This production system for magnesium chloride comprises: a first removal unit for lowering the concentration of sulfate ions in water to be treated, which contains sea water as a raw material; a second removal unit for lowering the concentration of sodium ions in the water to be treated, which has been discharged from the first removal unit and has a lowered sulfate ion concentration; an OARO separation unit which supplies the water to be treated at the same concentration to both sides of a semipermeable membrane, and separates the water to be treated, which has been discharged from the second removal unit and has a lowered sodium ion concentration, into concentrated water and low concentration water; and a concentration unit for further concentrating the concentrated water discharged from the OARO separation unit so as to produce a slurry in which magnesium chloride is crystallized.
Provided is a furnace facility capable of adjusting the flow rate of combustion air. A furnace body (110) forms a furnace space (S0) inside, and a floor (140) partitions the furnace space (S0) into an upper space (S1) and a lower space (S2) in the vertical direction, and has a communication part (141) communicating the upper space (S1) and the lower space (S2). The upper space (S1) is a space in which to-be-carbonized matter (W) is stored and carbonized, and the lower space (S2) is a space to which combustion exhaust gas generated by the carbonization of the to-be-carbonized matter (W) is guided from the upper space (S1) via the communication part (141). The furnace body (110) has an intake opening (122a) that communicates the upper space (S1) and the outside of the furnace body (110). A chimney (150) forms an exhaust flow path (P1) that communicates the lower space (S2) and the outside of the furnace body (110). A fan (161) is provided in the exhaust flow path (P1) and discharges a gas containing the combustion exhaust gas from the exhaust flow path (P1) to the outside of the furnace body (110).
C10B 49/02 - Distillation destructive des matières carbonées solides par chauffage direct au moyen d'agents porteurs de chaleur, y compris la combustion partielle de la matière à traiter avec des gaz ou des vapeurs à haute température, p. ex. les gaz chauds obtenus par la combustion partielle de la charge
This turbine blade comprises a blade wall, and an insert inserted into a space formed inside the blade wall. An internal cavity communicating with the outside of the turbine blade is formed inside the insert body part of the insert. A plurality of ridges protruding toward the inner surface of the blade wall and having an opposing surface facing the inner surface of the blade wall are formed on the outer surface of the insert body part. Each of the plurality of ridges has a flow passage communicating with the internal cavity, and a plurality of cooling holes communicating with the flow passage, opening on the opposing surface, and arranged along the longitudinal direction of the plurality of ridges. A recovery space is defined between adjacent two ridges out of the plurality of ridges. Between the outer surface of the insert body part and the inner surface of the blade wall, and between the hub-side edge of the blade wall and the hub-side end of the ridges in the longitudinal direction or between the tip-side edge of the blade wall and the tip-side end of the ridges, a recovery flow path communicating with the recovery space is defined. A discharge hole for communicating the recovery flow path with the outside of the turbine blade is formed in the blade wall.
An operation management method for a dust collection device according to at least one embodiment of the present disclosure is provided with: a step for acquiring a temperature difference between a temperature of a surface on one side and a temperature of a surface on the other side in the thickness direction of a pipe plate; and a step for evaluating, on the basis of the temperature difference acquired in the step for acquiring the temperature difference, the risk of damage to a porous filter due to deformation of the pipe plate caused by the temperature difference.
The purpose of the present invention is to achieve an operation state suitable for all load bands by supplying air at a flow rate sufficient to cool an unused burner and protecting a burner apparatus in a high-load zone, and setting an appropriate air flow rate in response to a decrease in heat load of a furnace in a low-load zone. This boiler system (2) comprises a boiler (10) having a plurality of burners (21), an air supply unit for supplying air to the burners (21), a cold gas damper (30d) for adjusting the amount of air supplied to the burners (21) by the air supply unit, and a control unit for controlling the cold gas damper (30d) so as to supply cooling air in an amount corresponding to the load of the boiler (10) when cooling air is supplied by the air supply unit to burners (21) that are not forming flames.
An inspection assistance system according to the present invention identifies the shape of an inspection object on the basis of a two-dimensional real image obtained as a result of the inspection object being imaged by an imaging device. A two-dimensional simulated image corresponding to the two-dimensional real image is extracted from a three-dimensional CAD model on the basis of the identified shape. A projection range designated from the two-dimensional real image is projected onto the three-dimensional CAD model by being adapted to the two-dimensional simulated image.
A control system for controlling each of a plurality of control objects by means of a physical machine having a plurality of virtual machines comprises: a first virtual machine that is at least one from among a plurality of virtual machines, the first virtual machine having a first communication unit that communicates with each of the plurality of control objects, receives data used in controlling the control objects, and transmits a control instruction to the control objects, and having a distribution unit that distributes the data received from the control objects to another virtual machine; and a second virtual machine that is different from the first virtual machine from among the plurality of virtual machines, the second virtual machine having a computation processing unit that issues a control instruction to the control objects on the basis of an analysis result obtained by analyzing the data.
G06F 9/50 - Allocation de ressources, p. ex. de l'unité centrale de traitement [UCT]
G05B 19/042 - Commande à programme autre que la commande numérique, c.-à-d. dans des automatismes à séquence ou dans des automates à logique utilisant des processeurs numériques
G06F 9/455 - ÉmulationInterprétationSimulation de logiciel, p. ex. virtualisation ou émulation des moteurs d’exécution d’applications ou de systèmes d’exploitation
G06F 13/10 - Commande par programme pour dispositifs périphériques
Provided are: a machining implement having a simple configuration with which a polishing surface can be caused to contact a target surface with an even force; and a machining method. The present invention is configured such that: a polishing part (210) and a traction part (220) are provided; the polishing part (210) has a second axis (L2) as the central axis and comprises an outer peripheral surface (211a) fitted with the shape of a valve seat (112a); the outer peripheral surface (211a) includes a polishing surface for polishing the valve seat (112a); and the traction part (220) pulls the central location of the polishing part (210) in the prescribed direction, with the outer peripheral surface (211a) of the polishing part (210) facing the valve seat (112a).
In a fuel supply pipe assembly according to at least one embodiment of the present disclosure, a fuel supply pipe comprises: a first flange portion that can be coupled to a fuel pipe for supplying fuel to the fuel supply pipe; and a second flange portion that can be coupled to a top hat portion. The top hat portion is provided in an end portion on one side in the axial direction of a first cylindrical portion, and includes: a top hat flange portion for attaching the top hat portion to a casing of a gas turbine; and a third flange portion that is provided in an end portion on the other side in the axial direction of a second cylindrical portion and that can be coupled to the second flange portion. The first flange portion is positioned between the top hat flange portion and the third flange portion, in the axial direction, when the second flange portion is coupled to the third flange portion.
This softened structure detection method for detecting a softened structure in an inspection object of a weld metal by using ultrasonic flaw detection comprises: a first flaw detection step for performing ultrasonic flaw detection of causing a first ultrasonic beam to enter into an inspection object along an inclination direction from at least one oblique angle probe to thereby acquire a reflection wave of the first ultrasonic beam returning to the oblique angle probe; a second flaw detection step for performing ultrasonic flaw detection of causing a second ultrasonic beam to enter into the inspection object along the inclination direction from a transmission-side probe to thereby acquire a reflected wave of the second ultrasonic beam received by a reception-side probe disposed opposite to the transmission-side probe across the weld metal; and a determination step for determining the presence or absence of a softened structure in the inspection object, on the basis of the ultrasonic flaw detection result of the first flaw detection step and the ultrasonic flaw detection result of the second flaw detection step.
The purpose of the present invention is to improve accuracy of estimating the clogging state of a nozzle even when steam is guided to a plurality of spaces. A steam turbine system (20) comprises: a steam pipe (7) through which steam jetted from a well flows; a steam turbine (8) having a nozzle to which the steam flowing through the steam pipe (7) is guided; a first steam pipe (21) that branches from the steam pipe (7) and guides steam to a first steam chamber (S1); a second steam pipe (22) that branches from the steam pipe (7) and guides steam to a second steam chamber (S2) having a smaller capacity than the first steam chamber (S1); a steam chamber communication valve (23) that adjusts the flow rate of the steam flowing through the second steam pipe (22); a flowmeter (18) that detects the flow rate of the steam flowing through the steam pipe (7); a pressure gauge that detects the pressure of the steam guided to the first steam chamber (S1); and a clogging state estimation unit that estimates the clogging state of the nozzle on the basis of the flow rate detected by the flowmeter (18), the pressure detected by the pressure gauge, and the opening degree of the steam chamber communication valve (23).
F03G 4/00 - Dispositifs produisant une puissance mécanique à partir d'énergie géothermique
F01D 21/00 - Arrêt des "machines" ou machines motrices, p. ex. dispositifs d'urgenceDispositifs de régulation, de commande ou de sécurité non prévus ailleurs
F01D 25/00 - Parties constitutives, détails ou accessoires non couverts dans les autres groupes ou d'un intérêt non traité dans ces groupes
F01K 21/00 - Ensembles fonctionnels de machines motrices à vapeur non prévus ailleurs
F01K 27/00 - Ensembles fonctionnels transformant la chaleur ou l'énergie d'un fluide en énergie mécanique, non prévus ailleurs
13.
GAS TURBINE CONTROL DEVICE, GAS TURBINE CONTROL METHOD, AND GAS TURBINE MODIFICATION METHOD
This gas turbine control device controls a gas turbine provided with: a combustor capable of mixing and burning a first fuel and a second fuel with combustion air; a bypass passage capable of bypassing at least a part of combustion air to a downstream side space of the combustor and supplying the same; and a bypass valve provided in the bypass passage. The gas turbine control device performs control so as to increase a mixed combustion rate of the second fuel as a load of the gas turbine increases, and controls an opening of the bypass valve on the basis of the mixed combustion rate. The opening control of the bypass valve is performed so as to control the opening of the bypass valve so that the bypass valve is fully closed in a second load smaller than a first load in which the bypass valve is fully closed when the opening is reduced in inverse proportion to the load of the gas turbine.
F02C 9/40 - Commande de l'alimentation en combustible spécialement adaptée à l'utilisation d'un combustible particulier ou de plusieurs combustibles
F02C 7/00 - Caractéristiques, parties constitutives, détails ou accessoires non couverts dans, ou d'un intérêt plus général que, les groupes Entrées d'air pour ensembles fonctionnels de propulsion par réaction
F02C 7/22 - Systèmes d'alimentation en combustible
F02C 7/232 - Soupapes pour combustibleSystèmes ou soupapes de drainage
F23R 3/00 - Chambres de combustion à combustion continue utilisant des combustibles liquides ou gazeux
According to the present invention, a gas turbine comprises: a first fuel injection nozzle which is capable of injecting a first fuel; and a second fuel injection nozzle which is capable of injecting a second fuel and is on a downstream side of the first fuel injection nozzle. The first fuel and the second fuel include hydrogen and fuel other than hydrogen, and are combusted by a combustor of the gas turbine. In a method for operating this gas turbine, when a total hydrogen co-firing ratio corresponding to the total fuel supplied to the combustor is increased to a preset target total hydrogen co-firing ratio value, a second hydrogen co-firing ratio corresponding to the second fuel is controlled to increase while restricting a first hydrogen co-firing ratio corresponding to the first fuel to a first maximum hydrogen co-firing ratio or less, if the total hydrogen co-firing ratio is equal to or greater than a threshold value.
A steam turbine according to one embodiment comprises: an inner casing; a first annular portion which is connected to the inner casing or is formed integrally with the inner casing, defines at least a portion of a steam inlet flow passage, and holds a first sealing device disposed on an outer peripheral surface of a rotor; a plurality of first stage stationary blades which are arranged at intervals in the circumferential direction of the rotor and which include an airfoil portion and an inner shroud positioned radially inward of the airfoil portion; a blade ring which is connected to the inner casing or is formed integrally with the inner casing and which holds at least the plurality of first stage stationary blades; a second annular portion which is attached to the inner shrouds of the plurality of first stage stationary blades; and a second sealing device which is provided between the first annular portion and the second annular portion.
The purpose of the present invention is to improve denitration efficiency. A denitration device (10) comprises: an ammonia injection part (11) that is provided inside a duct (3) through which exhaust gas circulates, and that injects ammonia into the exhaust gas circulating inside the duct (3); a denitration catalyst (13) that is provided on a downstream side of the ammonia injection part (11) inside the duct (3); and a rectification part (20) that is provided on an upstream side of the ammonia injection part (11) inside the duct (3) and spaced a predetermined distance from the ammonia injection part (11) and that rectifies the exhaust gas circulating inside the duct (3).
