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1.发明授权公开(公告)号：US12050012B2
公开(公告)日：2024-07-30
申请号：US17909408
申请日：2020-12-10
发明人： Stefan Dederichs , Michael Huth , Ramsatish Kaluri , Udo Schmitz , Anatol Schulz , Daniel Vogtmann
摘要： A burner component of a burner. The burner has a flow channel, in which combustion air flows in a flow direction from upstream to downstream. The burner component includes a wall portion, which adjoins the flow channel; a plurality of injection nozzles, which are arranged in the wall portion; and a plurality of vortex generators, which are arranged on the wall portion. The vortex generators have a concavely curved sloped surface rising in the flow direction to improve the distribution of the fuel in the combustion air.
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公开(公告)号：US11828469B2
公开(公告)日：2023-11-28
申请号：US17653376
申请日：2022-03-03
摘要： An adaptive trapped vortex combustor for a gas turbine engine includes a combustion chamber, a fuel injector, and one or more chutes. The combustion chamber is defined by an outer liner, an inner liner, and a dome, and includes a primary combustion zone within the combustion chamber defining a vortex cavity for a trapped vortex, the vortex cavity having a volume therein, a secondary combustion zone within the combustion chamber, and an opening from the primary combustion zone to the secondary combustion zone. The fuel injector injects a fuel into the primary combustion zone. The one or more chutes provide an air flow to the primary combustion zone and/or the secondary combustion zone. A feature of the adaptive trapped vortex combustor is controllable such that a residence time of the fuel in the vortex cavity is controllable based on an operating condition of the gas turbine engine.
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公开(公告)号：US20230358403A1
公开(公告)日：2023-11-09
申请号：US18354167
申请日：2023-07-18
发明人： Saket Singh , Pradeep Nalk , Daniel J. Kirtley , Rimple Rangrej , Ranganatha Narasimha Chiranthan
CPC分类号： F23R3/26 , F23R3/002 , F23R3/12 , F23R2900/03045
摘要： A combustor for a gas turbine engine. The combustor has a combustor liner that includes a vortex turbulence generator. The vortex turbulence generator has a flow passage extending therethrough, the flow passage being defined by a wall about a periphery of the flow passage, and a plurality of vortex generating turbulators disposed on the wall, each of the plurality of vortex generating turbulators a projection portion extending from a surface of the wall into the flow passage and generating a vortex turbulent flow of an oxidizer passing through the flow passage from a cold surface side of the combustor liner to a hot surface side of the combustor liner.
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公开(公告)号：US11773784B2
公开(公告)日：2023-10-03
申请号：US17499527
申请日：2021-10-12
申请人： Delavan Inc.
CPC分类号： F02C7/264 , F23R3/12 , F23R3/28 , F23R3/286 , F05D2220/32 , F05D2240/35 , F23R2900/00009
摘要： A fuel injector includes a fuel nozzle configured to issue a spray of fuel from a fuel outlet in a downstream direction along an injection axis. The fuel nozzle includes a nozzle body that defines a main flow passage therethrough. An injection fuel line is in fluid communication with the fuel nozzle to supply fuel to the fuel nozzle. A torch ignitor with a flame outlet opens into the main flow passage of the fuel nozzle for issuing flame into the main flow passage. The flame outlet meets the main flow passage at a position that is downstream of the fuel outlet with respect to the downstream direction along the injection axis.
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公开(公告)号：US20230280034A1
公开(公告)日：2023-09-07
申请号：US17653376
申请日：2022-03-03
摘要： An adaptive trapped vortex combustor for a gas turbine engine includes a combustion chamber, a fuel injector, and one or more chutes. The combustion chamber is defined by an outer liner, an inner liner, and a dome, and includes a primary combustion zone within the combustion chamber defining a vortex cavity for a trapped vortex, the vortex cavity having a volume therein, a secondary combustion zone within the combustion chamber, and an opening from the primary combustion zone to the secondary combustion zone. The fuel injector injects a fuel into the primary combustion zone. The one or more chutes provide an air flow to the primary combustion zone and/or the secondary combustion zone. A feature of the adaptive trapped vortex combustor is controllable such that a residence time of the fuel in the vortex cavity is controllable based on an operating condition of the gas turbine engine.
