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公开(公告)号：US20070044477A1
公开(公告)日：2007-03-01
申请号：US11217505
申请日：2005-09-01
Applicant: Timothy Held , James Cooper
Inventor： Timothy Held , James Cooper
IPC: F02C7/22
CPC classification number: F23L7/007 , F23D11/24 , F23D11/386 , F23D2209/30 , F23D2214/00 , F23L7/005 , F23R3/14 , F23R3/286 , F23R3/36 , Y02E20/344
Abstract: A gas turbine engine fuel nozzle includes an axis of symmetry extending therethrough, the nozzle body including a first passage extending coaxially therethrough, a second passage, and a third passage, the second passage circumscribing the first passage, the third passage formed radially outward of the second passage, and a nozzle tip coupled to the nozzle body, the nozzle tip including at least one primary discharge opening in flow communication with the first passage, at least one secondary discharge opening in flow communication with the second passage, and at least one tertiary discharge opening in flow communication with the third passage.
Abstract translation: 燃气涡轮发动机燃料喷嘴包括延伸穿过其中的对称轴线，喷嘴体包括同轴地延伸通过的第一通道，第二通道和第三通道，第二通道限定第一通道，第三通道径向向外形成 第二通道和联接到喷嘴主体的喷嘴尖端，喷嘴尖端包括与第一通道流动连通的至少一个主排出口，与第二通道流动连通的至少一个二次排放口，以及至少一个第三通道 排出口与第三通道流通。
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2.发明申请公开(公告)号：US20050229600A1
公开(公告)日：2005-10-20
申请号：US10826432
申请日：2004-04-16
Applicant: David Kastrup , Jeffrey Martini , Douglas Fortuna , Timothy Held , Shaun De Vane , James Cooper
Inventor： David Kastrup , Jeffrey Martini , Douglas Fortuna , Timothy Held , Shaun De Vane , James Cooper
CPC classification number: F23R3/14 , F23D2211/00
Abstract: A method facilitates fabricating a gas turbine engine combustor. The method comprises coupling a venturi to a primary swirler, and coupling the venturi to a secondary swirler such that a gap is defined between a portion of the venturi and a portion of one of the primary swirler and the secondary swirler.
Abstract translation: 一种方法有助于制造燃气涡轮发动机燃烧器。 该方法包括将文丘里管连接到初级旋流器，以及将文丘里管连接到次级旋流器，使得在文丘里管的一部分与初级旋流器和次级旋流器之一的部分之间限定间隙。
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公开(公告)号：US20070101726A1
公开(公告)日：2007-05-10
申请号：US11268183
申请日：2005-11-07
Applicant: Mark Durbin , Allen Danis , Timothy Held , James Cooper , Douglas Fortuna , Daniel Durstock
Inventor： Mark Durbin , Allen Danis , Timothy Held , James Cooper , Douglas Fortuna , Daniel Durstock
IPC: F02C3/30
CPC classification number: F02C3/30 , F05D2250/31 , F05D2250/314 , F23D14/58 , F23D2900/00014 , F23L7/005 , F23R3/343
Abstract: A method facilitates operating a gas turbine engine. The method comprises supplying steam to a nozzle, supplying primary fuel to the nozzle, discharging the steam into a combustor from a plurality of circumferentially-spaced steam outlets defined in a tip of the nozzle, and discharging the primary fuel into the combustor from at least one outlet that is spaced circumferentially between the steam outlets.
Abstract translation: 一种方法便于操作燃气涡轮发动机。 该方法包括向喷嘴供应蒸汽，向喷嘴供应初级燃料，将蒸汽从限定在喷嘴的尖端中的多个周向隔开的蒸汽出口排出到燃烧器中，并将主燃料从至少排出到燃烧器中 一个在蒸汽出口之间周向隔开的出口。
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公开(公告)号：US20060096296A1
公开(公告)日：2006-05-11
申请号：US11312273
申请日：2005-12-20
Applicant: Timothy Held , Mark Mueller , Jun Xu
Inventor： Timothy Held , Mark Mueller , Jun Xu
IPC: F23R3/30
Abstract: A method for operating a gas turbine engine facilitates reducing an amount of emissions from a combustor. The combustor includes a mixer assembly including a pilot mixer, a main mixer, and an annular centerbody extending therebetween. The method comprises injecting at least one of fuel and airflow into the combustor through at least one swirler positioned within the pilot mixer, and injecting fuel into the combustor through at least one swirler positioned within the main mixer, such that the fuel is directed into a combustion chamber downstream from the main mixer.
