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公开(公告)号：US20240200778A1
公开(公告)日：2024-06-20
申请号：US18104408
申请日：2023-02-01
Applicant: General Electric Company
Inventor： Perumallu Vukanti , Pradeep Naik , R Narasimha Chiranthan , Ajoy Patra , Arijit Sinha Roy , Pabitra Badhuk , Aritra Chakraborty , Bhavya Naidu Panduri , Michael T. Bucaro , Sibtosh Pal
Abstract: A combustor comprising a dome wall, an annular liner, a combustion chamber, a set of fuel cups, and a set of dilution passages for each fuel cup of the set of fuel cups. The set of fuel cups circumferentially spaced along the dome wall relative to the combustor centerline. The set of dilution passages terminating in a plurality of slots spaced about the corresponding fuel cup in the set of fuel cups.
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公开(公告)号：US20240200777A1
公开(公告)日：2024-06-20
申请号：US18104433
申请日：2023-02-01
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Pabitra Badhuk , Michael T. Bucaro , Pradeep Naik , Perumallu Vukanti , Arijit Sinha Roy , Sibtosh Pal , Bhavya Naidu Panduri , Aritra Chakraborty , Ajoy Patra , R Narasimha Chiranthan , Michael A. Benjamin
Abstract: A combustor comprising a dome wall, an annular liner, a combustion chamber, a set of fuel cups, and a set of dilution passages for each fuel cup of the set of fuel cups. The set of fuel cups circumferentially spaced along the dome wall relative to the combustor centerline. The set of dilution passages terminating in a plurality of slots spaced about the corresponding fuel cup in the set of fuel cups.
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公开(公告)号：US12007114B1
公开(公告)日：2024-06-11
申请号：US18187359
申请日：2023-03-21
Applicant: General Electric Company
Inventor： Perumallu Vukanti , Sibtosh Pal , Pradeep Naik , R Narasimha Chiranthan , Ajoy Patra , Michael T. Bucaro , Aritra Chakraborty , Arijit Sinha Roy , Pabitra Badhuk , Bhavya Naidu Panduri
IPC: F23R3/06
CPC classification number: F23R3/06
Abstract: A gas turbine engine includes a compressor section, a combustor section, and a turbine section in fore-to-aft serial flow arrangement and defines an engine centerline. The combustor section includes a combustor liner at least partially defining a combustor chamber and a dome wall, coupled to the combustor liner, and defining a forward end of the combustion chamber. A first fuel nozzle is located on the dome wall and fluidly coupled to the combustion chamber. A first set of compressed air openings emit compressed air into the combustion chamber along a first flow path and a second set of compressed air openings emit compressed air into the combustion chamber along a second flow path. The first and second flow paths intersect at an intersection point to form a sheet of air.
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公开(公告)号：US11994291B2
公开(公告)日：2024-05-28
申请号：US18060808
申请日：2022-12-01
Applicant: General Electric Company
Inventor： Hiranya Nath , Ravindra Shankar Ganiger , Ajoy Patra , Rajendra Wankhade
CPC classification number: F23R3/002 , F23R3/16 , F23R3/46 , F05D2220/32 , F05D2240/35
Abstract: An annular combustor includes a combustion liner defining a combustion chamber, the combustion liner having an outer liner and an inner liner and a plurality of dimples in the combustion liner. The combustion liner is characterized by a performance factor greater than or equal to one and less than or equal to seven. An engine includes the annular combustor.
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公开(公告)号：US20240102653A1
公开(公告)日：2024-03-28
申请号：US18529428
申请日：2023-12-05
Applicant: General Electric Company
Inventor： Saket Singh , Ravindra Shankar Ganiger , Hiranya Nath , Perumallu Vukanti , Ajoy Patra , Karthikeyan Sampath , Pradeep Naik , Rimple Rangrej , Veera Venkata Amarnath Manem
CPC classification number: F23R3/002 , F23R3/60 , F23R2900/00017 , F23R2900/03043
Abstract: A dome-deflector assembly for a gas turbine includes a dome, a deflector, and at least one dome-deflector connecting assembly that includes a connecting member connecting the dome and the deflector together with a cavity being defined between the dome and the deflector. The connecting member extends through the deflector and has a first end arranged at a hot surface side of the deflector and a second end arranged to connect with the dome. The dome-deflector connecting assembly is configured to provide a flow of cooling air from the cavity to the hot surface side of the deflector to cool the first end of the connecting member on the hot surface side of the deflector.
