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公开(公告)号：US20230324048A1
公开(公告)日：2023-10-12
申请号：US18085781
申请日：2022-12-21
Applicant: General Electric Company
Inventor： Owen Graham , Sharath Nagaraja , Nicholas Magina , Fei Han , Kwanwoo Kim
CPC classification number: F23R3/26 , F23R3/002 , F23R3/04 , F23R3/10 , F23R3/28 , F02C7/18 , F05D2240/35
Abstract: The systems and methods described herein relate to a dome of a gas turbine assembly configured to suppress pressure pulsations. The systems and methods provide a dome having an aperture configured to surround an injector assembly of a combustor. The dome having a front panel extending radially from the aperture. The systems and methods couple a first cavity to the front panel. The first cavity includes a series of ducts. A first duct of the series of ducts is configured to receive airflow into the first cavity from a compressor and a second set of ducts of the series of ducts and a third duct of the series of ducts are configured to direct airflow to the combustor from the first cavity, wherein the third duct has a larger diameter than the second set of ducts.
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公开(公告)号：US20230194094A1
公开(公告)日：2023-06-22
申请号：US17677165
申请日：2022-02-22
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Fei Han , Ramal Janith Samarasinghe , Pradeep Naik , Krishnakumar Venkatesan , Michael T. Bucaro , Ajoy Patra , Manampathy G. Giridharan
Abstract: A turbine engine having a compressor section, a combustion section and a turbine section in serial flow arrangement. The turbine engine further having a combustor, provided within the combustion section, defining a combustion chamber and having at least one fuel injector. The fuel injector having a fuel channel, a first set of fuel orifices, and a flow restrictor located within the fuel channel and having a second set of fuel orifices.
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公开(公告)号：US10290562B2
公开(公告)日：2019-05-14
申请号：US14060262
申请日：2013-10-22
Applicant: General Electric Company
Inventor： Fei Han , Mehmet Arik , Trevor Wood , Charles Franklin Wolfe, Jr.
IPC: H01L23/467 , F21V29/63 , F21K9/23 , F21Y105/10 , F21Y115/10
Abstract: Apparatus and method are provided for reducing acoustical noise when cooling a device, such as a lamp system. The apparatus includes at least a set of a first synthetic jet and a second synthetic jet. The first and second synthetic jets are responsive to respective actuating signals having a phase difference (e.g., 180°) between one another chosen to reduce acoustic noise produced by the first and second synthetic jets when cooling the device.
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14.发明申请Systems and Methods for Measuring Temperature in a Gas Turbine Using Acoustic Interference 有权使用声学干涉测量燃气轮机温度的系统和方法公开(公告)号：US20160223410A1
公开(公告)日：2016-08-04
申请号：US14611639
申请日：2015-02-02
Applicant: General Electric Company
Inventor： Eamon P. Gleeson , Fei Han
CPC classification number: G01K11/22 , G01K13/02 , G01K2013/024
Abstract: Systems and methods for measuring temperature in a gas turbine are disclosed. The method can include directing a first acoustic signal towards a gas path in a turbine; directing a second acoustic signal towards the gas path in the turbine; receiving the first acoustic signal and the second acoustic signal at a downstream gas path location; combining the first acoustic signal and the second acoustic signal to create a combined acoustic signal, where a portion of the first acoustic signal cancels out a portion of the second acoustic signal; and determining a temperature of the gas path based at least in part on the combined acoustic signal.
Abstract translation: 公开了一种用于测量燃气轮机温度的系统和方法。 该方法可以包括将第一声信号引向涡轮机中的气体路径; 将第二声学信号引导到所述涡轮机中的气体路径; 在下游气体路径位置处接收第一声信号和第二声信号; 组合第一声信号和第二声信号以产生组合声信号，其中第一声信号的一部分抵消第二声信号的一部分; 以及至少部分地基于组合的声学信号来确定气体路径的温度。
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公开(公告)号：US20140352322A1
公开(公告)日：2014-12-04
申请号：US13908156
申请日：2013-06-03
Applicant: General Electric Company
Inventor： Qingguo Zhang , Fei Han
IPC: F23R3/28
CPC classification number: F23R3/286 , F23N5/003 , F23N2025/08 , F23N2041/20
Abstract: A turbomachine combustor is provided. The turbomachine includes a combustion chamber and multiple micro-mixer nozzles arranged concentrically within a radial combustion liner and configured to receive fuel from one or more fuel supply pipes affixed to each of the plurality of micro-mixer nozzles at an upstream face. The multiple micro-mixer nozzle are also configured to receive air from a flow sleeve surrounding the radial combustion liner. Each of the micro-mixer nozzles include an annular strip having a multiple tubes or passages extending axially from the upstream face to a downstream face of each of the micro-mixer nozzles.
