COMBUSTOR NOZZLE, COMBUSTOR, AND GAS TURBINE INCLUDING SAME

    公开(公告)号:EP4459187A1

    公开(公告)日:2024-11-06

    申请号:EP24172973.0

    申请日:2024-04-29

    发明人: Shershnyov, Borys

    IPC分类号: F23R3/28

    摘要: A combustor nozzle (1400), a combustor including the combustor nozzle (1400), and a gas turbine including the combustor are disclosed. The combustor nozzle (1400) may include a plurality of mixing tubes (1420) through which air and fuel flow, a multi-tube (1410) into which the mixing tubes (1420) are inserted, the multi-tube (1410) supporting the mixing tubes (1420), a fuel tube (1450) formed inside the multi-tube (1410) and through which fuel flows, a tip plate (1415) coupled to a tip of the multi-tube (1410), a front plate (1430) spaced apart from the tip plate (1415), the front plate (1430) forming a cooling space (CP1), and a dispersion plate (1470) spaced apart from the front plate (1430) and connected to the fuel tube (1450), the dispersion plate (1470) forming a dispersion space (DP1) in which fuel discharged from the fuel tube (1450) is diffused.

    ROTOR ASSEMBLY FOR A GAS TURBINE, GAS TURBINE AND METHOD FOR ASSEMBLING A ROTOR ASSEMBLY

    公开(公告)号:EP4411111A1

    公开(公告)日:2024-08-07

    申请号:EP23214796.7

    申请日:2023-12-07

    发明人: LEE, Han Min

    IPC分类号: F01D5/32

    摘要: A rotor assembly and a gas turbine (1000) including the same are proposed. The rotor assembly includes blade fastening assembly (2000) including a fastening key (2100) having a through hole (2111), a rotor disk (1120) including a disk slot (1321) into which a root member (1313) is inserted, the rotor disk (1120) having a first groove (2001) with a shape corresponding to a portion of the fastening key (2100), and a pin groove (2003) connected with the first groove (2001), a platform (1312) having a second groove (2002) formed in communication with the first groove (2001) and forming a shape corresponding to a remaining portion of the fastening key (2100) in a state of being inserted into the disk slot (1321), and a fastening pin (2200) inserted into the threaded hole (2111) and the pin groove (2003). Further a method for assembling the rotor assembly is proposed.

    NOZZLE ASSEMBLY, COMBUSTOR, AND GAS TURBINE INCLUDING SAME

    公开(公告)号:EP4394251A1

    公开(公告)日:2024-07-03

    申请号:EP24150056.0

    申请日:2024-01-02

    发明人: Shershnyov, Borys

    IPC分类号: F23R3/14 F23R3/28

    CPC分类号: F23R3/286 F23R3/14

    摘要: A nozzle assembly, a combustor (100) using the same, and a gas turbine . The nozzle assembly is configured to inject fuel and compressed air into a combustion chamber of a combustor of a gas turbine, and includes a hollow nozzle frame (1410) , a mixture supply tube (1420) having a plurality of tubes (1421) configured to supply a mixture of air and fuel to the combustion chamber, a fuel supply part (1440) configured to supply fuel to the mixture supply tube, an air supply part (1440) configured to supply air to the mixture supply tube, and a mixing part (1450) including an injection member (1451) formed in each of the tubes and configured to inject fuel supplied from the fuel supply part toward air passing through the tube, and a swirl vane (1452) formed on one side of the injection member and configured to mix fuel and air passing through the injection member.

    DEVICE AND METHOD FOR DEGRADATION PREDICTION

    公开(公告)号:EP4361949A1

    公开(公告)日:2024-05-01

    申请号:EP23203037.9

    申请日:2023-10-11

    IPC分类号: G06T7/00

    摘要: Disclosed is a degradation prediction device predicting a lifetime of a target material, including: at least one processor, and the at least one processor is configured to train a degradation index prediction model based on the representative value of a degradation index of a material by environmental conditions and the environmental information of a material subjected to a destructive testing, train a LMP (Larson-Miller Parameter) value prediction model based on the representative value of a degradation index of a material by environmental conditions and a theoretical value of LMP at a destructive testing, predict a degradation index for a target material using the degradation index prediction model for which training is completed based on environmental information of the target material and predict a LMP value of the target material using the LMP value prediction model for which training is completed based on the predicted degradation index.