A sealing device including: a sealing member that is disposed between a rotating member of a rotating machine and a stationary member disposed on the outer side of the rotating member in the radial direction of the rotating member, and that creates a seal between the rotating member and the stationary member; and a biasing member that biases the sealing member toward the radially outer side. The sealing member has a base extending in the circumferential direction of the rotating member, a rib that extends in the circumferential direction and protrudes outward in the radial direction from the base, and a seal fin that extends in the circumferential direction and protrudes inward in the radial direction of the rotating member from the base. The rib has a cut-away part in which the biasing member is disposed between one end and the other end of the rib in the circumferential direction.
Provided is a method for controlling a boiler. The boiler has: a furnace that is composed of a furnace wall having a plurality of heat transfer pipes through which a fluid flows; a combustion device for generating a combustion gas by injecting solid fuel and combustion air into the furnace; and a plurality of soot blowers that inject steam onto the surfaces of the heat transfer pipes, and also are capable of switching between an insertion state, in which the soot blowers are inserted into the furnace, and a pull-out state, in which the soot blowers are pulled out from the furnace. The control method comprises: a temperature detection step (S102) for detecting the temperatures of the plurality of heat transfer pipes by a plurality of temperature detection units; and a control step (S104) for controlling the operation of a predetermined soot blower, on the basis of a plurality of first temperature detection values detected by a plurality of temperature detection sensors in a first period in which the predetermined soot blower starts steam injection in the insertion state.
F23J 3/00 - Enlèvement des résidus solides se trouvant dans les passages ou dans les chambres situés au delà du foyer, p. ex. dans les conduits de fumée par souffleurs de suie
F22B 37/56 - Dispositifs de commande du nettoyage des chaudières, p. ex. pour assurer une durée convenable de la purge de la chaudière
This combustor comprises a plurality of burner groups arranged in a circumferential direction with respect to a combustor axis. Each of the plurality of burner groups has a plurality of burners capable of injecting fuel together with compressed air. Each of the plurality of burners has an air flow passage frame through which air can flow and which can inject air, and a nozzle in which there is formed a fuel injection port through which fuel can be injected into the air flow passage frame. The air flow passage frame has an air inlet that is opened at an upstream-side end, and an air mixture outlet that is opened at a downstream-side end. The air mixture flow passage length, which is the distance in the direction of the combustor axis from the fuel injection port of the nozzle to the air mixture outlet of the air flow passage frame into which fuel is injected from the fuel injection port, is different between the burner groups that are adjacent to each other in the circumferential direction.
F23R 3/28 - Chambres de combustion à combustion continue utilisant des combustibles liquides ou gazeux caractérisées par l'alimentation en combustible
F23R 3/20 - Moyens de stabilisation de la flamme, p. ex. accroche-flamme de postcombustion d'ensembles fonctionnels à propulsion par réaction comprenant des moyens d'injection du combustible
F23R 3/32 - Chambres de combustion à combustion continue utilisant des combustibles liquides ou gazeux caractérisées par l'alimentation en combustible comprenant des dispositifs destinés à prévaporiser le combustible tubulaires
F23R 3/44 - Chambres de combustion comprenant un tube à flamme tubulaire à l'intérieur d'une enveloppe tubulaire
20.
MOISTURE SEPARATION HEATER MODULE AND METHOD FOR INSTALLING MOISTURE SEPARATION HEATER
This moisture separation heater module comprises: a moisture separation heater including a cylindrical body which extends so as to have a longitudinal axis; and an installation structure for supporting the moisture separation heater. The installation structure comprises: a frame; and a support mechanism fixed to an upper part of the frame and having a suspension member. The suspension member suspends and supports the moisture separation heater at at least two different positions in a direction along the longitudinal axis so that the longitudinal axis extends along the horizontal direction.
E04H 9/02 - Bâtiments, groupes de bâtiments ou abris conçus pour résister à des situations extérieures anormales, p. ex. à des bombardements, à des séismes ou à des climats extrêmes, ou pour se protéger de ces situations résistant aux séismes ou à l'effondrement du sol
F22G 3/00 - Surchauffeurs de vapeur caractérisés par des particularités structuralesDétails ou parties constitutives de ces appareils
21.
GAS TURBINE CLEARANCE CONTROL SYSTEM AND CLEARANCE CONTROL METHOD
This gas turbine clearance control system for controlling the clearance between a stationary-side component and a rotation-side component of a turbine comprises: a cooling passage which is formed in the stationary-side component and through which a cooling medium for cooling the stationary-side component circulates; a supply device which supplies the cooling medium to the cooling passage; an adjustment device which adjusts a first flow rate, which is the flow rate of the cooling medium circulating through the cooling passage; and a control device which operates the adjustment device. The control device is provided with: an acquisition unit which acquires a first index corresponding to the discharge temperature of a compressor of the gas turbine; a storage unit in which a function that is a reference for the control device to operate the adjustment device is incorporated; a determination unit which determines a second index, which is an index for an operation by the adjustment device for causing the flow rate of the cooling medium circulating through the cooling passage to be the first flow rate, from the first index on the basis of the function; and a transmission unit which transmits, to the adjustment device, a signal for causing the adjustment device to perform the operation of the second index. The function represents the relationship between the first index and the second index.
A first blade ring part includes a blade ring cooling flow passage for cooling the first blade ring part, a bypass flow passage for bypassing the blade ring part, a stationary blade cooling medium supply flow passage for supplying a cooling medium to a first stage stationary blade, and a plurality of combustor connection parts arranged in the circumferential direction. The stationary blade cooling medium supply flow passage has a first supply pipe for receiving the cooling medium, a first connection pipe for supplying the cooling medium in the circumferential direction, a plurality of stationary blade connection parts connected to the first connection pipe, and a plurality of stationary blade inlet connection pipes for respectively connecting the plurality of stationary blade connection parts and the cooling medium inlets of the plurality of first stage stationary blades. The combustor connection part has an inlet hole for receiving the cooling medium from the blade ring cooling flow passage and/or the bypass flow passage, and a discharge hole for discharging the cooling medium to the cooling flow passage of a combustor.
F02C 6/06 - Ensembles fonctionnels de turbines à gaz délivrant un fluide de travail chauffé ou pressurisé à d'autres appareils, p. ex. sans sortie de puissance mécanique délivrant des gaz comprimés
A hydrogen production device (10) has a reactor (12) that thermally decomposes a hydrocarbon gas, which is a raw material gas, using a catalyst (14), which is metal fine particles, to produce hydrogen, wherein a fluidized bed of the catalyst is formed inside the reactor by introducing the raw material gas from a lower part of the reactor. The catalyst is mixed with a fluidizing agent (17) which is inert particles for enhancing the fluidity of the catalyst.
C01B 3/30 - Production d'hydrogène ou de mélanges gazeux contenant de l'hydrogène par décomposition de composés organiques gazeux ou liquides d'hydrocarbures avec des particules solides mobiles utilisant la technique du lit fluidisé
C01B 3/26 - Production d'hydrogène ou de mélanges gazeux contenant de l'hydrogène par décomposition de composés organiques gazeux ou liquides d'hydrocarbures avec des catalyseurs
A hydrogen production device (10) has a reactor (12) for producing hydrogen by thermally decomposing a hydrocarbon gas, which is a raw material gas, using a catalyst (14), which is fine metal particles, and a fluidized bed of catalyst is formed inside the reactor by introducing raw material gas from the lower part. The reactor is configured to provide an activated catalyst.
C01B 3/30 - Production d'hydrogène ou de mélanges gazeux contenant de l'hydrogène par décomposition de composés organiques gazeux ou liquides d'hydrocarbures avec des particules solides mobiles utilisant la technique du lit fluidisé
B01J 8/24 - Procédés chimiques ou physiques en général, conduits en présence de fluides et de particules solidesAppareillage pour de tels procédés les particules étant fluidisées selon la technique du "lit fluidisé"
C01B 3/26 - Production d'hydrogène ou de mélanges gazeux contenant de l'hydrogène par décomposition de composés organiques gazeux ou liquides d'hydrocarbures avec des catalyseurs
25.
COMBUSTION FACILITY, POWER GENERATION FACILITY, AND METHOD FOR OPERATING COMBUSTION FACILITY
Provided is a boiler in which an ammonia fuel burner (110) has an atomizer (111) that guides ammonia fuel toward a furnace along a second axis (X2) and injects the ammonia fuel from a tip (111a), and the injection amount of ammonia fuel injected from the tip (111a) to one side closer to the center of the furnace than the second axis (X2) is greater than the injection amount of ammonia fuel injected from a plurality of second injection holes (111a2) to the other side closer to the wall surface of the furnace than the second axis (X2).
F23C 5/32 - Disposition des brûleurs pour obtenir des flammes tournantes, c.-à-d. des flammes se déplaçant hélicoïdalement ou en spirale
F23C 1/10 - Appareils à combustion spécialement adaptés à la combustion de plusieurs sortes de combustibles simultanément ou alternativement, au moins un des combustibles étant fluide ou étant un combustible solide en suspension dans l’air du combustible liquide et du combustible pulvérulent
F23D 11/38 - AjutagesDispositifs de nettoyage des ajutages
F23D 17/00 - Brûleurs pour la combustion simultanée ou alternative de combustibles gazeux, liquides ou pulvérulents
F23J 7/00 - Aménagement des dispositifs d'introduction de produits chimiques dans le foyer
26.
PREMIXING DEVICE, BOILER, AND METHOD FOR MODIFYING BOILER
Provided is a premixing device for forming a premixed gas of heated air and ammonia, the premixing device comprising an injection unit configured to inject liquid ammonia into a heated-air flow path, which communicates with a furnace and through which heated air flows.
F22B 31/08 - Installation dans la chaudière d'appareils échangeurs de chaleur ou de moyens de réchauffage de l'air de combustion
F23C 1/10 - Appareils à combustion spécialement adaptés à la combustion de plusieurs sortes de combustibles simultanément ou alternativement, au moins un des combustibles étant fluide ou étant un combustible solide en suspension dans l’air du combustible liquide et du combustible pulvérulent
F23D 11/00 - Brûleurs à pulvérisation directe de gouttelettes de liquide ou de liquide vaporisé dans l'enceinte de combustion
F23D 17/00 - Brûleurs pour la combustion simultanée ou alternative de combustibles gazeux, liquides ou pulvérulents
This boiler comprises: a furnace for burning fuel; an ammonia diffusion burner configured to eject liquid ammonia into the furnace; and an ammonia premix burner configured to inject a premixed gas of gaseous ammonia and air into the furnace.
F23C 1/08 - Appareils à combustion spécialement adaptés à la combustion de plusieurs sortes de combustibles simultanément ou alternativement, au moins un des combustibles étant fluide ou étant un combustible solide en suspension dans l’air du combustible liquide et du combustible gazeux
F23C 1/10 - Appareils à combustion spécialement adaptés à la combustion de plusieurs sortes de combustibles simultanément ou alternativement, au moins un des combustibles étant fluide ou étant un combustible solide en suspension dans l’air du combustible liquide et du combustible pulvérulent
F23C 1/12 - Appareils à combustion spécialement adaptés à la combustion de plusieurs sortes de combustibles simultanément ou alternativement, au moins un des combustibles étant fluide ou étant un combustible solide en suspension dans l’air du combustible gazeux et du combustible pulvérulent
F23D 17/00 - Brûleurs pour la combustion simultanée ou alternative de combustibles gazeux, liquides ou pulvérulents
F23N 1/00 - Régulation de l'alimentation en combustible
28.
GAS TURBINE POWER PLANT, AND METHOD OF OPERATING SAME
This gas turbine power plant comprises: a gas turbine; a gas turbine generator; an air bleed line capable of bleeding a portion of compressed air generated by a compressor of the gas turbine from the gas turbine as bleed air; an auxiliary turbine that is connected to the air bleed line and can be driven by the bleed air flowing through the air bleed line; an air bleed valve provided in the air bleed line; an auxiliary generator capable of generating electricity by being driven by the auxiliary turbine; and a storage battery capable of storing the electricity generated by the auxiliary generator.
