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公开(公告)号：US20220195939A1
公开(公告)日：2022-06-23
申请号：US17133216
申请日：2020-12-23
Applicant: Delavan Inc.
Inventor： Jason Ryon , Lev A. Prociw , Brandon Phillip Williams
Abstract: A torch ignitor system for a combustor of a gas turbine engine includes a torch ignitor, the torch ignitor including a combustion chamber oriented about a torch axis, the combustion chamber having axially upstream and downstream ends defining a flow direction through the combustion chamber, along the axis. The torch ignitor includes a cap defining the axially upstream end of the combustion chamber and oriented about the axis, wherein the cap is configured to receive a fuel injector and at least one glow plug. The torch ignitor includes an elbow connected to the downstream end of the combustion chamber for diverting combustion products along an ignition jet flame axis that is off of the torch axis for injection of combustion products into a gas turbine engine combustor. The torch ignitor further includes a tip at a downstream end of the elbow for issuing the injection of combustion products.
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公开(公告)号：US20210372621A1
公开(公告)日：2021-12-02
申请号：US17405276
申请日：2021-08-18
Applicant: Delavan Inc.
Inventor： Jason A. Ryon , Steve J. Myers , Philip E. O. Buelow , Lev A. Prociw
Abstract: A fuel injector for an exhaust heater includes a cover and an air blast nozzle. The cover has a nozzle seat, a fuel inlet, and an air inlet, the nozzle seat arranged along a flow axis. The air blast nozzle is seated in the nozzle seat and has a unibody. The air blast nozzle unibody is in fluid communication with the fuel inlet and the air inlet arranged along the flow axis to port fuel and air into a combustion volume, e.g., to heat a stream of exhaust gas flowing between an engine and a catalytic reactor by combustion with fuel introduced through the fuel inlet and air introduced through the air inlet.
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公开(公告)号：US20210332981A1
公开(公告)日：2021-10-28
申请号：US17243246
申请日：2021-04-28
Applicant: Delavan Inc.
Inventor： Lev A. Prociw , Jason Ryon , Philip E. O. Buelow
Abstract: A fluid nozzle includes a first fluid circuit, a second fluid circuit spaced apart from the first fluid circuit and a fuel circuit. The fuel circuit is defined between the first and second fluid circuits and between a first fuel circuit wall and a second fuel circuit wall. A ring-shaped permeable barrier is positioned between the first and second fuel circuit walls configured and adapted to provide a controlled resistance to fuel flow. A fuel distributor includes a first fuel circuit wall and a second fuel circuit wall spaced apart from the first fuel circuit wall. A fuel circuit is defined between the first and second fuel circuit walls. A ring-shaped permeable barrier is positioned between first and second fuel circuit walls. A combustion assembly includes a combustor housing, a combustor dome positioned at an upstream end of the combustor housing, and a fluid nozzle positioned adjacent the combustor dome.
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公开(公告)号：US20210207539A1
公开(公告)日：2021-07-08
申请号：US17193390
申请日：2021-03-05
Applicant: Delavan Inc.
Inventor： Jason A. Ryon , Lev A. Prociw , Gregory A. Zink , Joseph Samo
Abstract: A multipoint injection system includes a manifold with a plurality of flow passages defined through the manifold in the circumferential direction. The flow passages are spaced apart from one another in an axial direction. A plurality of feed arms extends radially inward from the manifold. Feed arm portions of the flow passages extend through each of the feed arms to respective outlets. The feed arm portions of the flow passages are within the axial width of the manifold. A plurality of injection nozzles are included, each in fluid communication with a respective one of the outlets. Each injection nozzle includes an air passage therethrough with an air inlet. The feed arms each follow a path that is circumferentially offset from the air inlets so each of the feed arms is clear from a flow path directly upstream in the axial direction of each of the air inlets.
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公开(公告)号：US20210156564A1
公开(公告)日：2021-05-27
申请号：US16696450
申请日：2019-11-26
Applicant: Delavan Inc.
Inventor： Lev A. Prociw , Jason Ryon
Abstract: A system includes a combustor. The combustor has a combustor wall with a combustor dome at an upstream end of the combustor wall, and an outlet at a downstream end of the combustor wall opposite the upstream end. The combustor wall includes an inner wall portion and an outer wall portion defining an interior of the combustor therebetween. Each of the inner wall portion and outer wall portion extends from the combustor dome to the downstream end of the combustor wall. The combustor wall includes an air cooling passage embedded inside at least one of the inner wall portion and the outer wall portion. The air cooling passage extends from the upstream end of the combustor wall to the downstream end of the combustor wall.
