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公开(公告)号：US20160376997A1
公开(公告)日：2016-12-29
申请号：US14752318
申请日：2015-06-26
Applicant: Delavan Inc
Inventor： Lev A. Prociw
Abstract: A combustion system for a gas turbine engine includes a combustor dome. The combustor dome includes a fuel manifold with an inlet and nozzle components of a plurality of nozzles circumferentially spaced around the combustor dome. The fuel manifold and nozzle components are integrated with the combustor dome for fluid communication from the inlet to the nozzle components.
Abstract translation: 燃气涡轮发动机的燃烧系统包括燃烧器穹顶。 燃烧器穹顶包括燃料歧管，其具有围绕燃烧器穹顶周向间隔开的多个喷嘴的入口和喷嘴部件。 燃料歧管和喷嘴部件与燃烧器圆顶集成，用于从入口到喷嘴部件的流体连通。
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公开(公告)号：US20160290291A1
公开(公告)日：2016-10-06
申请号：US14674709
申请日：2015-03-31
Applicant: Delavan Inc
Inventor： Lev A. Prociw
Abstract: A nozzle includes a nozzle body defining a longitudinal axis. The nozzle body has an air passage, a fuel circuit radially outboard from the air passage with respect to the longitudinal axis, and a cooling circuit. The fuel circuit extends from a fuel circuit inlet to a fuel circuit annular outlet. The fuel circuit is defined between a fuel circuit inner wall and a fuel circuit outer wall. At least a portion of the fuel circuit outer wall is radially outboard from the fuel circuit inner wall with respect to the longitudinal axis. A cooling circuit is defined within at least one of the fuel circuit inner wall or the fuel circuit outer wall. The cooling circuit extends from an axial position proximate the fuel circuit inlet to an axial position proximate the fuel circuit outlet.
Abstract translation: 喷嘴包括限定纵向轴线的喷嘴体。 喷嘴体具有空气通道，相对于纵向轴线从空气通道径向外侧的燃料回路和冷却回路。 燃料回路从燃料回路入口延伸到燃料回路环形出口。 燃料回路限定在燃料回路内壁和燃料回路外壁之间。 燃料回路外壁的至少一部分相对于纵向轴线从燃料回路内壁径向地外侧。 在燃料回路内壁或燃料回路外壁的至少一个内限定冷却回路。 冷却回路从靠近燃料回路入口的轴向位置延伸到靠近燃料回路出口的轴向位置。
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公开(公告)号：US09309848B2
公开(公告)日：2016-04-12
申请号：US14512305
申请日：2014-10-10
Applicant: Delavan Inc.
Inventor： Lev A. Prociw , Kevin E. Thompson , Steve J. Myers
CPC classification number: F02M53/08 , F01N3/0253 , F01N3/36 , F01N2610/03 , F01N2610/11 , F01N2610/1453 , Y02T10/20
Abstract: A pressure atomizing nozzle for injecting fuel includes an inlet housing configured to thermally isolate the interior space from external conditions and to remain relatively cool under operation so as to substantially eliminate heat soak back from the inlet housing to the interior space thereof after operation. First and second coolant conduits cool the nozzle tip region actively during operation and passively after operation. A cooling air jacket is configured to thermally isolate inboard components from exterior conditions, to provide clean air during operation to the nozzle tip region for diluting carbon to reduce carbon deposits in the nozzle tip region and for cooling the same, and to provide passive cooling to the nozzle tip region after operation.
Abstract translation: 用于喷射燃料的压力雾化喷嘴包括入口壳体，其构造成将内部空间与外部条件热隔离并且在操作下保持相对冷却，从而基本上消除在操作之后从入口壳体吸收回到其内部空间的热量。 第一和第二冷却剂管道在操作期间主动地冷却喷嘴尖端区域，在操作之后被动地冷却。 冷却空气套被配置为将内部组件与外部条件热隔离，以在操作期间向喷嘴尖端区域提供清洁空气，用于稀释碳以减少喷嘴尖端区域中的碳沉积并且用于冷却其，并且提供被动冷却 喷嘴尖端区域操作后。
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公开(公告)号：US20150159608A1
公开(公告)日：2015-06-11
申请号：US14512305
申请日：2014-10-10
Applicant: Delavan Inc.
Inventor： Lev A. Prociw , Kevin E. Thompson , Steve J. Myers
IPC: F02M53/08
CPC classification number: F02M53/08 , F01N3/0253 , F01N3/36 , F01N2610/03 , F01N2610/11 , F01N2610/1453 , Y02T10/20
Abstract: A pressure atomizing nozzle for injecting fuel includes an inlet housing configured to thermally isolate the interior space from external conditions and to remain relatively cool under operation so as to substantially eliminate heat soak back from the inlet housing to the interior space thereof after operation. First and second coolant conduits cool the nozzle tip region actively during operation and passively after operation. A cooling air jacket is configured to thermally isolate inboard components from exterior conditions, to provide clean air during operation to the nozzle tip region for diluting carbon to reduce carbon deposits in the nozzle tip region and for cooling the same, and to provide passive cooling to the nozzle tip region after operation.