F02C 9/52 - Commande de l'alimentation en combustible combinée avec une autre commande de l'ensemble fonctionnel avec la commande du flux du fluide de travail par prélèvement ou bipasse du fluide de travail
F01K 23/00 - Ensembles fonctionnels caractérisés par plus d'une machine motrice fournissant de l'énergie à l'extérieur de l'ensemble, ces machines motrices étant entraînées par des fluides différents
F02C 1/02 - Ensembles fonctionnels de turbines à gaz caractérisés par l'utilisation de gaz chauds ou de gaz sous pression non chauffés, comme fluide de travail le fluide de travail étant un gaz sous pression non chauffé
F02C 6/08 - Ensembles fonctionnels de turbines à gaz délivrant un fluide de travail chauffé ou pressurisé à d'autres appareils, p. ex. sans sortie de puissance mécanique délivrant des gaz comprimés le gaz étant prélevés sur le compresseur de la turbine à gaz
29.
HYDROGEN PRODUCTION DEVICE, HYDROGEN PRODUCTION METHOD, AND HYDROGEN PRODUCTION PROGRAM
A hydrogen production device (10) has a reactor (12) that thermally decomposes a hydrocarbon gas, which is a raw material gas, using a catalyst to produce hydrogen, wherein a fluidized bed of the catalyst is formed inside the reactor by introducing the raw material gas from a lower part of the reactor. The hydrogen production device comprises: a differential pressure sensor (43) configured to detect a pressure difference between an upper part of the reactor away from the fluidized bed and a lower part of the reactor corresponding to the fluidized bed; a supply device (21) configured to newly supply a catalyst to the reactor; an extraction device (31) configured to extract the catalyst with decreased activity from the reactor; and a control device (45) configured to control the operation of the supply device and the extraction device so that the pressure difference detected by the differential pressure sensor becomes constant.
C01B 3/30 - Production d'hydrogène ou de mélanges gazeux contenant de l'hydrogène par décomposition de composés organiques gazeux ou liquides d'hydrocarbures avec des particules solides mobiles utilisant la technique du lit fluidisé
B01J 8/24 - Procédés chimiques ou physiques en général, conduits en présence de fluides et de particules solidesAppareillage pour de tels procédés les particules étant fluidisées selon la technique du "lit fluidisé"
This seal device comprises: a movable seal member disposed in a first gap formed between a stationary member and a rotating member of a rotary machine; a holding member for supporting the movable seal member, which is disposed at a radially inner side, such that the movable seal member is movable along the radial direction; and a plurality of biasing devices that bias the movable seal member radially outward along the radial direction. The holding member or the movable seal member includes a first protrusion protruding toward the other along the radial direction, the other of the holding member and the movable seal member includes a first recess that can be engaged with the first protrusion, and each of the first protrusion and the first recess is disposed between an upper end-side biasing device disposed at an upper end side of the holding member in the circumferential direction and a lower end-side biasing device disposed at a lower end side thereof, and has a side surface extending along the radial direction when viewed from the axial direction, with the side surfaces slidably facing each other.
F01D 11/04 - Prévention ou réduction des pertes internes du fluide énergétique, p. ex. entre étages par obturation non contact, p. ex. du type labyrinthe utilisant un fluide d'obturation, p. ex. de la vapeur
F01D 25/00 - Parties constitutives, détails ou accessoires non couverts dans les autres groupes ou d'un intérêt non traité dans ces groupes
F02C 7/28 - Agencement des dispositifs d'étanchéité
31.
BOILER, POWER GENERATION FACILITY, AND METHOD FOR CONTROLLING BOILER
Provided is a method for controlling a boiler, the boiler including: a solid fuel burner that uses a solid fuel in a furnace to form a flame; a solid fuel adjustment unit that adjusts a supply amount of the solid fuel supplied to the solid fuel burner; an ammonia fuel burner that uses an ammonia fuel in the furnace to form a flame; and an ammonia fuel adjustment unit that adjusts a supply amount of the ammonia fuel supplied to the ammonia fuel burner, said method comprising a control step for controlling the solid fuel adjustment unit and the ammonia fuel adjustment unit, wherein, in the control step (S102), when a load increase operation for increasing the load of the boiler is performed, the ammonia fuel adjustment unit is controlled so as to increase the supply amount of the ammonia fuel supplied to the ammonia fuel burner during an operation period from the start of the load increase operation to the completion thereof.
F23N 1/00 - Régulation de l'alimentation en combustible
F22B 1/18 - Méthodes de production de vapeur caractérisées par le genre de chauffage par exploitation de l'énergie thermique contenue dans une source chaude la source chaude étant un gaz chaud, p. ex. des gaz d'évacuation tels que les gaz d'échappement de moteurs à combustion interne
F22B 35/00 - Systèmes de commande pour chaudières à vapeur
F23C 1/10 - Appareils à combustion spécialement adaptés à la combustion de plusieurs sortes de combustibles simultanément ou alternativement, au moins un des combustibles étant fluide ou étant un combustible solide en suspension dans l’air du combustible liquide et du combustible pulvérulent
F23C 1/12 - Appareils à combustion spécialement adaptés à la combustion de plusieurs sortes de combustibles simultanément ou alternativement, au moins un des combustibles étant fluide ou étant un combustible solide en suspension dans l’air du combustible gazeux et du combustible pulvérulent
F23J 7/00 - Aménagement des dispositifs d'introduction de produits chimiques dans le foyer
Provided is a burner capable of performing stable combustion when premixed combustion and diffusion combustion of ammonia fuel are combined. The burner is provided with: an outer cylinder nozzle that extends along a center axis (CL), and supplies a premixed gas of ammonia fuel and air to the inside of a furnace; a flame holder that holds the flame of the premixed gas; and a plurality of liquid ammonia nozzles (80) that supply liquid ammonia fuel to the inside of the furnace from a position closer to the outer peripheral side than the flame holder. The liquid ammonia fuel jetted from each liquid ammonia nozzle (80) is jetted from an injection position separated from others by 45° or more on a concentric circle (C1) centered on the center axis (CL), in a direction that opens more than 30° toward the center axis (CL) side from a tangential line (L1) direction on the concentric circle (C1) at the injection position.
To provide a burner using liquid ammonia fuel that is capable of achieving stable combustion even when a load of the burner is adjusted. This burner comprises: an outer cylinder nozzle extending along the center axis and supplying ammonia fuel and air into the furnace; a flame holder holding flame formed by the outer cylinder nozzle; a liquid ammonia nozzle supplying the liquid ammonia fuel to the inside of the furnace from a position on the outer peripheral side of the flame holder; and a control unit adjusting the load by adjusting the supply amount of the liquid ammonia supplied from the liquid ammonia nozzle after making the supply amount of the ammonia fuel supplied to the outer cylinder nozzle constant.
F23D 11/24 - Brûleurs à pulvérisation directe de gouttelettes de liquide ou de liquide vaporisé dans l'enceinte de combustion le combustible étant comprimé avant un ajutage d'où il est pulvérisé dans une enceinte du fait d'une réduction appréciable de la pression
F23D 11/26 - Brûleurs à pulvérisation directe de gouttelettes de liquide ou de liquide vaporisé dans l'enceinte de combustion le combustible étant comprimé avant un ajutage d'où il est pulvérisé dans une enceinte du fait d'une réduction appréciable de la pression avec dispositifs permettant de faire varier le régime de pulvérisation du combustible
F23D 17/00 - Brûleurs pour la combustion simultanée ou alternative de combustibles gazeux, liquides ou pulvérulents
Provided is a burner capable not only of mono-fuel combustion, but also co-combustion of biomass and carbon-free fuel, for example. The present invention comprises: an outer cylinder nozzle (62); a flame holder (71) that holds a flame formed by the outer cylinder nozzle (62); an inner cylinder nozzle (61) that extends along a centerline (CL) on the inner peripheral side of the outer cylinder nozzle (62) and opens toward the inside of a furnace (11); and a plurality of ammonia nozzles (80) that can supply ammonia fuel to the inside of the furnace (11) from a position closer to the outer peripheral side than the flame holder (71); swivel vanes (76, 77) provided on the outer periphery of the inner cylinder nozzle (61); and a distributor (78) which is provided between the swirl vanes (76, 77) and the tip of the inner cylinder nozzle (61), distributes a flow passage between the outer cylinder nozzle (62) and the inner cylinder nozzle (61) to an inner peripheral side flow passage (79a) and an outer peripheral side flow passage (79b), and at which the cross-sectional area of the outer peripheral side flow passage (79b) expands toward the tip of the outer cylinder nozzle (62).
F23J 7/00 - Aménagement des dispositifs d'introduction de produits chimiques dans le foyer
F23D 11/24 - Brûleurs à pulvérisation directe de gouttelettes de liquide ou de liquide vaporisé dans l'enceinte de combustion le combustible étant comprimé avant un ajutage d'où il est pulvérisé dans une enceinte du fait d'une réduction appréciable de la pression
F23D 14/02 - Brûleurs à gaz avec prémélangeurs, c.-à-d. dans lesquels le combustible gazeux est mélangé à l'air de combustion en amont de la zone de combustion
F23D 17/00 - Brûleurs pour la combustion simultanée ou alternative de combustibles gazeux, liquides ou pulvérulents
The present invention comprises: a rotor; an annular sealing body part that includes the inner peripheral surface which is a static wall surface facing the outer peripheral surface of the rotor and a plurality of holes which are formed in the inner peripheral surface; a plurality of static fin parts that are disposed on the inner peripheral surface at intervals in the axial direction of the rotor; and at least one first rotor fin part that is disposed on the outer peripheral surface of the rotor. Each of the plurality of static fin parts extends along the circumferential direction of the rotor and protrudes toward the outer peripheral surface of the rotor from the inner peripheral surface, and each of the at least one first rotor fin part extends along the circumferential direction and protrudes toward the hole from the outer peripheral surface of the rotor.
F01D 11/02 - Prévention ou réduction des pertes internes du fluide énergétique, p. ex. entre étages par obturation non contact, p. ex. du type labyrinthe
F01D 25/00 - Parties constitutives, détails ou accessoires non couverts dans les autres groupes ou d'un intérêt non traité dans ces groupes
F04B 39/00 - Parties constitutives, détails ou accessoires de pompes ou de systèmes de pompage spécialement adaptés aux fluides compressibles, non prévus dans les groupes ou présentant un intérêt autre que celui visé par ces groupes
This method for operating a lock hopper (34) comprises a solid movement step. The solid movement step is for moving a solid from one of the inside and the outside of a combustible gas generation system to the other by introducing the solid into the lock hopper or discharging the solid from the lock hopper. The combustible gas generation system is for generating a combustible gas. The method for operating a lock hopper comprises a non-combustible gas introduction step and a discharge step. The non-combustible gas introduction step is for introducing a non-combustible gas into the lock hopper from a path different from a solid introduction opening and a solid discharge opening. The discharge step is for discharging, from the lock hopper, a gas inside the lock hopper using a path different from the solid introduction opening and the solid discharge opening.
C01B 3/26 - Production d'hydrogène ou de mélanges gazeux contenant de l'hydrogène par décomposition de composés organiques gazeux ou liquides d'hydrocarbures avec des catalyseurs
The gas turbine combustor according to at least one embodiment of the present disclosure is provided with: a combustion cylinder that comprises a combustion chamber therein; an air hole plate, in which a plurality of air holes extending in the axial direction of the combustion cylinder are formed, and which is located upstream of the combustion chamber; a cylindrical member which comprises in the interior thereof an internal space that extends in the axial direction, and which is located on the side opposite the combustion cylinder with respect to the air hole plate; and a top hat section that comprises a head end section that is located on the side opposite the air hole plate with respect to the cylindrical member. The cylindrical member comprises an opening section that is formed in a side section of the cylindrical member and is for drawing air within a combustor compartment into an internal space. When the top hat section is attached to a casing that demarcates the combustor compartment, at least part of the opening section is located further into the interior of the combustor compartment than the inner peripheral surface of the casing.
This gas turbine operation method includes executing: a first fuel single firing step of supplying only a first fuel to a first nozzle of a first burner, and not supplying the first fuel and a second fuel to a second nozzle for each of a plurality of second burners; a co-firing step of supplying only the first fuel to the first nozzle, and supplying only the second fuel to the second nozzle; a second fuel single firing preparation step of supplying the second fuel only to the second nozzle, without supplying the first fuel and the second fuel to the first nozzle; and a second fuel single firing step of supplying only the second fuel to the first nozzle and the second nozzle.