    COMBINED REFORMER
    7.
    发明公开
    COMBINED REFORMER 审中-公开

    公开(公告)号:EP4309779A1

    公开(公告)日:2024-01-24

    申请号:EP23185821.8

    申请日:2023-07-17

    IPC分类号: B01J8/04 B01J8/06

    摘要: The present disclosure provides a combined reformer capable of continuously performing different reforming reactions by sequentially supplying heat from the combustion gas to the two or more catalyst tubes that react at different temperatures. Also, the present disclosure provides a combined reformer capable of enhancing the reforming efficiency with a U-shaped first catalyst tube including a preheating section where the hydrocarbon gas is preheated, flowing parallel to the combustion gas, and a reforming section where the catalytic reforming takes place.

    COMBUSTOR NOZZLE, COMBUSTOR, AND GAS TURBINE INCLUDING THE SAME

    公开(公告)号:EP4230914A2

    公开(公告)日:2023-08-23

    申请号:EP23157302.3

    申请日:2023-02-17

    发明人: SHERSHNYOV, Borys

    IPC分类号: F23R3/28 F23R3/16

    摘要: Disclosed herein is a nozzle(1400) for a combustor(1200) that burns fuel containing hydrogen, which includes a plurality of mixing tubes(1420) through which air and fuel flow, a multi-tube(1410) configured to contain and support the mixing tubes(1420), a fuel tube(1450) formed inside the multi-tube(1410) and through which fuel flows, a tip plate(1415) coupled to a tip of the multi-tube(1410), and a front plate(1460, 2460, 3460) spaced apart from the tip plate(1415) to define a cooling space(CS1).

    COMBINED POWER GENERATION SYSTEM AND DRIVING METHOD THEREOF

    公开(公告)号:EP4230847A1

    公开(公告)日:2023-08-23

    申请号:EP23156285.1

    申请日:2023-02-13

    IPC分类号: F01K23/10 C01B3/04

    摘要: A combined power generation system includes a gas turbine, a heat recovery steam generator (HRSG) configured to heat feedwater using combustion gases discharged from the gas turbine and having a high-pressure section, a medium-pressure section, and a low-pressure section having different pressure levels, an ammonia decomposer decomposing ammonia with the combustion gases discharged from the gas turbine, a first exhaust gas line through which the exhaust gases discharged from the gas turbine are transferred to the HRSG, a second exhaust gas line through which the exhaust gases discharged from the gas turbine are transferred to the ammonia decomposer, a third exhaust gas line through which the exhaust gases discharged from the ammonia decomposer are transferred to the HRSG, and a decomposed gas transfer tube connecting the ammonia decomposer and the gas turbine of a combustor to transfer decomposed gases generated with the decomposition of ammonia to the combustor.

    COMBINED POWER GENERATION SYSTEM AND DRIVING METHOD THEREOF

    公开(公告)号:EP4227501A1

    公开(公告)日:2023-08-16

    申请号:EP22210743.5

    申请日:2022-12-01

    摘要: A combined power generation system (101, 102, 103, 104) includes a gas turbine (20), a heat recovery steam generator (50) (HRSG) generating steam using combustion gas from the gas turbine (20), a vaporizer (73) vaporizing liquefied ammonia, an ammonia decomposer section (30) decomposing ammonia with the combustion gas, a first exhaust gas line (27) through which exhaust gas from the gas turbine (20) is transferred to the HRSG (50), a steam turbine (40) generating a rotational force with the steam from the HRSG (50), a decomposed gas supply line (34) through which decomposed gases generated in the ammonia decomposer section (30) are supplied to a combustor (23), and a cold heat transfer line (62) absorbing cold heat of the liquefied ammonia and supply the cold heat to the condenser section (60), and a condenser section (60) condensing the steam from the steam turbine (20).