Abstract translation: 提供涡轮机燃烧器。 涡轮机包括燃烧室和多个微型混合器喷嘴，其同心地布置在径向燃烧衬套内并且构造成在上游面处从固定到多个微混合器喷嘴中的每一个的一个或多个燃料供给管接收燃料。 多个微型混合器喷嘴还构造成从围绕径向燃烧衬套的流动套筒接收空气。 每个微型混合器喷嘴包括具有从每个微混合器喷嘴的上游面到下游面轴向延伸的多个管或多个管的环形条。
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Patent Agency Ranking
16.发明申请公开(公告)号：US20140124589A1
公开(公告)日：2014-05-08
申请号：US14060262
申请日：2013-10-22
Applicant: General Electric Company
Inventor： Fei Han , Mehmet Arik , Trevor Wood , Charles Franklin Wolfe, JR.
IPC: H01L23/467
CPC classification number: H01L23/467 , F21K9/23 , F21V29/63 , F21Y2105/10 , F21Y2115/10 , H01L2924/0002 , H01L2924/00
Abstract: Apparatus and method are provided for reducing acoustical noise when cooling a device, such as a lamp system. The apparatus includes at least a set of a first synthetic jet and a second synthetic jet. The first and second synthetic jets are responsive to respective actuating signals having a phase difference (e.g., 180°) between one another chosen to reduce acoustic noise produced by the first and second synthetic jets when cooling the device.
Abstract translation: 提供了用于在冷却诸如灯系统的装置时降低声学噪声的装置和方法。 该装置至少包括一组第一合成射流和第二合成射流。 第一和第二合成射流响应于相应的致动信号，其具有彼此之间的相位差（例如，180°），其被选择为在冷却装置时减少由第一和第二合成射流产生的声音噪声。
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公开(公告)号：US20210302020A1
公开(公告)日：2021-09-30
申请号：US17138048
申请日：2020-12-30
Applicant: General Electric Company
Inventor： Owen Graham , Kwanwoo Kim , Nicholas Magina , Sharath Nagaraja , Fei Han
Abstract: The systems and methods described herein relate to a dome of a gas turbine assembly configured to suppress pressure pulsations. The systems and methods provide a dome having an aperture configured to surround an injector assembly of a combustor. The dome having a front panel extending radially from the aperture. The systems and methods couple a first cavity to the front panel. The first cavity includes a series of ducts. A first duct of the series of ducts is configured to receive airflow into the first cavity from a compressor and a second set of ducts of the series of ducts and a third duct of the series of ducts are configured to direct airflow to the combustor from the first cavity, wherein the third duct has a larger diameter than the second set of ducts.
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公开(公告)号：US10941939B2
公开(公告)日：2021-03-09
申请号：US15714118
申请日：2017-09-25
Applicant: General Electric Company
Inventor： Owen Graham , Kwanwoo Kim , Nicholas Magina , Sharath Nagaraja , Fei Han
Abstract: The systems and methods described herein relate to a dome of a gas turbine assembly configured to suppress pressure pulsations. The systems and methods provide a dome having an aperture configured to surround an injector assembly of a combustor. The dome having a front panel extending radially from the aperture. The systems and methods couple a first cavity to the front panel. The first cavity includes a series of ducts. A first duct of the series of ducts is configured to receive airflow into the first cavity from a compressor and a second set of ducts of the series of ducts and a third duct of the series of ducts are configured to direct airflow to the combustor from the first cavity, wherein the third duct has a larger diameter than the second set of ducts.
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公开(公告)号：US10513984B2
公开(公告)日：2019-12-24
申请号：US14834467
申请日：2015-08-25
Applicant: General Electric Company
Inventor： Kwanwoo Kim , Fei Han , Owen Graham
IPC: F02C7/045 , F02C7/24 , F01D25/04 , F02C3/14 , F23R3/04 , F01D9/02 , F02C3/04 , F02C7/04 , F02C9/18 , F23R3/42
Abstract: In one aspect the present subject matter is directed to a system for suppressing acoustic noise within a combustion section of a gas turbine. The system includes at least one static structure disposed forward of a combustion chamber defined within the combustion section. The static structure at least partially defines a diffuser cavity upstream of the combustion chamber. A baffle plate is coupled to the static structure. The baffle plate and the static structure at least partially define an air plenum within the combustion section forward of the combustion chamber. The baffle plate includes an aperture that provides for fluid communication between the diffuser cavity and the air plenum. The at least one static structure and the baffle plate define a Helmholtz resonator within the combustion section.
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公开(公告)号：US20190162350A1
公开(公告)日：2019-05-30
申请号：US15827587
申请日：2017-11-30
Applicant: General Electric Company
Inventor： Ramal Janith Samarasinghe , Nicholas Arthur Magina , Andrew Wickersham , Arin Cross , Fei Han
Abstract: An inline fluid damper device comprises a flow-through conduit configured to be placed inside a larger exterior conduit through which a fluid flows. The flow-through conduit is elongated and extending around a center axis. The damper device also comprising an indirect flow conduit coupled with the flow-through conduit. The indirect flow conduit is also configured to be placed inside the larger exterior conduit. The flow-through conduit and the indirect flow conduit are configured to dampen one or more flow fluctuations or pressure fluctuations in the fluid flowing in the larger exterior conduit by dividing the fluid into a first portion that flows along the center axis through the flow-through conduit and a second portion that concurrently flows outside of the flow-through conduit along the center axis and along a different direction.
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