F02C 9/40 - Commande de l'alimentation en combustible spécialement adaptée à l'utilisation d'un combustible particulier ou de plusieurs combustibles
F02C 7/22 - Systèmes d'alimentation en combustible
F02C 7/228 - Division du fluide entre plusieurs brûleurs
F02C 7/232 - Soupapes pour combustibleSystèmes ou soupapes de drainage
F23R 3/10 - Aménagements de l'entrée d'air pour l'air primaire
F23R 3/28 - Chambres de combustion à combustion continue utilisant des combustibles liquides ou gazeux caractérisées par l'alimentation en combustible
F23R 3/30 - Chambres de combustion à combustion continue utilisant des combustibles liquides ou gazeux caractérisées par l'alimentation en combustible comprenant des dispositifs destinés à prévaporiser le combustible
F23R 3/36 - Alimentation en combustibles différents
This combustor comprises a central burner and an outer burner. The outer burner includes: an inner peripheral burner provided so as to surround an outer axis located on the radial outer-side of a demarcated combustor axis; and an outer peripheral burner provided so as to surround the demarcated inner peripheral burner. The amount of fuel supplied to demarcated fuel nozzles can be independently adjusted for the demarcated inner peripheral burner and the demarcated outer peripheral burner. A hole-free region where demarcated air holes of the outer peripheral burner are not formed is provided between the inner peripheral burner and the demarcated central burner on the downstream end face.
This generation system generates a gas of interest in a pressurized state. The gas of interest is a combustible gas. The generation system is provided with a lock hopper (34) and a combustible gas path. The lock hopper is configured to move a solid material from one of the inside of the generation system and the outside of the generation system to the other. In the lock hopper, a part different from an inlet port for the solid material and a discharge port for the solid material is connected to the combustible gas path. The combustible gas path is a path through which the combustible gas in the lock hopper is evacuated to the outside of the lock hopper. A downstream side of the combustible gas path is connected to an internal path in the generation system.
C01B 3/26 - Production d'hydrogène ou de mélanges gazeux contenant de l'hydrogène par décomposition de composés organiques gazeux ou liquides d'hydrocarbures avec des catalyseurs
C01B 3/56 - Séparation de l'hydrogène ou des gaz contenant de l'hydrogène à partir de mélanges gazeux, p. ex. purification par contact avec des solidesRégénération des solides usés
A turbine moving blade according to at least one embodiment of the present disclosure includes: a second cooling flow path; and a first cooling flow path that extends in the blade height direction, is formed on the leading edge side relative to the second cooling flow path, and is connected to the second cooling flow path at a first folded section on the base end side of an airfoil section. The first folded section includes an upstream-side region extending along the extension direction of the first folded section, from the inlet section at a position in the same blade height direction as the base end of the airfoil section to the central position in the wall thickness direction of the first partition wall when viewed from the blade height direction. The upstream-side region has, in at least a part of the blade height direction, a region in which an inner wall surface of a back-side blade wall and a partition wall surface on a leading edge side of a second partition wall is connected by a curved surface that protrudes outward from the inside of the airfoil section when viewed from the blade height direction, the region having a radius of curvature of the curved surface that increases from the tip end side toward the base end side of the airfoil section.
This rubbing determination device is for determining rubbing in a rotary machine having a rotation part rotatably supported with respect to a stationary part by a bearing. The device acquires an AE signal from an AE sensor attached to the stationary part. A maximum value and a minimum value of an envelope obtained by performing envelope processing on the temporal change of the AE signal are identified by signal analysis of the AE signal, and a first frequency spectrum corresponding to a first time zone including the maximum value in the temporal change, a second frequency spectrum corresponding to a second time zone including the minimum value in the temporal change, and an average spectrum of the first frequency spectrum and the second frequency spectrum are calculated. A first signal intensity ratio is calculated as a ratio of the signal intensity in a frequency band higher than a reference frequency in the first frequency spectrum with respect to the ratio of the signal intensity in the entire frequency band of the average spectrum. A second signal intensity ratio is calculated as a ratio of the signal intensity in a frequency band higher than the reference frequency in the second frequency spectrum with respect to the ratio of the signal intensity in the entire frequency band of the average spectrum. A first index is calculated as a ratio of the first signal intensity ratio to the second signal intensity ratio. The presence or absence of rubbing is determined on the basis of the first index.
G01M 99/00 - Matière non prévue dans les autres groupes de la présente sous-classe
G01H 17/00 - Mesure des vibrations mécaniques ou des ondes ultrasonores, sonores ou infrasonores non prévue dans les autres groupes de la présente sous-classe
This method for directly cracking a hydrocarbon into carbon and hydrogen comprises a step for bringing a starting gas containing methane and a hydrocarbon having two or more carbon atoms into contact with an unsupported catalyst that is an aggregate of multiple iron particles. The concentration of hydrocarbon having two or more carbon atoms in the starting gas is 0.02-10 vol%.
C01B 3/26 - Production d'hydrogène ou de mélanges gazeux contenant de l'hydrogène par décomposition de composés organiques gazeux ou liquides d'hydrocarbures avec des catalyseurs
This seal device comprises an annular seal ring centered on a seal axis, and a seal holding ring for holding the seal ring. The seal holding ring has an annular holding groove recessed radially inward. The seal ring has a contact surface that can come into contact with a low-pressure side groove side surface in the axial direction among surfaces that define the holding groove. The seal ring is divided into four or more in a circumferential direction with respect to the seal axis. The thrust load center radius is a radial distance between the seal axis and a thrust load center which is an intermediate position between the radially outer end of the contact surface and the position most radially inward in the seal ring. The inner end radius is the radial distance between the seal axis and the most radially inner end of the contact surface. The ratio of the inner end radius to the thrust load center radius is 1.20 or less.
This condenser comprises a plurality of heat transfer pipes, an in-body bypass pipe, and a body. The in-body bypass pipe is disposed between an exhaust steam port and a heat transfer pipe group consisting of the plurality of heat transfer pipes disposed in the body. The in-body bypass pipe includes a bypass pipe main body and an inspection nozzle connected to the bypass pipe main body. The bypass pipe main body extends in a pipe extension direction, and has a base end portion, which is one end portion in the pipe extension direction, that is connected to the body, and a tip end portion, which is the other end portion in the pipe extension direction, that is sealed. The bypass pipe main body has a plurality of steam ejection holes arranged in the pipe extension direction between the base end portion and the tip end portion. The inspection nozzle includes: an inspection nozzle pipe having one end connected to the bypass pipe main body so as to communicate with the inside of the bypass pipe main body; and a lid closing the other end of the inspection nozzle pipe.
F28G 9/00 - Nettoyage par lessivage ou par lavage, p. ex. avec des solvants chimiques
F28B 1/02 - Condenseurs dans lesquels la vapeur d'eau ou autre vapeur est séparée de l'agent de refroidissement par des parois, p. ex. condenseur à surface utilisant l'eau ou un autre liquide comme agent de refroidissement
47.
VANE ANGLE MEASUREMENT DEVICE AND VANE ANGLE MEASUREMENT METHOD USING SAME
This vane angle measurement device comprises a goniometer and a mount that supports the goniometer and that is capable of contacting a second member of an axial flow fluid machine. The goniometer has a measurement arm which is capable of contacting an arm contact surface of a first member in the axial flow fluid machine, and a goniometer body that supports the measurement arm in a manner allowing rotation about a measurement center axis, and that is capable of measuring the rotation angle of the measurement arm. The mount has a base plate to which the goniometer body is attached, and a first leg and second leg which extend from the base plate in the direction of the measurement center axis. The first leg has a device reference surface that is capable of contacting a first leg contact surface of the second member, and an arm height maintaining surface that is capable of contacting a second leg contact surface of the second member. The second leg has a second contact end that is capable of contacting the second leg contact surface. The length of the second leg from the base plate to the second contact end can be altered.
This quality evaluation device evaluates the quality of a rotary machine having a rotation unit that is supported by a bearing rotatably with respect to a stationary unit. The device acquires an AE signal from at least one AE sensor provided in the stationary unit, and calculates a rubbing detection index on the basis of the AE signal. The device then estimates the amount of wear of the rotary machine by integrating the rubbing detection index.
G01M 99/00 - Matière non prévue dans les autres groupes de la présente sous-classe
G01N 29/14 - Recherche ou analyse des matériaux par l'emploi d'ondes ultrasonores, sonores ou infrasonoresVisualisation de l'intérieur d'objets par transmission d'ondes ultrasonores ou sonores à travers l'objet utilisant des techniques d'émission acoustique
This combustible gas generation system comprises a reactor (16) and a filter device (22). The reactor is configured so as to thermally decompose a hydrocarbon, which is supplied to the combustible gas generation system, into carbon and hydrogen. The filter device is configured so as to capture the carbon that has flowed out from the reactor, and a combustible gas in the combustible gas generation system can be supplied to the filter device as a backwashing gas for regeneration processing of the filter device.
C01B 3/24 - Production d'hydrogène ou de mélanges gazeux contenant de l'hydrogène par décomposition de composés organiques gazeux ou liquides d'hydrocarbures
C01B 3/30 - Production d'hydrogène ou de mélanges gazeux contenant de l'hydrogène par décomposition de composés organiques gazeux ou liquides d'hydrocarbures avec des particules solides mobiles utilisant la technique du lit fluidisé
C01B 3/56 - Séparation de l'hydrogène ou des gaz contenant de l'hydrogène à partir de mélanges gazeux, p. ex. purification par contact avec des solidesRégénération des solides usés
50.
GASIFICATION FURNACE SYSTEM AND METHOD FOR OPERATING GASIFICATION FURNACE SYSTEM
A gas furnace system (1) comprises: a gasification furnace (10) that generates a synthesized gas; a high-temperature gas cooler (20) to which the synthesized gas discharged from the gasification furnace (10) is guided, and which cools the synthesized gas by exchanging heat with a cooling medium; an ash removal unit (30) to which the synthesized gas cooled by the high-temperature gas cooler (20) is guided, and which removes ash included in the synthesized gas; a low-temperature gas cooler (40) to which the synthesized gas, having ash been removed therefrom by the ash removal unit (30), is guided, and which cools the synthesized gas by heat exchange with a cooling medium; a tar removal unit (50) to which the synthesized gas cooled by the low-temperature gas cooler (40) is guided, and which removes tar contained in the synthesized gas; and a cooling medium line (L13) which guides, to the high-temperature gas cooler (20), the cooling medium having undergone heat exchange with the synthesized gas in the low-temperature gas cooler (40).
In a burner assembly according to at least one embodiment of the present disclosure, each of a plurality of burners includes at least one fuel nozzle for injecting fuel, and a mixing flow passage into which the fuel injected from the at least one fuel nozzle and air flows, wherein the burner assembly has a first region in which a plurality of the mixing flow passages are arranged collectively when viewed from an extension direction of the mixing flow passages, and a second region in which the number of mixing flow passages per unit area when viewed from the extension direction is smaller than in the first region. The burner assembly according to at least one embodiment of the present disclosure is provided, in at least a portion of a region of the second region in which there is no mixing flow passage, with a flow guide that protrudes farther toward an upstream side than an upstream end portion of a flow of air in the mixing flow passages.
F23R 3/28 - Chambres de combustion à combustion continue utilisant des combustibles liquides ou gazeux caractérisées par l'alimentation en combustible
F02C 7/232 - Soupapes pour combustibleSystèmes ou soupapes de drainage
F23R 3/10 - Aménagements de l'entrée d'air pour l'air primaire
F23R 3/30 - Chambres de combustion à combustion continue utilisant des combustibles liquides ou gazeux caractérisées par l'alimentation en combustible comprenant des dispositifs destinés à prévaporiser le combustible
This gas turbine plant comprises: a gas turbine having a combustor; a fuel gas line for guiding fuel gas containing gaseous ammonia to the combustor; and water recovery equipment into which exhaust gas from the gas turbine can flow. The water recovery equipment includes: a water recovery tower capable of recovering water contained in the exhaust gas from the gas turbine; a water cooler capable of cooling the water recovered in the water recovery tower; a recovered water line for guiding the water cooled by the water cooler to a target place; and a water spray line branched from the recovered water line and guiding portion of the water cooled by the water cooler to the water recovery tower. The water recovery tower has a recovery container into which the exhaust gas can flow, and a water sprayer capable of spraying water from the water spray line into the recovery container.