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公开(公告)号：US11739731B2
公开(公告)日：2023-08-29
申请号：US16315207
申请日：2017-07-06
发明人： Neil Andrew Hawkes
CPC分类号： F03D9/39 , F03D3/005 , F03D3/061 , F03D3/02 , F03D9/34 , F05B2240/132 , F05B2240/211 , F05B2240/30 , F05B2240/3062 , F05B2260/209 , F15C1/16 , F23R3/12 , F23R3/58 , Y02B10/30 , Y02E10/70 , Y02E10/728 , Y10T137/2087 , Y10T137/2104
摘要： This invention relates to a vortex station and method for producing a vortex similar to one of a group consisting of dust-devils and waterspouts. The apparatus comprises a ground platform forming a base for the vortex station, a plurality of vanes to direct an air flow into a vortex station and about the vortex station in a substantially swirling manner, at least one wind turbine disposed near the centre of said vortex station, in a path of a concentrated air flow, wherein the movement of the air in the vortex station is such that an atmospheric buoyancy vortex is created in the centre of the vortex station, a supply of a working fluid (e.g. water) to the vortex station at or near the centre of the vortex station such that the air is of a saturated condition or an at least partially saturated condition with the working fluid (e.g. water), the working fluid (e.g. water) supplied at a sufficient quantity or amount so as to assist with maintaining buoyancy and stability of a vortex created.
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公开(公告)号：US11598527B2
公开(公告)日：2023-03-07
申请号：US15177825
申请日：2016-06-09
发明人： Justin M. Locke , Dennis Moura , Duane McCormick , Scott A. Liljenberg , Theodore Strickland , William Proscia
摘要： A method of reducing noise from a combustor of a gas turbine engine includes the steps of establishing a maximum noise limit that may be for a particular frequency range. A primary fuel flow percentage, which may be emitted from a fuel nozzle arrangement having various groupings of simplex and duplex nozzles, is then established. An immersion depth measured between an aft rim of a swirler and a distal tip of the fuel nozzles may then be reduced thereby reducing the noise amplitude.
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公开(公告)号：US20220412557A1
公开(公告)日：2022-12-29
申请号：US17889833
申请日：2022-08-17
发明人： Jeremy Eron Fetvedt , Xijia Lu , Brent Gregory , Chris Bonilha , James Lenertz , Stefan Tschirren , Hassan Abdulsater
摘要： The present disclosure relates to apparatuses and methods that are useful for one or more aspects of a power production plant. More particularly, the disclosure relates to combustor apparatuses and methods for a combustor adapted to utilize different fuel mixtures derived from gasification of a solid fuel. Combustion of the different fuel mixtures within the combustor can be facilitated by arranging elements of the combustor controlled so that a defined set of combustion characteristics remains substantially constant across a range of different fuel mixtures.
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9.发明申请公开(公告)号：US20220290863A1
公开(公告)日：2022-09-15
申请号：US17199257
申请日：2021-03-11
摘要： A mixer for blending fuel and air in a combustor of a turbine engine. The mixer includes a central body having a central passageway and a central axis. The mixer includes a plurality of tubes positioned radially around the central axis and circumferentially around a periphery of the mixer. Each of the tubes of the mixer includes opposed openings and a tangential opening. Each of the tubes of the mixer includes a cylindrical interior mixing passage configured to receive air flow from the opposed openings and the tangential opening and a fuel flow. The opposed openings are configured to spread the fuel flow laterally and the tangential opening is configured to spread the fuel flow tangentially.
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公开(公告)号：US11435077B2
公开(公告)日：2022-09-06
申请号：US17087022
申请日：2020-11-02
发明人： Jeremy Eron Fetvedt , Xijia Lu , Brent Gregory , Chris Bonilha , James Lenertz , Stefan Tschirren , Hassan Abdulsater
IPC分类号： F23R3/12 , F23M5/08 , F23G5/027 , F23B90/06 , F23R3/00 , F02B43/12 , F02C3/22 , F23L7/00 , F23D14/24 , F23R3/06 , F23R3/36
摘要： The present disclosure relates to apparatuses and methods that are useful for one or more aspects of a power production plant. More particularly, the disclosure relates to combustor apparatuses and methods for a combustor adapted to utilize different fuel mixtures derived from gasification of a solid fuel. Combustion of the different fuel mixtures within the combustor can be facilitated by arranging elements of the combustor controlled so that a defined set of combustion characteristics remains substantially constant across a range of different fuel mixtures.
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