Abstract translation: 用于操作燃气涡轮发动机的方法有助于减少来自燃烧器的排放量。 燃烧器包括一个混合器组件，该混合器组件包括一个先导式混合器，一个主混合器和一个在其间延伸的环形中心体。 该方法包括通过位于先导混合器内的至少一个旋流器将燃料和气流中的至少一种喷射到燃烧器中，并且通过位于主混合器内的至少一个旋流器将燃料喷射到燃烧器中，使得燃料被引导到 燃烧室主搅拌机下游。
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公开(公告)号：US20060042253A1
公开(公告)日：2006-03-02
申请号：US10931550
申请日：2004-09-01
Applicant: Douglas Fortuna , Timothy Held , David Kastrup
Inventor： Douglas Fortuna , Timothy Held , David Kastrup
IPC: F02C7/22
CPC classification number: F23L7/002 , F23D11/24 , F23D17/002 , F23R3/36
Abstract: A method enables a gas turbine engine to be assembled. The method comprises coupling a fuel nozzle within the engine to inject fuel into the engine, wherein the fuel nozzle includes three independent injection circuits arranged such that the second injection circuit is between the first and third injection circuits, coupling a liquid fuel source to a first injection circuit defined within the nozzle and including an annular discharge opening, and coupling a water source to one of the second injection circuit and the third injection circuits such that the water source is coupled in flow communication to an annular discharge opening.
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Patent Agency Ranking
公开(公告)号：US20050103021A1
公开(公告)日：2005-05-19
申请号：US10929909
申请日：2004-08-30
Applicant: Timothy Held , Mark Mueller , Jun Xu
Inventor： Timothy Held , Mark Mueller , Jun Xu
Abstract: A method for operating a gas turbine engine facilitates reducing an amount of emissions from a combustor. The combustor includes a mixer assembly including a pilot mixer, a main mixer, and an annular centerbody extending therebetween. The method comprises injecting at least one of fuel and airflow into the combustor through at least one swirler positioned within the pilot mixer, and injecting fuel into the combustor through at least one swirler positioned within the main mixer, such that the fuel is directed into a combustion chamber downstream from the main mixer.
Abstract translation: 用于操作燃气涡轮发动机的方法有助于减少来自燃烧器的排放量。 燃烧器包括一个混合器组件，该混合器组件包括一个先导式混合器，一个主混合器和一个在其间延伸的环形中心体。 该方法包括通过位于先导混合器内的至少一个旋流器将燃料和气流中的至少一种喷射到燃烧器中，并且通过位于主混合器内的至少一个旋流器将燃料喷射到燃烧器中，使得燃料被引导到 燃烧室主搅拌机下游。
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7.发明授权公开(公告)号：US09926811B2
公开(公告)日：2018-03-27
申请号：US14475678
申请日：2014-09-03
Applicant: Joshua Giegel , Timothy Held , Brett Bowan , Cameron Close
Inventor： Joshua Giegel , Timothy Held , Brett Bowan , Cameron Close
Abstract: Systems and methods for controlling a heat engine system are provided. One method includes initiating flow of a working fluid through a working fluid circuit having a high pressure side and a low pressure side by controlling a pump to pressurize and circulate the working fluid through the working fluid circuit and determining a configuration of the working fluid circuit by determining which of a plurality of waste heat exchangers and which of a plurality of recuperators to position in the high pressure side of the working fluid circuit. The method also includes determining, based on the determined configuration of the working fluid circuit, for each of a plurality of valves, whether to position each respective valve in an opened position, a closed position, or a partially opened position and actuating each of the plurality of valves to the determined opened position, closed position, or partially opened position.