F02C 3/22 - Ensembles fonctionnels de turbines à gaz caractérisés par l'utilisation de produits de combustion comme fluide de travail utilisant un combustible, un oxydant ou un fluide de dilution particulier pour produire les produits de combustion le combustible ou l'oxydant étant gazeux aux température et pression normales
F02C 6/18 - Utilisation de la chaleur perdue dans les ensembles fonctionnels de turbines à gaz à l'extérieur des ensembles eux-mêmes, p. ex. ensembles fonctionnels de chauffage à turbine à gaz
F02C 7/00 - Caractéristiques, parties constitutives, détails ou accessoires non couverts dans, ou d'un intérêt plus général que, les groupes Entrées d'air pour ensembles fonctionnels de propulsion par réaction
F02C 7/224 - Chauffage du combustible avant son arrivée au brûleur
53.
CLASSIFIER, GRINDING MILL, AND METHOD OF PRODUCING CLASSIFIER
The purpose of the present invention is to easily provide an attachment section to a blade. This rotary classifier (16) rotates about a central axis (C) extending in the vertical direction, and classifies particles that have been guided by a carrier gas from outside in the radial direction into particles larger than a predetermined particle size and particles at or below the predetermined particle size, said classifier comprising: a main body (70) that rotates about the central axis (C); and a plurality of blades (60) that are supported on the main body (70), extend in the vertical direction, are arranged lined up at predetermined intervals along the circumferential direction about the central axis (C), and repel, at a collision surface, the particles larger than the predetermined particle size. The main body (70) has a plurality of brackets supporting the blades (60). The blades (60) each comprise: a base (62) formed of stainless steel; a hardened section (63) that covers a front surface of the base (62) in a direction of rotation and is formed of a material of a higher hardness than that of the base (62); and an attachment section that is to be fixed to a rear surface of the base (62) in the direction of rotation and attached to the bracket.
B02C 23/12 - Séparation ou triage de matériaux, associé au broyage ou à la désagrégation au moyen d'un séparateur situé dans le passage de décharge de la zone de broyage ou de désagrégation avec retour des matériaux hors dimension à la zone de broyage ou de désagrégation
B02C 15/04 - Appareils comportant des cylindres serrés, montés pendulairement, p. ex. serrés par des ressorts
B02C 17/18 - Désagrégation au tonneau, c.-à-d. par des appareils constitués par une cuve où les produits à désagréger sont chargés, avec ou sans éléments particuliers de désagrégation tels que billes ou boulets Parties constitutives
B02C 23/16 - Séparation ou triage de matériaux, associé au broyage ou à la désagrégation au moyen d'un séparateur délimitant la fin de la zone de broyage ou de désagrégation, p. ex. au moyen d'un tamis empêchant la sortie des matériaux hors dimension
B02C 25/00 - Systèmes de commande spécialement adaptés au broyage ou à la désagrégation
B07B 7/083 - Séparation sélective des matériaux solides portés par des courants de gaz, ou dispersés dans ceux-ci utilisant la force centrifuge produite par la rotation d'ailettes, de disques, de tambours ou de brosses
54.
CLINKER FALL DETECTION DEVICE AND CLINKER FALL DETECTION SYSTEM
This clinker fall detection device includes: a vibration data acquisition unit configured to acquire vibration data indicating a physical quantity related to vibration of a lower part of a furnace of a boiler from a sensor that detects the physical quantity related to vibration of the lower part; and a clinker fall detection unit configured to detect a fall of clinker to a bottom part of the furnace on the basis of the vibration data acquired by the vibration data acquisition unit.
F22B 37/38 - Détermination ou signalisation des conditions de marche dans les chaudières à vapeur, p. ex. enregistrant la direction ou le débit du courant d'eau dans les tubes
F23M 11/04 - Moyens pour surveiller la combustion, p. ex. fenêtres
F23N 5/24 - Systèmes prévenant le développement de conditions anormales ou indésirables, c.-à-d. dispositifs de sécurité
G01H 17/00 - Mesure des vibrations mécaniques ou des ondes ultrasonores, sonores ou infrasonores non prévue dans les autres groupes de la présente sous-classe
The present invention is provided with: a gas turbine; a bleed-air line enabled for bleeding off as bleed air a portion of compressed air generated in a compressor of the gas turbine; a branch line that branches from the bleed-air line; a bleed-air turbine that is connected to the branch line and is enabled for being driven by the bleed air having flowed through the branch line; and a volume-contraction device that is connected to the bleed-air line and is enabled for contracting the volume of the bleed air having flowed through the bleed-air line. The volume-contraction device has a device-internal compressor enabled for compressing the bleed air, and an assistance mechanism to assist the driving of the device-internal compressor. The assistance mechanism causes the drive energy of the bleed-air turbine to be used for driving the at least one device-internal compressor.
F02C 6/08 - Ensembles fonctionnels de turbines à gaz délivrant un fluide de travail chauffé ou pressurisé à d'autres appareils, p. ex. sans sortie de puissance mécanique délivrant des gaz comprimés le gaz étant prélevés sur le compresseur de la turbine à gaz
F02C 6/00 - Ensembles fonctionnels multiples de turbines à gazCombinaisons d'ensembles fonctionnels de turbines à gaz avec d'autres appareilsAdaptations d'ensembles fonctionnels de turbines à gaz à des applications particulières
F02C 6/16 - Ensembles fonctionnels de turbines à gaz comportant des moyens pour emmagasiner l'énergie, p. ex. pour faire face à des pointes de charge pour emmagasiner de l'air comprimé
F02C 9/48 - Commande de l'alimentation en combustible combinée avec une autre commande de l'ensemble fonctionnel
56.
APPARATUS AND METHOD FOR DIRECT DECOMPOSITION OF HYDROCARBON
In the present invention, an apparatus for direct decomposition of a hydrocarbon directly decomposes a hydrocarbon into carbon and hydrogen using a gas containing methane and a hydrocarbon having two or more carbon atoms as a raw material gas. The apparatus comprises: a reformer that houses a first catalyst for methanation of a hydrocarbon having two or more carbon atoms; a reactor which is configured so that a reformed gas discharged from the reformer flows into the reactor, and which houses a second catalyst that is an iron-based catalyst; and a recycling line that connects a produced gas line in which a produced gas discharge from the reactor flows, to a raw material gas line for introducing the raw material gas into the reformer.
C01B 3/26 - Production d'hydrogène ou de mélanges gazeux contenant de l'hydrogène par décomposition de composés organiques gazeux ou liquides d'hydrocarbures avec des catalyseurs
B01J 23/46 - Ruthénium, rhodium, osmium ou iridium
Provided is a filter regeneration system in which the risk of abnormal combustion of a deposited char that has fallen from a filter can be avoided, and the filter can be regenerated without performing inspection and cleaning of the filter after cooling the filter. This filter regeneration system includes: a main body container (23) into which a dust-containing gas including char discharged from a gasification furnace for gasifying coal is introduced; a porous filter (24) that is provided inside the main body container (23) and filters the dust-containing gas; a regeneration gas supply means (34) that, when regenerating the porous filter (24), supplies a regeneration gas for heating and reacting the char adhering to the porous filter (24) to the porous filter (24); and an inactive gas supply means (35) that supplies an inactive gas to a lower space (28) of the main body container (23) positioned below the porous filter (24).
The present application pertains to a gas turbine control device for controlling a gas turbine provided with a combustor capable of co-firing a first fuel and a second fuel that has a high combustion speed. The device controls a co-firing rate of the second fuel to be a preset target co-firing rate. If the co-firing rate is determined to be larger than a first reference value set larger than the target co-firing rate, the fuel flow rate of the second fuel is controlled so that the co-firing rate becomes smaller than a second reference value set lower than the target co-firing rate.
F02C 9/40 - Commande de l'alimentation en combustible spécialement adaptée à l'utilisation d'un combustible particulier ou de plusieurs combustibles
F02C 3/22 - Ensembles fonctionnels de turbines à gaz caractérisés par l'utilisation de produits de combustion comme fluide de travail utilisant un combustible, un oxydant ou un fluide de dilution particulier pour produire les produits de combustion le combustible ou l'oxydant étant gazeux aux température et pression normales
F02C 7/22 - Systèmes d'alimentation en combustible
A turbine blade according to at least one embodiment of the present disclosure includes a shroud portion located farther to the blade tip-end side than an airfoil portion. A trailing edge side end portion of the shroud portion includes a trailing edge side contact surface formed so as to face the trailing edge side in the chord direction, and a trailing edge side curved surface connected to the leading edge side end portion of the trailing edge side contact surface. When viewed in the blade height direction, the radius of curvature at a first position of the trailing edge side curved surface is defined as a first radius of curvature, and the radius of curvature at a second position farther from the trailing edge side contact surface than the first position is defined as a second radius of curvature. The turbine blade according one embodiment is such that the trailing edge curved surface has a region that is recessed farther toward the leading edge side than an extension line of the trailing edge side contact surface when viewed in the blade height direction, and the second radius of curvature is smaller than the first radius of curvature.
The present invention pertains to a method for calculating the amount of change in a clearance of a blade ring and a method for adjusting the position of the blade ring. This method for calculating the amount of change in a clearance of a blade ring calculates the amount of change in a clearance in a vertical direction between an inner peripheral surface of the blade ring and an outer peripheral surface of a rotary shaft disposed inside the blade ring, the blade ring having a ring shape being configured by connecting a blade ring upper half part and a blade ring lower half part. The method comprises: a step for acquiring a displacement amount in a horizontal direction of the blade ring between a first state in which the blade ring upper half part is connected to the blade ring lower half part and a second state in which the blade ring upper half part has been removed from the blade ring lower half part; a step for calculating a second neutral axis of the blade ring in the second state on the basis of the displacement amount; and a step for calculating the amount of change in a clearance between the first state and the second state by comparing a first neutral axis of the blade ring in the first state with the second neutral axis.
The purpose of the present invention is to even the concentration of a reducing agent in a gas flowing in a duct. An ammonia injection part (20) injects a reducing agent into an exhaust gas flowing in a duct (3), the reducing agent having the function of reducing nitrogen oxides contained in the exhaust gas. The ammonia injection part (20) comprises: a plurality of ejection nozzles (21) for injecting an ammonia gas into the exhaust gas flowing in the duct (3); a plurality of base pipes (22) which have the plurality of ejection nozzles (21) provided thereto and in which the ammonia gas flows; and a header (23) which is provided to the inside of the duct (3) on the downstream side along the gas flow direction from the base pipes (22) and supplies the reducing agent to the plurality of base pipes (22). The distance (D) from the base pipes (22) to the header (23) is longer than three times the outer diameter (d) of each of the base pipes (22).
A biomass gasification device (1) comprises: a gasification furnace body in which a first cylindrical part (4), a second cylindrical part (5), and a third cylindrical part (6) are connected in that order from the upstream side of the gas flow, from top to bottom; a gasifying agent supply part (10) that is connected to the first cylindrical part (4) and that supplies a gasifying agent; and a biomass raw material supply part (14) that is connected to the second cylindrical part (5) and that supplies a granular biomass raw material. If the representative diameter (ΦL) of the first cylindrical part (4) is 1, the representative diameter (ΦU) of the third cylindrical part (6) is 3-9 (excluding 6.5-7.5).
The purpose of the present invention is to collectively provide a user with a plurality of plant components constituting a fluid transport system. This purchase assistance device (1a) comprises: a condition input assistance unit (31) that acquires, as a selection condition, a requested function and a requested specification relating to a fluid transport system that a user desires to purchase; a standard system constitution generation unit (32) that identifies a plurality of standard components respectively corresponding to a plurality of element components constituting the fluid transport system, on the basis of the selection condition, from a standard component database (21) storing information relating to a plurality of standard components relating to the fluid transport system; and an order specification creation unit (61) that creates an ordered specification on the basis of a standard fluid transport system constituted of the specified plurality of standard components.
