| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | 油炉灭火装置 | CN200980119741.9 | 2009-02-06 | CN102047043B | 2012-07-04 | 金哲; 金载勋; 金载镐 |
| 本发明涉及一种在固芯式油炉翻倒或者地震发生时通过截断给油管来对油炉进行紧急灭火的装置，其由无需电源的结构形成，可以节省成本、无故障担忧，在对油炉灭火后可轻松恢复到运行前的状态。本发明提供的固芯式油炉，包括：外壳(40)，该外壳(40)设置于所述底座(10)上，并且为六面体结构；杠杆(50)，该杠杆(50)可上下摆动并支撑设置于所述外壳(40)的底板(41b)上，在所述杠杆一端的底面和所述底板(41b)之间设置有弹性支撑结构(53)，在所述杠杆的另一端和所述底板(41b)之间设置有由耐热性柔性材料形成的所述给油管(22)；重量结构(60)，该重量结构(60)包括在所述上板(41a)和杠杆(50)的一端之间，并通过弹性结构(61)设置为对向部面接触的上部重量体(62a)和下部重量体(62b)，所述上部重量体(62a)的上端和所述下部重量体(62b)的下端面接触设置于所述上板(41a)和杠杆(50)的一端，在所述上部重量体(62a)和所述下部重量体(62b)之中的至少一个受到超过预定值的冲击力时，所述重量结构被折曲；归位杆(70)，该归位杆(70)的下端连接于所述杠杆(50)，其自由端凸出设置于所述上板(41a)外部。 | ||||||
| 2 | 分流器组件 | CN201210191823.8 | 2012-06-12 | CN102829488B | 2016-02-24 | E.齐林斯基 |
| 本发明涉及装有分流器组件的燃烧器燃料控制系统。一种分流器组件，包括分流阀和平衡阀。分流阀包括被设置用于接收燃料流的分流腔和设置在分流腔内的活塞装置，并且活塞装置被选择性定位以用于将分流腔内的燃料流分流至第一分流阀端口和第二分流阀端口内。平衡阀被流体连接至分流阀并且被设置用于接收第一部分燃料流和第二部分燃料流。平衡阀包括平衡腔和设置在平衡腔内的平衡装置，并且平衡装置被选择性定位以用于以第三压力将第一部分燃料流引入第一平衡腔端口并且以第四压力将第二部分燃料流引入第二平衡腔端口，从而使第一压力约等于第二压力。 | ||||||
| 3 | 装有分流器组件的燃烧器燃料控制系统 | CN201210191823.8 | 2012-06-12 | CN102829488A | 2012-12-19 | E.齐林斯基 |
| 本发明涉及装有分流器组件的燃烧器燃料控制系统。一种分流器组件，包括分流阀和平衡阀。分流阀包括被设置用于接收燃料流的分流腔和设置在分流腔内的活塞装置，并且活塞装置被选择性定位以用于将分流腔内的燃料流分流至第一分流阀端口和第二分流阀端口内。平衡阀被流体连接至分流阀并且被设置用于接收第一部分燃料流和第二部分燃料流。平衡阀包括平衡腔和设置在平衡腔内的平衡装置，并且平衡装置被选择性定位以用于以第三压力将第一部分燃料流引入第一平衡腔端口并且以第四压力将第二部分燃料流引入第二平衡腔端口，从而使第一压力约等于第二压力。 | ||||||
| 4 | 油炉灭火装置 | CN200980119741.9 | 2009-02-06 | CN102047043A | 2011-05-04 | 金哲; 金载勋; 金载镐 |
| 本发明涉及一种在固芯式油炉翻倒或者地震发生时通过截断给油管来对油炉进行紧急灭火的装置，其由无需电源的结构形成，可以节省成本、无故障担忧，在对油炉灭火后可轻松恢复到运行前的状态。本发明提供的固芯式油炉，包括：外壳(40)，该外壳(40)设置于所述底座(10)上，并且为六面体结构；杠杆(50)，该杠杆(50)可上下摆动并支撑设置于所述外壳(40)的底板(41b)上，在所述杠杆一端的底面和所述底板(41b)之间设置有弹性支撑结构(53)，在所述杠杆的另一端和所述底板(41b)之间设置有由耐热性柔性材料形成的所述给油管(22)；重量结构(60)，该重量结构(60)包括在所述上板(41a)和杠杆(50)的一端之间，并通过弹性结构(61)设置为对向部面接触的上部重量体(62a)和下部重量体(62b)，所述上部重量体(62a)的上端和所述下部重量体(62b)的下端面接触设置于所述上板(41a)和杠杆(50)的一端，在所述上部重量体(62a)和所述下部重量体(62b)之中的至少一个受到超过预定值的冲击力时，所述重量结构被折曲；归位杆(70)，该归位杆(70)的下端连接于所述杠杆(50)，其自由端凸出设置于所述上板(41a)外部。 | ||||||
| 5 | 用于涡轮机组的燃料喷射器 | CN201380009834.2 | 2013-02-12 | CN104114834B | 2016-11-16 | 埃米莉·夏洛特·波赛; 乔斯·罗纳德·罗德里格斯 |
| 用于涡轮机组的燃料喷射器。本发明涉及用于涡轮机组的燃料喷射器，包括本体(2)，该本体(2)包括压力下燃料进入的装置；截止阀，提供该截止阀以供给主燃料回路(31、20)；以及安装在截止阀下游的计量阀(15)，提供该计量阀(15)以供给次级燃料回路(17、21)。喷射器(1)包括至少一个泄漏通道(35)，该泄漏通道(35)由例如，螺纹形成，该螺纹从位于截止阀(7)下游和计量阀(15)上游的区域(32)延伸到位于计量阀(15)下游的区域(17)，以在次级回路(17、21)中产生永久的泄漏流。 | ||||||
| 6 | 燃烧器及燃气轮机 | CN201280070543.X | 2012-11-30 | CN104169651B | 2016-08-17 | 中村聪介; 松村嘉和; 片野光; 谷口健太; 山崎博行 |
| 本发明的燃烧器具备：内筒(12)，从外部供给空气(A)；第一喷嘴(14)，沿着内筒(12)的内周呈环状设置多个，分别将空气(A)与燃料(f)的预混合气(M)向内筒(12)的内部供给；以及尾筒(15)，在基端(15b)连接内筒(12)，并且使从第一喷嘴(14)供给的预混合气(M)燃烧而形成随着朝向轴向前端侧而向外周侧扩展的火焰面(F)，各第一喷嘴(14)使燃料浓度绕着该第一喷嘴(14)的中心轴变化地供给预混合气(M)，以使得在轴向上火焰面(F)成为均匀的温度。 | ||||||
| 7 | 燃烧器及燃气轮机 | CN201280070543.X | 2012-11-30 | CN104169651A | 2014-11-26 | 中村聪介; 松村嘉和; 片野光; 谷口健太; 山崎博行 |