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公开(公告)号：US20170362963A1
公开(公告)日：2017-12-21
申请号：US15536404
申请日：2015-12-07
Applicant: Steven R. HOSTLER , Timothy HELD , Katherine HART , Jason MILLER
Inventor： Steven R. Hostler , Timothy Held , Katherine Hart , Jason Miller
CPC classification number: F01K13/025 , F01D15/005 , F01D15/10 , F01D25/125 , F01K13/00 , F01K21/00 , F01K21/02 , F01K23/02 , F01K23/103 , F01K27/02 , Y02E20/14
Abstract: A pressure reduction system may include an alternator with a casing and a rotor positioned, at least in part, within a cavity defined by the casing. The pressure reduction system may also include a mass management system that includes a control tank configured to be maintained at a tank pressure lower than a cavity pressure within the cavity of the alternator, thereby forming a pressure differential. A first transfer conduit may transfer a working fluid from the cavity of the alternator to the control tank via the pressure differential. The mass management system may be positioned at an elevation above the alternator, and include a refrigeration loop configured to cool the working fluid contained within the control tank. A second transfer conduit may fluidly couple the alternator and the mass management system, and may transfer the cooled working fluid from the control tank to the cavity via gravitational force.
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9.发明申请公开(公告)号：US20060130486A1
公开(公告)日：2006-06-22
申请号：US11017186
申请日：2004-12-17
Applicant: Allen Danis , Timothy Held
Inventor： Allen Danis , Timothy Held
IPC: F23R3/42
CPC classification number: F23R3/06 , F23R3/002 , F23R2900/00014 , Y02T50/675
Abstract: A method enables the operation of a gas turbine engine. The method comprises channeling airflow into a cooling passageway defined between the combustor casing and an inner liner of the combustor, wherein the inner liner is fabricated from a plurality of panels coupled together, channeling airflow into a cooling passageway defined between the combustor casing and an outer liner of the combustor; wherein the outer liner is fabricated from a plurality of panels coupled together, and channeling dilution airflow into a combustion chamber defined between the inner and outer liners, through a plurality of openings formed within at least one panel within at least one of the inner liner panels and the outer liner panels, wherein the plurality of openings are non-circular.
Abstract translation: 一种方法使得能够操作燃气涡轮发动机。 该方法包括将气流引导到限定在燃烧器壳体和燃烧器的内衬之间的冷却通道中，其中内衬由多个联接在一起的面板制成，将气流引导到限定在燃烧器壳体和外壳之间的冷却通道 燃烧室内衬; 其中所述外衬套由耦合在一起的多个面板制成，并且通过形成在所述内衬板内的至少一个内的至少一个面板内的多个开口将稀释气流引导到限定在所述内衬层和所述内衬之间的燃烧室中 和外衬板，其中多个开口是非圆形的。
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公开(公告)号：US20170130614A1
公开(公告)日：2017-05-11
申请号：US15231047
申请日：2016-08-08
Applicant: Timothy Held , Jason D. Miller
Inventor： Timothy Held , Jason D. Miller
CPC classification number: F01K27/02 , F01D15/08 , F01D15/10 , F01K13/006 , F01K23/02 , F01K25/04 , F01K25/08 , F28B1/00 , F28B7/00 , H02K7/1823 , Y02T10/166
Abstract: A heat engine system and a method for cooling a fluid stream in thermal communication with the heat engine system are provided. The heat engine system may include a working fluid circuit configured to flow a working fluid therethrough, and a cooling circuit in fluid communication with the working fluid circuit and configured to flow the working fluid therethrough. The cooling circuit may include an evaporator in fluid communication with the working fluid circuit and configured to be in fluid communication with the fluid stream. The evaporator may be further configured to receive a second portion of the working fluid from the working fluid circuit and to transfer thermal energy from the fluid stream to the second portion of the working fluid.
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