This hydrogen production system comprises: a solid oxide electrolysis cell (SOEC) that electrolyzes water vapor; a water vapor generation device that heats supply water to generate water vapor; and a combustor that partially burns hydrogen included in water vapor discharged from a hydrogen electrode of the SOEC. The water vapor generation device is configured such that the supply water is at least partially heated through heat exchange between at least part of the supply water and gas including combustion gas generated in the combustor so as to produce at least part of the water vapor.
C25B 1/042 - Hydrogène ou oxygène par électrolyse de l'eau par électrolyse de la vapeur
C25B 9/00 - Cellules ou assemblages de cellulesÉléments de structure des cellulesAssemblages d'éléments de structure, p. ex. assemblages d'électrode-diaphragmeCaractéristiques des cellules relatives aux procédés
F22D 1/02 - Appareils de chauffage d'eau d'alimentation, p. ex. préchauffeurs avec tubes d'eau disposés dans le foyer de la chaudière, les tubes de fumées ou sur le trajet des fumées
The present application relates to a gas turbine control device for controlling a gas turbine including a combustor capable of co-firing a first fuel with a second fuel having a lower heat quantity per unit volume. This device controls the gas turbine on the basis of a control parameter that is obtained by correcting a reference value corresponding to mono-firing of the first fuel, using a correction value. The correction value is calculated such that as the second fuel co-firing ratio increases, the control parameter becomes smaller or larger than the reference value, and the amount of deviation from the reference value increases.
Provided is an electrolysis system (10) comprising: an electrolysis cell (11); an air supply system (20) for supplying, to an oxygen electrode, air for adjusting the temperature of the electrolysis cell (11); a discharge system (30) through which exhaust air containing oxygen and air and discharged from the electrolysis cell (11) flows; a circulation system (40) for guiding at least part of the exhaust air discharged to the discharge system (30) to the air supply system (20); an oxygen concentration measurement unit (60) for measuring the oxygen concentration of the exhaust air discharged from the electrolysis cell (11) to the discharge system (30); and a steam supply system (70) for decreasing the oxygen concentration of the exhaust air guided from the circulation system (40) to the air supply system (20) so that the oxygen concentration measured by the oxygen concentration measurement unit (60) does not exceed a set concentration range.
C25B 15/023 - Mesure, analyse ou test pendant la production électrolytique
C25B 1/042 - Hydrogène ou oxygène par électrolyse de l'eau par électrolyse de la vapeur
C25B 9/00 - Cellules ou assemblages de cellulesÉléments de structure des cellulesAssemblages d'éléments de structure, p. ex. assemblages d'électrode-diaphragmeCaractéristiques des cellules relatives aux procédés
C25B 15/021 - Commande ou régulation des opérations de chauffage ou de refroidissement
67.
ELECTROLYSIS SYSTEM AND CONTROL METHOD FOR ELECTROLYSIS SYSTEM
Provided is an electrolysis system (100) including an electrolysis module (10); a water vapor supply system (40) that supplies water vapor to a hydrogen electrode; a hydrogen recovery system (50) that recovers hydrogen-enriched water vapor; an air supply system (20) that supplies air to an oxygen electrode; an oxygen recovery system (30) that recovers exhaust air; a hydrogen-enriched water vapor release system (60) that releases hydrogen-enriched water vapor from the hydrogen recovery system (50) into the atmosphere; an exhaust air release system (70) that releases exhaust air from the oxygen recovery system (30) into the atmosphere; a hydrogen-enriched water vapor discharge valve (63) disposed in the hydrogen-enriched water vapor discharge system (60); and an exhaust air discharge valve (73) disposed in the exhaust air discharge system (70), wherein the opening degrees of the hydrogen-enriched water vapor discharge valve (63) and the exhaust air discharge valve (73) are controlled to be adjustable when the electrolytic module (10) is stopped.
C25B 15/08 - Alimentation ou vidange des réactifs ou des électrolytesRégénération des électrolytes
C25B 1/042 - Hydrogène ou oxygène par électrolyse de l'eau par électrolyse de la vapeur
C25B 9/00 - Cellules ou assemblages de cellulesÉléments de structure des cellulesAssemblages d'éléments de structure, p. ex. assemblages d'électrode-diaphragmeCaractéristiques des cellules relatives aux procédés
C25B 15/023 - Mesure, analyse ou test pendant la production électrolytique
68.
GAS TURBINE CONTROL DEVICE, GAS TURBINE CONTROL METHOD, AND GAS TURBINE CONTROL PROGRAM
In order to control a gas turbine in a rated operation state on the basis of a maximum output command, this gas turbine control device calculates, for an inlet guide vane for adjusting the intake air flow rate of the gas turbine and on the basis of at least one of the atmospheric pressure and the intake air temperature of the gas turbine, the basic target opening degree corresponding to the maximum output command. The opening degree of the inlet guide vane of the gas turbine is controlled on the basis of a target opening degree obtained by using a bias correction value to correct the basic target opening degree. Calculation of the bias correction value is performed such that the target opening degree becomes smaller than the basic target opening degree if the combustion temperature of the gas turbine is lower than the temperature upper limit value corresponding to the maximum output command. If the output of the gas turbine is lower than the rated output value corresponding to the maximum output command, calculation of the bias correction value is performed such that the target opening degree becomes greater than the basic target opening degree.
In a burner assembly according to at least one embodiment of the present disclosure, each of a plurality of burners is provided with a flow passage through which air can flow. The flow passage includes a first region, in which a fuel injection hole is formed, and a second region, which is located downstream of the first region and in which the fuel injected through the injection hole and air are mixed. The first region extends from an upstream-side end part of the flow passage to a connection position with the second region, and the injection hole is formed at a position closer to the connection position than the upstream-side end part. The first region has at least one protrusion, which protrudes radially inward of the flow passage and in which the injection hole is formed, and at least one peripheral wall, which is adjacent to the at least one protrusion in the circumferential direction of the flow passage and in which the protrusion is not provided. The cross-sectional area of the flow passage is such that a second cross-sectional area within the second region is less than a first cross-sectional area within the first region.
F23R 3/28 - Chambres de combustion à combustion continue utilisant des combustibles liquides ou gazeux caractérisées par l'alimentation en combustible
F23R 3/32 - Chambres de combustion à combustion continue utilisant des combustibles liquides ou gazeux caractérisées par l'alimentation en combustible comprenant des dispositifs destinés à prévaporiser le combustible tubulaires
70.
HYDROGEN PRODUCTION SYSTEM AND METHOD FOR OPERATING HYDROGEN PRODUCTION SYSTEM
This hydrogen production system is provided with: a solid oxide electrolytic cell (SOEC) that electrolyzes water vapor; a power supply device that applies a voltage equal to or greater than a thermal neutral voltage to the SOEC; and a water vapor generation device that generates at least a portion of water vapor to be supplied to the SOEC by heating water using surplus heat generation of the SOEC.
C25B 1/042 - Hydrogène ou oxygène par électrolyse de l'eau par électrolyse de la vapeur
C25B 9/00 - Cellules ou assemblages de cellulesÉléments de structure des cellulesAssemblages d'éléments de structure, p. ex. assemblages d'électrode-diaphragmeCaractéristiques des cellules relatives aux procédés
C25B 9/67 - Moyens de chauffage ou de refroidissement
C25B 15/02 - Commande ou régulation des opérations
C25B 15/021 - Commande ou régulation des opérations de chauffage ou de refroidissement
A gas turbine according to at least one embodiment of the present disclosure comprises a combustor capable of co-combustion of a first fuel and a hydrogen fuel that has a higher combustion speed than the first fuel. The gas turbine according to at least one embodiment of the present disclosure has a co-combustion rate acquisition unit that acquires information which indicates the co-combustion rate of the hydrogen fuel and a steam injection control unit that controls the injection amount of steam to be injected with respect to air which has been compressed by a compressor and which flows through a flow path for supplying the compressed air to the combustor. The steam injection control unit controls the injection amount the steam on the basis of the co-combustion rate of hydrogen fuel acquired by the co-combustion rate acquisition unit.
F02C 9/00 - Commande des ensembles fonctionnels de turbines à gazCommande de l'alimentation en combustible dans les ensembles fonctionnels de propulsion par réaction alimentés en air ambiant
F02C 3/30 - Addition d'eau, de vapeur ou d'autres fluides aux composants combustibles ou au fluide de travail avant l'échappement de la turbine
F02C 7/22 - Systèmes d'alimentation en combustible
F02C 9/28 - Systèmes de régulation sensibles aux paramètres ambiants ou à ceux de l'ensemble fonctionnel, p. ex. à la température, à la pression, à la vitesse du rotor
F02C 9/40 - Commande de l'alimentation en combustible spécialement adaptée à l'utilisation d'un combustible particulier ou de plusieurs combustibles
72.
GAS TURBINE CONTROL DEVICE, GAS TURBINE CONTROL METHOD, AND GAS TURBINE CONTROL PROGRAM
This gas turbine control device is a control device for controlling a gas turbine provided with a combustor capable of co-firing a first fuel and a second fuel. The device controls the flow rate of the first fuel to be a flow rate target value when a load reduction request with respect to the gas turbine has been acquired. The flow rate target value when the load reduction request is acquired is set by correcting a basic flow rate target value of the first fuel, which is for achieving a load corresponding to the load reduction request through single firing of the first fuel, on the basis of a co-firing rate.
F02C 9/28 - Systèmes de régulation sensibles aux paramètres ambiants ou à ceux de l'ensemble fonctionnel, p. ex. à la température, à la pression, à la vitesse du rotor
F02C 7/22 - Systèmes d'alimentation en combustible
F02C 7/232 - Soupapes pour combustibleSystèmes ou soupapes de drainage
F02C 9/00 - Commande des ensembles fonctionnels de turbines à gazCommande de l'alimentation en combustible dans les ensembles fonctionnels de propulsion par réaction alimentés en air ambiant
F02C 9/40 - Commande de l'alimentation en combustible spécialement adaptée à l'utilisation d'un combustible particulier ou de plusieurs combustibles
F23R 3/28 - Chambres de combustion à combustion continue utilisant des combustibles liquides ou gazeux caractérisées par l'alimentation en combustible
73.
EXHAUST GAS PURIFICATION METHOD AND EXHAUST GAS PURIFICATION APPARATUS
An exhaust gas purification method comprising: allowing an exhaust gas containing at least one substance selected from the group consisting of ash dust, hydrogen chloride, a nitrogen oxide, a sulfur oxide, mercury, a volatile organic compound and a carbon oxide to pass through a catalyst bag filter having at least one function selected from the group consisting of a denitration function, an NO oxidation function, an Hg022 absorption solution to reduce carbon dioxide in the exhaust gas.
B01D 53/14 - Séparation de gaz ou de vapeursRécupération de vapeurs de solvants volatils dans les gazÉpuration chimique ou biologique des gaz résiduaires, p. ex. gaz d'échappement des moteurs à combustion, fumées, vapeurs, gaz de combustion ou aérosols par absorption
A steam turbine exhaust chamber according to one embodiment comprises a diffuser that forms a diffuser space, and an exhaust casing that forms an exhaust space. The diffuser has an outer diffuser defining a radially outer edge of the diffuser space, and an inner diffuser defining a radially inner edge of the diffuser space. Regarding a first flow guide, the distance in an axial direction from an axis downstream-side end second of a blade end of a final stage moving blade to an axis downstream-side end section of the first flow guide is 20% to 45% of the blade height of the final stage moving blade, for example.
This gas turbine device comprises a combustor casing to which compressed air from a gas turbine compressor is guided, a combustor which is provided in the combustor casing and which includes a gas nozzle for injecting gaseous fuel and an oil nozzle for ejecting oil fuel, a first purge air line configured to supply first air derived from bleed air from the combustor casing to the oil nozzle, and a second purge air line configured to supply second air compressed by an external compressor separate from the gas turbine compressor to the oil nozzle, the gas turbine device being configured to be capable of selectively supplying the first air from the first purge air line and the second air from the second purge air line as purge air to the oil nozzle.
Provided is an assistance device that prevents misattachment of pipe. This assistance device comprises: an acquisition unit that acquires code information of a pipe which has a plurality of connection ports and on which the code information is displayed on each of the connection ports, and code information displayed on a connection target apparatus; a database that associates and stores the code information of each connection port and code information of every connection target; a determination unit that makes a determination of suitable if the code information of the pipe and the connection target code information acquired by the acquisition unit are associated and stored in the database, and if not, makes a determination of not suitable; and a control unit that controls, in accordance with determination results, a display mode of the pipe in a model in which an apparatus to which the pipe is connected is displayed. The pipe is displayed in different display modes in accordance with the number of the connection ports, of the plurality of connection ports, determined to be suitable.