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Patent Agency Ranking
公开(公告)号：US20240053012A1
公开(公告)日：2024-02-15
申请号：US18494322
申请日：2023-10-25
Applicant: General Electric Company
Inventor： Vishal Sanjay Kediya , Pradeep Naik , Ajoy Patra , Narasimhan S. Sahana
CPC classification number: F23R3/10 , F02C3/00 , F05D2240/35 , F05D2220/32
Abstract: A combustor for a gas turbine engine has an annular inner liner and an annular outer liner forming a combustion chamber therebetween. A dilution horn pair includes dilution horns that provide a flow of an oxidizer gas into the combustion chamber in a dilution zone. At least one of the dilution horns forming the dilution horn pair is arranged so as to provide a lateral flow component of the flow of oxidizer gas therethrough into the combustion chamber, the lateral flow component having a flow direction extending laterally across and non-orthogonal to an axial flow direction of combustion gases within the combustion chamber.
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公开(公告)号：US11846419B2
公开(公告)日：2023-12-19
申请号：US17810678
申请日：2022-07-05
Applicant: General Electric Company
Inventor： Saket Singh , Ravindra Shankar Ganiger , Hiranya Nath , Perumallu Vukanti , Ajoy Patra , Karthikeyan Sampath , Pradeep Naik , Rimple Rangrej , Veera Venkata Amarnath Manem
CPC classification number: F23R3/002 , F23R3/60 , F23R2900/00017 , F23R2900/03043
Abstract: A dome-deflector assembly for a gas turbine includes a dome, a deflector, and at least one dome-deflector connecting assembly that includes a connecting member connecting the dome and the deflector together with a cavity being defined between the dome and the deflector. The connecting member extends through the deflector and has a first end arranged at a hot surface side of the deflector and a second end arranged to connect with the dome. The dome-deflector connecting assembly is configured to provide a flow of cooling air from the cavity to the hot surface side of the deflector to cool the first end of the connecting member on the hot surface side of the deflector.
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公开(公告)号：US20230366551A1
公开(公告)日：2023-11-16
申请号：US18350205
申请日：2023-07-11
Applicant: General Electric Company
Inventor： Perumallu Vukanti , Pradeep Naik , Clayton S. Cooper , Michael A. Benjamin , Michael T. Bucaro , Manampathy G. Giridharan , Steven C. Vise , Ajoy Patra , Saket Singh , R Narasimha Chiranthan
Abstract: An engine can utilize a combustor to combust fuel to drive the engine. A fuel nozzle assembly can supply fuel to the combustor for combustion or ignition of the fuel. The fuel nozzle assembly can include a swirler and a fuel nozzle to supply a mixture of fuel and air for combustion, which can supply a primary fuel supply and a secondary fuel supply. Increasing efficiency and reducing emission require the use of alternative fuels, which combust at higher temperatures or burn at faster burn speeds than traditional fuels, requiring improved fuel introduction without the occurrence of flame holding or flashback.
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公开(公告)号：US20230288065A1
公开(公告)日：2023-09-14
申请号：US17810678
申请日：2022-07-05
Applicant: General Electric Company
Inventor： Saket Singh , Ravindra Shankar Ganiger , Hiranya Nath , Perumallu Vukanti , Ajoy Patra , Karthikeyan Sampath , Pradeep Naik , Rimple Rangrej , Veera Venkata Amarnath Manem
CPC classification number: F23R3/002 , F23R3/60 , F23R2900/00017 , F23R2900/03043
Abstract: A dome-deflector assembly for a gas turbine includes a dome, a deflector, and at least one dome-deflector connecting assembly that includes a connecting member connecting the dome and the deflector together with a cavity being defined between the dome and the deflector. The connecting member extends through the deflector and has a first end arranged at a hot surface side of the deflector and a second end arranged to connect with the dome. The dome-deflector connecting assembly is configured to provide a flow of cooling air from the cavity to the hot surface side of the deflector to cool the first end of the connecting member on the hot surface side of the deflector.
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公开(公告)号：US20230235884A1
公开(公告)日：2023-07-27
申请号：US17685883
申请日：2022-03-03
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Pradeep Naik , Manampathy G. Giridharan , Michael T. Bucaro , Ajoy Patra , Perumallu Vukanti , R Narasimha Chiranthan , Gregory A. Boardman
CPC classification number: F23R3/002 , F02C3/04 , F05D2240/35
Abstract: A turbine engine can include a compressor section, a combustion section, and a turbine section in serial flow arrangement. The combustion section can have a combustor with a combustor liner at least partially defining a combustion chamber, as well as a fuel-air mixer including at least one set of mixing tubes.
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