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公开(公告)号：US11226103B1
公开(公告)日：2022-01-18
申请号：US17123778
申请日：2020-12-16
Applicant: Delavan Inc.
Inventor： Jason Ryon , Lev Alexander Prociw , Brandon P. Williams
Abstract: A torch ignitor system provides a continuous flame to ignite fuel within a combustor of a gas turbine engine. The torch ignitor system includes a torch ignitor, a housing, a flow channel, and an outlet nozzle. The torch ignitor system is configured to receive high-pressure air from the high-pressure compressor region of a gas turbine engine to increase operational characteristics of the torch ignitor system, including fuel atomization, cooling of the torch ignitor system, and circulation of combustion air within the torch ignitor system.
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公开(公告)号：US11131458B2
公开(公告)日：2021-09-28
申请号：US15949779
申请日：2018-04-10
Applicant: Delavan, Inc.
Inventor： Lev Alexander Prociw , Jason A. Ryon , Gregory A. Zink
Abstract: A fuel injector for a multipoint injection system can include a body defining an air cavity for allowing air to flow therethrough and an interior cavity. A fuel is tube disposed at least partially within the interior cavity of the body. The fuel tube can include a first end configured to connect to a fuel injector connector of a fuel manifold, and a second end configured to connect to a fuel distributor of the fuel injector, wherein the fuel injector is configured to be disposed at least partially in a combustor dome. The fuel tube is configured to move in an axial direction to allow flexibility between the fuel manifold and the combustor dome.
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公开(公告)号：US11067278B2
公开(公告)日：2021-07-20
申请号：US15992470
申请日：2018-05-30
Applicant: Delavan Inc
Inventor： Lev Alexander Prociw , Timothy Griffith
Abstract: A fuel system includes a fuel supply system. A plurality of fuel nozzles are connected in fluid communication with the fuel supply system to supply fuel from a fuel source to be issued for combustion from the fuel nozzles. A cooling system is included, wherein at least one of the fuel nozzles includes a cooling circuit in addition to a fuel circuit for issuing fuel from the fuel supply system for combustion. The cooling circuit includes an inlet and an outlet. The inlet is in fluid communication with the cooling system for circulation of coolant through the cooling circuit and back to the cooling system out the outlet of the cooling circuit for cooling the fuel circuit with the fuel circuit staged off.
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公开(公告)号：US11053862B2
公开(公告)日：2021-07-06
申请号：US15714597
申请日：2017-09-25
Applicant: Delavan Inc.
Inventor： Jason A. Ryon , Lev Alexander Prociw
Abstract: A fuel injector for a gas turbine engine includes a feed arm defining a conduit extending between an inlet end and an outlet end and a plunger. The plunger is disposed within the conduit and is movable between a plunger first position and a plunger second position. A flow area defined between the plunger and the feed arm is smaller in the plunger first position than in the plunger second position to bias fuel flow through the fuel injector. Fuel systems, gas turbine engines, and methods of controlling fuel flow in gas turbine engine fuel systems are also described.
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公开(公告)号：US11014054B2
公开(公告)日：2021-05-25
申请号：US16387153
申请日：2019-04-17
Applicant: Delavan Inc.
Inventor： Lev Alexander Prociw , Jason Ryon , Philip E. O. Buelow , Brandon Phillip Williams
Abstract: A fluid-gas mixer including a housing, defining a primary axis, for mixing fluid and gas, a mixer nozzle circumscribing the primary axis, wherein an annular gap between an outer surface of the mixer nozzle and an inner surface of the housing defines at least one outer gas path, a swirling gas passage defining an inner gas path for mixing with the outer gas path.
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Patent Agency Ranking
公开(公告)号：US10830446B2
公开(公告)日：2020-11-10
申请号：US15844216
申请日：2017-12-15
Applicant: Delavan, Inc.
Inventor： Lev Alexander Prociw , Jason A. Ryon , Jacob Greenfield
Abstract: A method for assembling a fuel distribution system for a turbomachine fuel injector includes inserting a liquid fuel distributor into an interior cavity of a shroud to create a liquid fuel distribution circuit between the liquid fuel distributor and the shroud and inserting a gas fuel distributor into the interior cavity of the shroud and into an interior cavity of the liquid fuel distributor to create a gas fuel distribution circuit between the gas fuel distributor and the liquid fuel distributor. The method includes inserting a fuel transfer tube into an outer diameter of the shroud. The method includes brazing or shrink fitting at least one of the fuel transfer tube, the gas fuel distributor, or the liquid fuel distributor to the shroud.