G06F 30/18 - Conception de réseaux, p. ex. conception basée sur les aspects topologiques ou d’interconnexion des systèmes d’approvisionnement en eau, électricité ou gaz, de tuyauterie, de chauffage, ventilation et climatisation [CVC], ou de systèmes de câblage
A turbine stator vane according to at least one embodiment of the present disclosure comprises: a vane-shaped part; an inner shroud; a pair of circumferential wall parts that, at ends on one side and the other side in the circumferential direction in the inner shroud, extend in the extending direction of the ends; a longitudinal wall part which extends in the circumferential direction, in which ends on one side and the other side in the circumferential direction are connected to the pair of circumferential wall parts, and which projects from the inner shroud; a connection part that connects, through a gentle curved surface, the longitudinal wall part and the pair of circumferential wall parts; and a first plate member that constitutes a cavity together with a surface on the opposite side of the inner shroud and the pair of circumferential wall parts. The first plate member has a first planar part along the pair of circumferential wall parts, a second planar part along the longitudinal wall part, and a curved surface part along the connection part. The curved surface part includes, at at least ends of one side and the other side in the circumferential direction, thick sections thicker than the thickness of the first and second planar parts.
F01D 9/02 - InjecteursLogement des injecteursAubes de statorTuyères de guidage
F01D 9/04 - InjecteursLogement des injecteursAubes de statorTuyères de guidage formant une couronne ou un secteur
F01D 25/00 - Parties constitutives, détails ou accessoires non couverts dans les autres groupes ou d'un intérêt non traité dans ces groupes
F02C 7/00 - Caractéristiques, parties constitutives, détails ou accessoires non couverts dans, ou d'un intérêt plus général que, les groupes Entrées d'air pour ensembles fonctionnels de propulsion par réaction
78.
HYDROGEN PRODUCTION SYSTEM AND METHOD FOR OPERATING HYDROGEN PRODUCTION SYSTEM
A hydrogen production system according to the present invention comprises: a solid oxide electrolysis cell (SOEC) that electrolyzes water vapor; a water vapor supply line for supplying water vapor to a hydrogen electrode of the SOEC; a water vapor discharge line through which water vapor discharged from the hydrogen electrode circulates; a first bypass line that communicates the water vapor supply line with the water vapor discharge line; and a first regulation device for regulating the flow rate of water vapor circulating through the first bypass line.
C25B 1/042 - Hydrogène ou oxygène par électrolyse de l'eau par électrolyse de la vapeur
C25B 9/00 - Cellules ou assemblages de cellulesÉléments de structure des cellulesAssemblages d'éléments de structure, p. ex. assemblages d'électrode-diaphragmeCaractéristiques des cellules relatives aux procédés
Provided are an operation mode switching assistance device, an economic efficiency simulator, a fuel production system, an operation mode switching assistance method, and an operation mode switching assistance program with which a choice can be switched in order to increase profit. An operation mode switching assistance device (50) of a fuel production system (1) for producing fuel by combining a biomass-fired power generation facility (10), a water electrolysis device (20), and a fuel production reaction device (30), acquires the selling price of electricity generated by the biomass-fired power generation facility (10) and the selling price of the fuel produced by the fuel production system (1), and controls switching between an electricity selling mode in which the electricity is sold and a fuel production mode in which fuel is produced, on the basis of the result of a comparison between the electricity selling price and the fuel selling price.
A tubular body for a combustor according to at least one embodiment of the present disclosure comprises: a first cooling passage that is formed in an upstream-side region which is located inside a wall part of the tube body and which is positioned on the upstream side of the tube body, that has a supply port which opens on the outer peripheral surface of the tube body, and that is capable of cooling the upstream-side region with a first cooling fluid introduced thereto; a second cooling passage that is formed in a downstream-side region which is located inside the wall part and which is positioned on the downstream side of the tube body relative to the upstream-side region, that is capable of cooling the downstream-side region, and that has a discharge port via which a second cooling fluid can be discharged to space outside the tube body; and a first wall that is disposed between the supply port and the discharge port and that extends along the outer peripheral surface in the circumferential direction of the tube body. The first wall has a first wall part, the base end portion of which is connected to the outer peripheral surface, which extends in a direction away from the outer peripheral surface, and which extends in the circumferential direction, and a first discontinuous part in which the first wall part is discontinuous in the circumferential direction.
F23R 3/42 - Chambres de combustion à combustion continue utilisant des combustibles liquides ou gazeux caractérisées par la disposition ou la forme des tubes à flamme ou des chambres de combustion
A cylinder for a combustor according to one embodiment, inside which combustion gas generated by combustion of fuel can circulate, comprises a cylinder body extending along an axis line. The cylinder body has at least one cooling passage which is formed in a wall part of the cylinder body, which extends in the extension direction of the axis line, and in which a cooling fluid can circulate. The at least one cooling passage has: an inlet opening that is an inlet for the cooling fluid and that opens on a peripheral surface of the cylinder body; and an outlet opening that is an outlet for the cooling fluid and that opens on the peripheral surface of the cylinder body. The inlet opening and/or the outlet opening has a first dimension in the extension direction of the axis line greater than a second dimension in the circumferential direction of the cylinder body.
F02C 7/18 - Refroidissement des ensembles fonctionnels caractérisé par l'agent refroidisseur l'agent refroidisseur étant gazeux, p. ex. l'air
F23R 3/28 - Chambres de combustion à combustion continue utilisant des combustibles liquides ou gazeux caractérisées par l'alimentation en combustible
F23R 3/42 - Chambres de combustion à combustion continue utilisant des combustibles liquides ou gazeux caractérisées par la disposition ou la forme des tubes à flamme ou des chambres de combustion
This power generation system includes a pyrolysis device (10) and a gas turbine (16). The pyrolysis device is for pyrolyzing a hydrocarbon gas into hydrogen and carbon. The fuel of the gas turbine includes a gas mixture of hydrogen and hydrocarbon gas generated by pyrolyzing said hydrocarbon gas by the pyrolysis device.
F02C 3/28 - Ensembles fonctionnels de turbines à gaz caractérisés par l'utilisation de produits de combustion comme fluide de travail utilisant un combustible, un oxydant ou un fluide de dilution particulier pour produire les produits de combustion le combustible ou l'oxydant étant solide ou pulvérulent, p. ex. mélangé avec un liquide ou en suspension utilisant un générateur de gaz séparé pour gazéifier le combustible avant la combustion
C01B 3/26 - Production d'hydrogène ou de mélanges gazeux contenant de l'hydrogène par décomposition de composés organiques gazeux ou liquides d'hydrocarbures avec des catalyseurs
C10L 3/00 - Combustibles gazeuxGaz naturelGaz naturel de synthèse obtenu par des procédés non prévus dans les sous-classes , Gaz de pétrole liquéfié
This electrical power generation system comprises a heater (12), a reactor (10), an exhaust gas heat exchanger (14), and a gas turbine (22). The heater is configured to supply heat to the reactor. The reactor is configured to generate hydrogen by pyrolysis of hydrocarbon gas into hydrogen and carbon. Fuel for the gas turbine includes hydrogen produced by the reactor. The exhaust gas heat exchanger is configured to provide heat of exhaust gas, which is discharged from the heater, to fuel gas in the electrical power generation system.
F02C 3/22 - Ensembles fonctionnels de turbines à gaz caractérisés par l'utilisation de produits de combustion comme fluide de travail utilisant un combustible, un oxydant ou un fluide de dilution particulier pour produire les produits de combustion le combustible ou l'oxydant étant gazeux aux température et pression normales
C01B 3/26 - Production d'hydrogène ou de mélanges gazeux contenant de l'hydrogène par décomposition de composés organiques gazeux ou liquides d'hydrocarbures avec des catalyseurs
C10L 3/00 - Combustibles gazeuxGaz naturelGaz naturel de synthèse obtenu par des procédés non prévus dans les sous-classes , Gaz de pétrole liquéfié
F02C 6/00 - Ensembles fonctionnels multiples de turbines à gazCombinaisons d'ensembles fonctionnels de turbines à gaz avec d'autres appareilsAdaptations d'ensembles fonctionnels de turbines à gaz à des applications particulières
84.
COMBUSTION SYSTEM, BOILER SYSTEM, AND METHOD FOR OPERATING COMBUSTION SYSTEM
The objective of the present invention is to appropriately reuse ammonia discharged from a fuel supply system, using a simple construction. This combustion system comprises: a burner (21D) for burning ammonia to form a flame inside a furnace; a combustion gas passage through the inside of which a combustion gas generated in the furnace flows; an ammonia fuel supply system (210) for supplying ammonia to the burner (21D) as fuel; a purge gas line (221) for supplying into the ammonia fuel supply system (210) a purge gas for discharging the ammonia from the ammonia fuel supply system (210); and an ammonia supply system (220) for supplying the ammonia discharged from the ammonia fuel supply system (210) into the combustion gas passage.
F23J 15/00 - Aménagement des dispositifs de traitement de fumées ou de vapeurs
F23C 1/04 - Appareils à combustion spécialement adaptés à la combustion de plusieurs sortes de combustibles simultanément ou alternativement, au moins un des combustibles étant fluide ou étant un combustible solide en suspension dans l’air du combustible en morceaux et du combustible gazeux
85.
ELECTROLYSIS CELL SYSTEM AND ELECTROLYSIS CELL SYSTEM OPERATION METHOD
The purpose of this invention is to improve energy efficiency in an electrolysis cell system. An electrolysis cell system (10) comprises: an electrolysis cell (11) that has an oxygen electrode and a hydrogen electrode, wherein water vapor supplied to the hydrogen electrode is electrolyzed to generate hydrogen at the hydrogen electrode and generate oxygen at the oxygen electrode; a supply system (20) supplying air for adjusting the temperature of the electrolysis cell (11) to the electrolysis cell (11); a discharge system (30) through which air discharged from the electrolysis cell (11) flows; a circulation system (40) directing the air discharged to the discharge system (30) to the supply system (20); and a supply air temperature adjusting heat exchanger (28) for adjusting the temperature of air supplied to the electrolysis cell (11).
C25B 9/00 - Cellules ou assemblages de cellulesÉléments de structure des cellulesAssemblages d'éléments de structure, p. ex. assemblages d'électrode-diaphragmeCaractéristiques des cellules relatives aux procédés
C25B 9/19 - Cellules comprenant des électrodes fixes de dimensions stablesAssemblages de leurs éléments de structure avec des diaphragmes
86.
REPAIR METHOD, AND METHOD FOR MANUFACTURING COMBUSTION CYLINDER
A repair method according to at least one embodiment of the present disclosure includes: a step for removing, from a member internally including at least one passage through which a fluid can flow, a portion of a passage-forming portion that forms the at least one passage; a step for performing welding to build up the passage-forming portion from which said portion has been removed; after the buildup, a step for forming at least one communicating hole formed by removing a portion of the built-up welded portion, the communicating hole providing communication between the outside of the member and the at least one passage; and a step for closing an open end of the at least one communicating hole that opens in an outer surface of the member.
B23K 31/00 - Procédés relevant de la présente sous-classe, spécialement adaptés à des objets ou des buts particuliers, mais non couverts par un seul des groupes principaux
B23K 9/04 - Soudage pour d'autres buts que l'assemblage de pièces, p. ex. soudage de rechargement
B23P 6/04 - Réparation de pièces ou de produits métalliques brisés ou fissurés, p. ex. de pièces de fonderie
F02C 7/00 - Caractéristiques, parties constitutives, détails ou accessoires non couverts dans, ou d'un intérêt plus général que, les groupes Entrées d'air pour ensembles fonctionnels de propulsion par réaction
F02C 7/18 - Refroidissement des ensembles fonctionnels caractérisé par l'agent refroidisseur l'agent refroidisseur étant gazeux, p. ex. l'air
87.
