公开(公告)号：US20240280265A1

公开(公告)日：2024-08-22

申请号：US18452958

申请日：2023-08-21

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Nayan Vinod Patel ,  Michael A. Benjamin

IPC: F23R3/34 ,  F02C7/22 ,  F23R3/06 ,  F23R3/14 ,  F23R3/28 ,  F23R3/36

CPC classification number: F23R3/06 ,  F23R3/34 ,  F02C7/22 ,  F23R3/14 ,  F23R3/28 ,  F23R3/346 ,  F23R3/36

Abstract: A turbine engine can include a compressor section, a combustion section, and a turbine section in serial flow arrangement. A combustor in the combustion section can include a combustion chamber, a fuel supply fluidly coupled to the combustion chamber, and a fuel nozzle assembly. The fuel nozzle assembly can include an air flow passage and a fuel flow passage.

公开(公告)号：US12215869B2

公开(公告)日：2025-02-04

申请号：US18452958

申请日：2023-08-21

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Nayan Vinod Patel ,  Michael A. Benjamin

IPC: F23R3/06 ,  F23R3/14 ,  F23R3/34 ,  F23R3/36 ,  F02C7/22 ,  F23R3/28

Abstract: A turbine engine can include a compressor section, a combustion section, and a turbine section in serial flow arrangement. A combustor in the combustion section can include a combustion chamber, a fuel supply fluidly coupled to the combustion chamber, and a fuel nozzle assembly. The fuel nozzle assembly can include an air flow passage and a fuel flow passage.

公开(公告)号：US11774100B2

公开(公告)日：2023-10-03

申请号：US17725895

申请日：2022-04-21

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Nayan Vinod Patel ,  Michael A. Benjamin

IPC: F23R3/34 ,  F23R3/14 ,  F23R3/36 ,  F23R3/06 ,  F02C7/22 ,  F23R3/28

CPC classification number: F23R3/34 ,  F23R3/06 ,  F23R3/14 ,  F23R3/36 ,  F02C7/22 ,  F23R3/28 ,  F23R3/346

Abstract: A turbine engine can include a compressor section, a combustion section, and a turbine section in serial flow arrangement. A combustor in the combustion section can include a combustion chamber, a fuel supply fluidly coupled to the combustion chamber, and a fuel nozzle assembly. The fuel nozzle assembly can include an air flow passage and a fuel flow passage.

公开(公告)号：US20230228424A1

公开(公告)日：2023-07-20

申请号：US17725895

申请日：2022-04-21

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Nayan Vinod Patel ,  Michael A. Benjamin

IPC: F02C7/22 ,  F02C3/04 ,  F23R3/14 ,  F23R3/28 ,  F23R3/36

CPC classification number: F02C7/22 ,  F02C3/04 ,  F23R3/14 ,  F23R3/28 ,  F23R3/36 ,  F05D2220/30 ,  F05D2240/35

Abstract: A turbine engine can include a compressor section, a combustion section, and a turbine section in serial flow arrangement. A combustor in the combustion section can include a combustion chamber, a fuel supply fluidly coupled to the combustion chamber, and a fuel nozzle assembly. The fuel nozzle assembly can include an air flow passage and a fuel flow passage.