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公开(公告)号：US20200309376A1
公开(公告)日：2020-10-01
申请号：US16370767
申请日：2019-03-29
Applicant: Delavan Inc.
Inventor： Lev Alexander Prociw , Jason Ryon , Philip E. O. Buelow , Brandon Phillip Williams
Abstract: A nozzle includes an outer gas flow path, an inner gas flow path radially inward from the outer gas flow path, a liquid flow path defined radially between the inner gas flow path and the outer gas flow path, and a core conduit defined radially inward from the inner gas flow path. An injector assembly includes an outer housing, a nozzle within the outer housing, and an outer housing gas flow path defined radially outward from the nozzle between an inner surface of the outer housing and an outer surface of the nozzle. The nozzle includes an outer gas flow path, an inner gas flow path radially inward from the outer gas flow path, a liquid flow path defined radially between the inner gas flow path and the outer gas flow path and a core conduit defined radially inward from the inner gas flow path.
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公开(公告)号：US20190093560A1
公开(公告)日：2019-03-28
申请号：US15714265
申请日：2017-09-25
Applicant: Delavan Inc.
Inventor： Jason A. Ryon , Jacob Greenfield , Lev Alexander Prociw
CPC classification number: F02C7/222 , F05D2220/32 , F05D2240/35 , F23R3/10 , F23R3/346 , F23R3/36 , F23R2900/00012
Abstract: A fluid manifold includes a manifold body, a first annular passage and a second annular passage. The first annular passage is defined within the manifold body between a first passage inlet and a first passage outlet downstream from the first passage inlet. The second annular passage is defined within the manifold body nested radially outward from the first annular passage, and between a second passage inlet and a second passage outlet downstream from the second passage inlet. The first and second annular passages are concentric about a manifold axis. The first passage outlet and the second passage outlet are positioned at the same axial position relative to the manifold axis.
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公开(公告)号：US20170282273A1
公开(公告)日：2017-10-05
申请号：US15630313
申请日：2017-06-22
Applicant: Delavan Inc
Inventor： Lev Alexander Prociw , Jason A. Ryon , Steven J. Myers , Michael J. Bronson , Fouad T. Khairallah
CPC classification number: B23K1/20 , B23K3/0623 , B23K3/0638 , B23K35/0244 , B23K35/3006 , B23K35/3013 , B23K35/302 , B23K35/3033 , B23K35/3053 , B23K35/32 , B23K35/322
Abstract: A method of manufacturing includes depositing a braze filler adjacent to a void between a first component and a second component thus holding the components in position before brazing. The first and second components are heated to melt and flow the braze filler into the void. A braze joint is formed between the first and second components by cooling the braze filler. Depositing the braze filler can include laser cladding the braze filler to the first and/or second components adjacent the void. The method also optionally includes welding the first and second components in position with the braze filler adjacent to the void. The braze filler may be deposited as a powder, cold spray, melted brazed filament, spherical ball or any other suitable form.
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公开(公告)号：US20150361896A1
公开(公告)日：2015-12-17
申请号：US14835654
申请日：2015-08-25
Applicant: Delavan Inc
Inventor： Lev Alexander Prociw , Jason Ryon
IPC: F02C7/22
CPC classification number: F23R3/14 , F02C7/22 , F23D11/107 , F23D2900/11101 , F23R3/10 , F23R3/12 , F23R3/28 , F23R3/286 , F23R3/30
Abstract: An injector for a multipoint combustor system includes an inner air swirler which defines an interior flow passage and a plurality of swirler inlet ports in an upstream portion thereof. The inlet ports are configured and adapted to impart swirl on flow in the interior flow passage. An outer air cap is mounted outboard of the inner swirler. A fuel passage is defined between the inner air swirler and the outer air cap, and includes a discharge outlet between downstream portions of the inner air swirler and the outer air cap for issuing fuel for combustion. The outer air cap defines an outer air circuit configured for substantially unswirled injection of compressor discharge air outboard of the interior flow passage.
Abstract translation: 用于多点燃烧器系统的喷射器包括内部空气旋流器，其在其上游部分中限定内部流动通道和多个旋流器入口。 入口端口被配置和适于在内部流动通道中产生流动的漩涡。 外部空气盖安装在内旋流器的外侧。 在内部空气旋流器和外部空气帽之间限定有燃料通道，并且在内部空气旋流器的下游部分和用于燃烧燃料的外部空气帽之间包括排出口。 外部空气帽限定了外部空气回路，该外部空气回路经配置以基本上不加注入内部流动通道外侧的压缩机排放空气。
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