PURCHASE ASSISTANCE DEVICE, PURCHASE ASSISTANCE METHOD, AND PURCHASE ASSISTANCE PROGRAM
The purpose of the present invention is to collectively provide a user with a plurality of plant components configuring a fluid conveyance system. A purchase assistance device (1) comprises: a condition input assistance unit (31) that acquires a required function and a required specification as selection conditions; a standard system configuration generation unit (32) that identifies, from a standard component database (21) and on the basis of the selection conditions, a plurality of standard components configuring a fluid conveyance system, and generates a standard system configuration diagram in which the plurality of identified standard components are joined together; a system component selection unit (34) that selects, from a supplier component database (22), one or more supplier components for each standard component configuring the standard system configuration diagram; and a selection candidate generation unit (35) that generates, on the basis of the selected supplier components, at least one system configuration candidate which is a combination of the supplier components configuring the fluid conveyance system, and transmits the same to a client terminal.
The present invention comprises: second gas piping that is connected to first gas piping for guiding first combustible gas from a first supply source to a gas-using device, the second gas piping guiding second combustible gas from a second supply source to the gas-using device via the first gas piping; two gas cutoff valves that are positioned in the second gas piping; vent piping that is connected to a position on the second gas piping between the two gas cutoff valves; a vent valve that is positioned in the vent piping; and a pressure gauge that reports the pressure within vent pressure control piping in the vent piping. When the two gas cutoff valves are closed, the vent valve operates so that the pressure within the vent pressure control piping is less than the supply pressure of the first combustible gas supplied by the first supply source to the first gas piping and the supply pressure of the second combustible gas supplied by the second supply source to the second gas piping, and is greater than atmospheric pressure.
This gas turbine cogeneration system comprises: a gas turbine including a combustor; an exhaust heat recovery boiler for generating boiler steam with exhaust gas exhausted from the gas turbine as a heat source; a water recovery device for recovering moisture from the exhaust gas by heat exchange between refrigerant water and the exhaust gas exhausted from the exhaust heat recovery boiler; and a fuel gas generation facility for generating gas turbine fuel gas to be supplied to the combustor, with industrial water (recovered water and supply water) including recovered water recovered by the water recovery device as at least one of raw materials.
F02C 7/22 - Systèmes d'alimentation en combustible
F02C 6/18 - Utilisation de la chaleur perdue dans les ensembles fonctionnels de turbines à gaz à l'extérieur des ensembles eux-mêmes, p. ex. ensembles fonctionnels de chauffage à turbine à gaz
F23R 3/28 - Chambres de combustion à combustion continue utilisant des combustibles liquides ou gazeux caractérisées par l'alimentation en combustible
90.
BIOMASS GASIFICATION FURNACE, LIQUID FUEL PRODUCTION EQUIPMENT, AND METHOD FOR OPERATING BIOMASS GASIFICATION FURNACE
Provided is a biomass gasification furnace capable of preventing clinker from adhering to the inner walls of the gasification furnace body. The biomass gasification furnace is equipped with a gasification furnace body (2) that is a cylindrical body having a center axis line (CL) in the vertical direction and that gasifies a biomass raw material within, a screw feeder (3) that introduces the biomass raw material into the gasification furnace body (2), and a gasification agent introduction pipe (5), provided below the screw feeder (3), that introduces the gasification agent into the gasification furnace body (2) so that a swirling flow is formed around the center axis line (CL).
The present invention has: a tool electrode that is cylindrical around the tool axis and that forms an electrolytic solution passage on the inner circumferential side thereof; and an insulating layer that is formed on the outer circumferential surface of the cylindrical tool electrode. The electrolytic solution passage has: an outlet that is formed at the end on a first side, among the first side and a second side in the axis direction in which the tool axis extends, within the tool electrode; and a diameter expansion portion in which the inner diameter thereof increases gradually toward the first side. The end on the first side in the diameter expansion portion is said outlet.
Provided are: a boiler control device that estimates a fuel heat value and stably operates a boiler; a boiler; a boiler control method; and a boiler control program. A boiler control device (50) that controls a boiler comprises: a state quantity acquisition unit (51) that acquires a state quantity of a boiler; and a calculation unit (52) that calculates the fuel heat value, which is the heat value of fuel fed to the boiler, on the basis of the state quantity of the boiler and the boiler efficiency set in advance in the boiler control device (50). If the change quantity of the fuel heat value calculated by the calculation unit (52) satisfies a prescribed condition, the boiler control device performs control to correct the flow rate of fuel fed to the boiler using the fuel heat value.
Provided is a drift structure, a crusher, and a method for assembling a crusher with which the frequency of maintenance can be reduced. Provided is a drift structure (60) for drifting a conveyance gas blown up from below, inside a housing (11) of a crusher, the drift structure comprising a drift member (70) having a block shape. The drift member (70) has a downward inclination surface (71) extending obliquely upward toward a central axis extending in the vertical direction of the housing (11), and onto which the conveyance gas is blown, and a hanging part (76) that is hung on a hook part (93) provided on the inner wall of the housing (11).
B02C 15/04 - Appareils comportant des cylindres serrés, montés pendulairement, p. ex. serrés par des ressorts
B02C 23/26 - Passage de gaz au travers de la zone de broyage ou de désagrégation caractérisé par l'endroit où le gaz est introduit ou évacué ou par le chemin suivi par le gaz
The present application relates to a fuel gas supply device for supplying fuel gas to a plurality of fuel nozzles provided in a combustor of a gas turbine. This device is provided with: a shutoff valve provided upstream of a plurality of flow rate regulating valves for regulating a flow rate of fuel gas to be supplied to each fuel nozzle; a shutoff-valve bypassing valve provided in a bypass line provided to bypass the shutoff valve; and a control device for controlling an upstream side pressure of the flow rate regulating valve. In a normal operation time, the shutoff-valve bypassing valve is closed while the shutoff valve is opened, whereby an upstream side pressure is controlled by a supply pressure of a fuel gas supply source. In at least one of an ignition time and a speed raising time of a gas turbine, the shutoff-valve bypassing valve is opened while the shutoff valve is closed, whereby an upstream side pressure is controlled to be lower compared to the normal operation time.
F02C 3/22 - Ensembles fonctionnels de turbines à gaz caractérisés par l'utilisation de produits de combustion comme fluide de travail utilisant un combustible, un oxydant ou un fluide de dilution particulier pour produire les produits de combustion le combustible ou l'oxydant étant gazeux aux température et pression normales
F02C 7/22 - Systèmes d'alimentation en combustible
F02C 9/28 - Systèmes de régulation sensibles aux paramètres ambiants ou à ceux de l'ensemble fonctionnel, p. ex. à la température, à la pression, à la vitesse du rotor
F02C 9/40 - Commande de l'alimentation en combustible spécialement adaptée à l'utilisation d'un combustible particulier ou de plusieurs combustibles
The present disclosure relates to a fuel oil supply device for supplying fuel oil to a combustor of a gas turbine. The fuel oil supply device is provided with: a pump for supplying fuel oil; a supply pressure control valve disposed downstream of the pump and used for controlling the pressure of the fuel oil supplied by the pump; and a plurality of flow rate controlling valves disposed downstream of the supply pressure regulating valve and used for controlling the flow rates of the fuel oil supplied to a plurality of fuel nozzles provided in a combustor. Further, a plurality of cavitation suppressing parts are provided downstream of the plurality of flow rate controlling valves. The openings of the flow rate regulating valves are controlled on the basis of the first pressure of the fuel oil upstream of the flow rate controlling valves, the second pressure of the fuel oil downstream of the flow rate controlling valves, and the flow rates of the fuel oil supplied to the fuel nozzles.
F02C 9/28 - Systèmes de régulation sensibles aux paramètres ambiants ou à ceux de l'ensemble fonctionnel, p. ex. à la température, à la pression, à la vitesse du rotor
This gas turbine control device comprises: a fuel flow rate command value calculation unit; and a fuel flow rate control unit. The fuel flow rate command value calculation unit calculates a fuel flow rate command value by means of proportional integration control based on the deviation between a gas turbine rotation number and a target rotation number, or the deviation between a gas turbine output and a target output load. The fuel flow rate control unit controls the flow rate of a fuel with respect to a gas turbine on the basis of the fuel flow rate command value. The fuel flow rate command value calculation unit calculates the fuel flow rate command value so that the output of the gas turbine in a first output band increases at a first rate of change, and calculates the fuel flow rate command value so that the output of the gas turbine in a second output band which is higher than the first output band increases at a second rate of change which is smaller than the first rate of change. Further, an integration gain in the first output band of the proportional integration control is set to be smaller than an integration gain in the second output band.
F02C 9/28 - Systèmes de régulation sensibles aux paramètres ambiants ou à ceux de l'ensemble fonctionnel, p. ex. à la température, à la pression, à la vitesse du rotor
An operation method for a gas turbine according to one embodiment is for a gas turbine provided with a combustor that has a main nozzle and a pilot nozzle and that is capable of using, as fuel, hydrogen and a fuel other than hydrogen. In the operation method for the gas turbine according to said one embodiment, with regard to the ratio of the hydrogen co-combustion rate of the fuel injected from the pilot nozzle to the hydrogen co-combustion rate of the fuel injected from the main nozzle, when compared with a first ratio during operation at a low hydrogen co-combustion rate, a second ratio during operation at a high hydrogen co-combustion rate, during which the hydrogen co-combustion rate is higher than that during the operation at the low hydrogen co-combustion rate, is higher.
A method for operating a gas turbine according to one embodiment is for operating a gas turbine including a combustor that can use hydrogen and a fuel other than hydrogen as fuel. This combustor includes a nozzle having at least one first injection hole and at least one second injection hole. When performing low hydrogen co-firing rate operation, a first fuel is injected from the at least one first injection hole, and when performing high hydrogen co-firing rate operation, in which the hydrogen co-firing rate is higher than in the low hydrogen co-firing rate operation, a second fuel having a higher hydrogen content than the first fuel is injected from the at least one first injection hole, and water is injected from the second injection hole.
This turbine blade comprises: a blade wall; and an insert inserted in a space formed inside the blade wall. An internal cavity that is in communication with the outside of the turbine blade is formed inside the insert, and a plurality of protrusions protruding toward the inner surface of the blade wall are formed on the outer surface of the insert. Between two adjacent protrusions among the plurality of protrusions, a recovery space that is in communication with the outside of the turbine blade is defined. Each of the plurality of protrusions has formed therein a flow channel which is in communication with the internal cavity and at least one cooling hole which is in communication with the flow channel and which is opened so as to face the inner surface of the blade wall. When the length of the flow channel in a direction in which the plurality of protrusions are arrayed side by side is defined as the width of the flow channel, the width of the flow channel at a position where the flow channel is connected to the cooling hole is denoted by b, and the inner diameter of the cooling hole is denoted by d, b/d≥1.2 is satisfied.
F01D 9/02 - InjecteursLogement des injecteursAubes de statorTuyères de guidage
F01D 5/18 - Aubes creusesDispositifs de chauffage, de protection contre l'échauffement ou de refroidissement des aubes
F01D 25/00 - Parties constitutives, détails ou accessoires non couverts dans les autres groupes ou d'un intérêt non traité dans ces groupes
F02C 7/00 - Caractéristiques, parties constitutives, détails ou accessoires non couverts dans, ou d'un intérêt plus général que, les groupes Entrées d'air pour ensembles fonctionnels de propulsion par réaction
F02C 7/18 - Refroidissement des ensembles fonctionnels caractérisé par l'agent refroidisseur l'agent refroidisseur étant gazeux, p. ex. l'air
This turbine blade comprises a blade wall and an insert inserted in a space formed inside the blade wall. Inside the insert, an inner cavity communicating with the outside of the turbine blade is formed. On the outer surface of the insert, a plurality of projections projecting toward the inner surface of the blade wall are formed. Between two adjacent projections among the plurality of projections, a collection space communicating with the outside of the turbine blade is defined. Formed in each of the plurality of projections are a flow path communicating with the inner cavity, and at least one cooling hole that is open so as to communicate with the flow path and face the inner surface of the blade wall. On at least one cross section of the turbine blade vertical to the blade height direction of the turbine blade between the tip-side edge and the hub-side edge of the turbine blade, given that the length of at least one projection is defined as the length of at least one projection among the plurality of projections extending from the outer surface of the insert toward the inner surface of the blade wall, that the length of at least one projection is L, and that the inner diameter of at least one cooling hole formed in at least one projection is d, L > 5d is satisfied.