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Patent Agency Ranking
公开(公告)号：US20210101169A1
公开(公告)日：2021-04-08
申请号：US16593732
申请日：2019-10-04
Applicant: Delavan Inc.
Inventor： Jason Ryon , Lev A. Prociw
IPC: B05B15/14
Abstract: A method includes forming a fluid conduit inside a heat shield in an additive manufacturing process, wherein a fluid nozzle is defined at a downstream end of the fluid conduit, and wherein the heat shield is formed about the fluid nozzle. The method includes removing powder from an interior passage of the fluid conduit and fluid nozzle and from an insulation gap defined between the heat shield and the fluid conduit and fluid nozzle. The method includes separating the heat shield, fluid conduit, and fluid nozzle from the build platform. The method includes shifting the fluid conduit and fluid nozzle to a shifted position relative to the heat shield, and securing the fluid conduit and fluid nozzle to the heat shield in the shifted position.
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公开(公告)号：US10859269B2
公开(公告)日：2020-12-08
申请号：US15476362
申请日：2017-03-31
Applicant: Delavan Inc
Inventor： Jason A. Ryon , Lev A. Prociw , Gregory A. Zink
Abstract: A combustor dome system includes an annular combustor dome defining a main axis therethrough. The combustor dome includes opposed upstream and downstream faces, wherein the upstream face is configured to face upstream toward a compressor discharge space, wherein the downstream face is configured to face downstream toward a combustor space. The downstream face has a curved cross-sectional profile. A plurality of nozzles extends at least partially through the combustor dome from the upstream face to the downstream face for injection of fuel into the combustor space. A fuel manifold is in fluid communication with the plurality of nozzles.
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公开(公告)号：US20190024897A1
公开(公告)日：2019-01-24
申请号：US15656815
申请日：2017-07-21
Applicant: Delavan Inc.
Inventor： Lev A. Prociw , Jason A. Ryon , Gregory A. Zink
IPC: F23R3/14
Abstract: A nozzle assembly includes a fuel distributor for issuing a spray of fuel. A fuel conduit is in fluid communication with the fuel distributor and has a first end and a second end. The first end and/or the second end of the fuel conduit is operatively connected to the fuel distributor. The fuel conduit is configured to allow relative movement between the first end and the second end to accommodate dimensional variations of at least one of the nozzle assembly or a combustor. A nozzle system includes the nozzle assembly and a combustor wall having a nozzle inlet. The nozzle assembly is positioned adjacent to the nozzle inlet.
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公开(公告)号：US20180283692A1
公开(公告)日：2018-10-04
申请号：US15476362
申请日：2017-03-31
Applicant: Delavan Inc
Inventor： Jason A. Ryon , Lev A. Prociw , Gregory A. Zink
IPC: F23R3/28
Abstract: A combustor dome system includes an annular combustor dome defining a main axis therethrough. The combustor dome includes opposed upstream and downstream faces, wherein the upstream face is configured to face upstream toward a compressor discharge space, wherein the downstream face is configured to face downstream toward a combustor space. The downstream face has a curved cross-sectional profile. A plurality of nozzles extends at least partially through the combustor dome from the upstream face to the downstream face for injection of fuel into the combustor space. A fuel manifold is in fluid communication with the plurality of nozzles.
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公开(公告)号：US09573146B2
公开(公告)日：2017-02-21
申请号：US14163150
申请日：2014-01-24
Applicant: Delavan Inc , Delavan Limited
Inventor： Lev A. Prociw , Frank Whittaker , Neil Smith
CPC classification number: B05B1/3426 , B05B1/3431 , B05B1/3447 , B05B1/3468 , F23D11/383
Abstract: A swirler for swirling fluid in a nozzle has a swirler body. The swirler body defines an inlet end, an outlet end opposed to the inlet end, and a circumferential periphery. The circumferential periphery extends axially from the inlet end to the outlet end. The outlet end defines a first swirl chamber. The inlet end defines a second swirl chamber.
Abstract translation: 喷嘴中旋转流体的旋流器具有旋流器体。 旋流器主体限定入口端，与入口端相对的出口端和周向周边。 周向周边从入口端轴向延伸到出口端。 出口端限定第一涡流室。 入口端限定第二涡流室。
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