-
公开(公告)号：US11747018B2
公开(公告)日：2023-09-05
申请号：US17587169
申请日：2022-01-28
Applicant: General Electric Company
Inventor： Perumallu Vukanti , Varun S. Lakshmanan , Michael T. Bucaro , Pradeep Naik , Steven C. Vise , Michael A. Benjamin
CPC classification number: F23R3/06 , F23R3/16 , F23R3/28 , F23R2900/03044
Abstract: A gas turbine engine including a compressor section and a combustion section in serial flow arrangement along an engine centerline, the combustion section having a combustor liner, a dome wall coupled to the combustor liner, and a dome inlet located in the dome wall, a fuel injector fluidly coupled to the dome inlet, a combustion chamber fluidly coupled to the fuel injector and defined at least in part by the combustor liner and the dome wall, and at least one set of dilution openings located in the dome wall and fluidly coupled to the combustion chamber.
-
公开(公告)号：US20230266009A1
公开(公告)日：2023-08-24
申请号：US17734469
申请日：2022-05-02
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Pradeep Naik , Manampathy G. Giridharan , Ajoy Patra , Perumallu Vukanti , R Narasimha Chiranthan
CPC classification number: F23R3/286 , F23R3/002 , F02C7/22 , F05D2240/35
Abstract: A turbine engine can include a compressor section, a combustion section, and a turbine section in axial flow arrangement. The combustion section can include a combustor having a fuel-air mixer. The fuel-air mixer can include a body with at least an air passage, as well as a set of mixing passages.
-
公开(公告)号：US11725819B2
公开(公告)日：2023-08-15
申请号：US17682373
申请日：2022-02-28
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.
-
公开(公告)号：US20230204214A1
公开(公告)日：2023-06-29
申请号：US17586082
申请日：2022-01-27
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Manampathy G. Giridharan , Ajoy Patra , Pradeep Naik , R Narasimha Chiranthan , Perumallu Vukanti , Michael T. Bucaro
CPC classification number: F23R3/286 , F23D14/583 , F23D14/62
Abstract: A turbine engine that includes an engine core having at least a compressor section and a combustion section. The combustion section includes a combustor. The combustor section or combustor includes a fuel-air mixing assembly fluidly coupled to the compressor section. The fuel-air mixing assembly includes an outer wall, a center body at least partially circumscribed by the outer wall, and an annular flow passage between the outer wall and center body. At least one fuel orifice includes a fuel outlet fluidly coupled to the annular flow passage.
-
25.发明公开公开(公告)号：US20230194093A1
公开(公告)日：2023-06-22
申请号：US17717739
申请日：2022-04-11
Applicant: General Electric Company
Inventor： Michael T. Bucaro , Ajoy Patra , Pradeep Naik , Perumallu Vukanti , R Narasimha Chiranthan , Clayton S. Cooper , Michael A. Benjamin , Steven C. Vise , Manampathy G. Giridharan , Krishnakumar Venkatesan
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. The fuel nozzle can include both a primary and secondary fuel passage, and an additional air passage to provide for greater flame control, fuel provision, or local fuel and air mixing prior to combustion.
-
Patent Agency Ranking
公开(公告)号：US20230194092A1
公开(公告)日：2023-06-22
申请号：US17682510
申请日：2022-02-28
Applicant: General Electric Company
Inventor： Pradeep Naik , Perumallu Vukanti , Michael T. Bucaro , Steven C. Vise , Ajoy Patra , R Narasimha Chiranthan , Manampathy G. Giridharan , Michael A. Benjamin , Clayton S. Cooper , Dharmaraj Pachaiappan
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. Increasing efficiency and meeting emission needs can be met with the use of alternative fuels, which combust at higher temperatures or higher speeds than traditional fuels, requiring improved fuel introduction without the occurrence of flame holding or flashback.
-
公开(公告)号：US20230175695A1
公开(公告)日：2023-06-08
申请号：US17653399
申请日：2022-03-03
Applicant: General Electric Company
Inventor： Rimple Rangrej , Saket Singh , Pradeep Naik , Ajoy Patra
IPC: F23R3/06
CPC classification number: F23R3/06
Abstract: A combustor for a turbomachine engine includes a combustion chamber, a liner forming a boundary of the combustion chamber, and multiple dilution holes through the liner to permit airflow into the combustion chamber. The dilution holes include converging dilution holes and diverging dilution holes, the converging dilution holes having a converging cross-sectional profile and the diverging dilution holes having a diverging cross-sectional profile.
-
公开(公告)号：US11635209B2
公开(公告)日：2023-04-25
申请号：US17649128
申请日：2022-01-27
Applicant: General Electric Company
Inventor： Perumallu Vukanti , Pradeep Naik , Sripathi Mohan , Karthikeyan Sampath , Steven C. Vise , Shai Birmaher , Saket Singh
Abstract: A swirler assembly includes a swirler having a primary swirler and a secondary swirler, and a flare connected the secondary swirler, and a dome disposed radially outward of the flare. A flare oxidizer flow passage is defined by a flare outer surface and a dome inner surface, and the flare oxidizer flow passage includes a swirl inducing member therewithin that induces a swirled flow of an oxidizer passing through the flare oxidizer flow passage into a combustion chamber.
-
公开(公告)号：US20230053389A1
公开(公告)日：2023-02-23
申请号：US17649128
申请日：2022-01-27
Applicant: General Electric Company
Inventor： Perumallu Vukanti , Pradeep Naik , Sripathi Mohan , Karthikeyan Sampath , Steven C. Vise , Shai Birmaher , Saket Singh
Abstract: A swirler assembly includes a swirler having a primary swirler and a secondary swirler, and a flare connected the secondary swirler, and a dome disposed radially outward of the flare. A flare oxidizer flow passage is defined by a flare outer surface and a dome inner surface, and the flare oxidizer flow passage includes a swirl inducing member therewithin that induces a swirled flow of an oxidizer passing through the flare oxidizer flow passage into a combustion chamber.
-
公开(公告)号：US20220325891A1
公开(公告)日：2022-10-13
申请号：US17228433
申请日：2021-04-12
Applicant: General Electric Company
Inventor： Vishal Sanjay Kediya , Pradeep Naik , Ajoy Patra , Narasimhan S. Sahana
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.
-
-
-
-
-
-
-
-
-
Search Results
230
records
(took 0.026 seconds)