Abstract translation: 用于喷射燃料的压力雾化喷嘴包括入口壳体，其构造成将内部空间与外部条件热隔离并且在操作下保持相对冷却，从而基本上消除在操作之后从入口壳体吸收回到其内部空间的热量。 第一和第二冷却剂管道在操作期间主动地冷却喷嘴尖端区域，在操作之后被动地冷却。 冷却空气套被配置为将内部组件与外部条件热隔离，以在操作期间向喷嘴尖端区域提供清洁空气，用于稀释碳以减少喷嘴尖端区域中的碳沉积并冷却其，并且提供被动冷却 喷嘴尖端区域操作后。
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公开(公告)号：US11994290B2
公开(公告)日：2024-05-28
申请号：US17357906
申请日：2021-06-24
Applicant: Delavan Inc.
Inventor： Jason A. Ryon , Lev A. Prociw
CPC classification number: F23R3/002 , B23P15/26 , F01D25/145 , F23R3/005 , F23R3/50 , F28D15/0266 , F28D15/0275 , F28D15/0283 , F28D15/04 , F28D15/046 , F05D2230/22 , F05D2240/35 , F05D2260/208 , F23R2900/00018 , F28D2021/0026
Abstract: A heat transfer arrangement includes two or more heat transfer cells. The heat transfer cells together define a boundary between a higher temperature region and a lower temperature region. Each of the two or more heat transfer cells includes two or more walls defining a fluid tight cavity. One or more wick is fused to an inner surface of one or more of the walls to wick liquid from a lower temperature portion of the cavity to a higher temperature portion of the cavity. Combustors having heat transfer arrangements with heat transfer cells and methods of making heat transfer arrangements are also described.
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Patent Agency Ranking
公开(公告)号：US11965654B2
公开(公告)日：2024-04-23
申请号：US17376494
申请日：2021-07-15
Applicant: Delavan Inc.
Inventor： Lev A. Prociw , Timothy Griffith
CPC classification number: F23R3/283 , F02C7/222 , F02C7/228 , F23R3/346 , F02C7/224 , F05D2260/232 , F23D14/78 , F23D2214/00 , F23R3/28
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：US11852075B2
公开(公告)日：2023-12-26
申请号：US17229346
申请日：2021-04-13
Applicant: Delavan Inc.
Inventor： Jacob Greenfield , Jason A. Ryon , Lev A. Prociw
CPC classification number: F02C7/222 , F02C7/20 , F02C7/28 , F23R3/34 , F23R3/343 , F05D2230/60 , F05D2240/14 , F05D2240/35 , F05D2240/55 , F05D2250/75 , F05D2260/941 , F23R2900/00005 , F23R2900/00018
Abstract: A turbomachine fuel injector system includes an air distributor configured to be mounted to and contained within a casing and to provide air to mix with a fuel from one or more fuel distribution systems. The system includes a fuel manifold configured to be mounted indirectly to the casing such that the fuel manifold system is contained within the casing but is independent such that fuel manifold does not touch or directly mount to either an interior of the casing or touch the air distributor within the casing to prevent or reduce thermal transfer from the air distributor to the fuel manifold.
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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
Applicant: Delavan Inc.
Inventor： Jason Ryon , Lev A. Prociw , Brandon Phillip Williams
CPC classification number: F02C7/264 , F23R3/12 , F23R3/28 , F23R3/286 , F05D2220/32 , F05D2240/35 , F23R2900/00009
Abstract: 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：US11761634B2
公开(公告)日：2023-09-19
申请号：US17080796
申请日：2020-10-26
Applicant: Delavan Inc.
Inventor： Lev A. Prociw , Jason A. Ryon , Jacob Greenfield
CPC classification number: F23R3/36 , F23D17/002 , F23R3/283 , F23D2204/10 , F23D2213/00 , F23D2900/00008 , F23K2300/20 , F23R2900/00017
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：US11692487B2
公开(公告)日：2023-07-04
申请号：US17578926
申请日：2022-01-19
Applicant: Delavan Inc.
Inventor： Jason A. Ryon , Lev A. Prociw , Gregory A. Zink
CPC classification number: F02C7/24 , F02C7/222 , F23R3/283 , F05D2240/35 , F05D2260/231 , F05D2270/3032
Abstract: A fuel injector system includes an outer support and an inner support, with a feed arm extending radially between the inner support and the outer support. A plurality of outlet openings extend in an axial direction from the feed arm for feeding respective injection nozzles. The outer support and feed arm define a plurality of fuel passages therethrough to convey fluid from an external source through the outer support and feed arm to the outlet openings. A heat shield extends around the feed arm from the outer support to the inner support. The heat shield is spaced apart from the feed arm with an insulative gap therebetween.
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