| 本发明的燃烧器具备：内筒(12)，从外部供给空气(A)；第一喷嘴(14)，沿着内筒(12)的内周呈环状设置多个，分别将空气(A)与燃料(f)的预混合气(M)向内筒(12)的内部供给；以及尾筒(15)，在基端(15b)连接内筒(12)，并且使从第一喷嘴(14)供给的预混合气(M)燃烧而形成随着朝向轴向前端侧而向外周侧扩展的火焰面(F)，各第一喷嘴(14)使燃料浓度绕着该第一喷嘴(14)的中心轴变化地供给预混合气(M)，以使得在轴向上火焰面(F)成为均匀的温度。 | ||||||
| 8 | 用于涡轮机组的燃料喷射器 | CN201380009834.2 | 2013-02-12 | CN104114834A | 2014-10-22 | 埃米莉·夏洛特·波赛; 乔斯·罗纳德·罗德里格斯 |
| 用于涡轮机组的燃料喷射器。本发明涉及用于涡轮机组的燃料喷射器，包括本体(2)，该本体(2)包括压力下燃料进入的装置；截止阀，提供该截止阀以供给主燃料回路(31、20)；以及安装在截止阀下游的计量阀(15)，提供该计量阀(15)以供给次级燃料回路(17、21)。喷射器(1)包括至少一个泄漏通道(35)，该泄漏通道(35)由例如，螺纹形成，该螺纹从位于截止阀(7)下游和计量阀(15)上游的区域(32)延伸到位于计量阀(15)下游的区域(17)，以在次级回路(17、21)中产生永久的泄漏流。 | ||||||
| 9 | FUEL INJECTOR FOR A TURBINE ENGINE | US14378797 | 2013-02-12 | US20150007572A1 | 2015-01-08 | Emilie Charlotte Pousseo; Jose Roland Rodrigues |
| A fuel injector for a turbine engine, the injector including a body including a mechanism for admitting fuel under pressure, a stop valve for feeding a primary fuel circuit, and a metering valve mounted downstream from the stop valve for feeding a secondary fuel circuit. The injector further includes at least one leakage channel, that can be formed by a thread, that extends from a zone situated downstream from the stop valve and upstream from the metering valve to a zone situated downstream from the metering valve to generate a permanent leakage flow in the secondary circuit. | ||||||
| 10 | COMBUSTOR FUEL CONTROL SYSTEMS WITH FLOW DIVIDER ASSEMBLIES | US13159175 | 2011-06-13 | US20120312378A1 | 2012-12-13 | Edward Zielinski |
| A flow divider assembly includes a dividing valve and a balancing valve. The dividing valve includes a dividing cavity configured to receive a flow of fuel and a piston device arranged within the dividing cavity and selectively positioned to divide the flow of fuel in the dividing cavity into the first dividing valve port and the second dividing valve port. The balancing valve is fluidly coupled to the dividing valve and configured to receive the first portion and the second portion of the flow. The balancing valve includes a balancing cavity and a balancing device arranged within the balancing cavity and selectively positioned to direct the first portion of the flow into the first balancing cavity port at a third pressure and the second portion of the flow into the second balancing cavity port at a fourth pressure such that the first pressure is approximately equal to the second pressure. | ||||||
| 11 | SUPERCRITICAL OR MIXED PHASE MULTI-PORT FUEL INJECTOR | US13337738 | 2011-12-27 | US20120167580A1 | 2012-07-05 | Timothy C. Roesler |
| A system includes a turbine engine with a fueling system including a valve fluidly coupled to a fuel supply on an upstream side and fluidly coupled to fueling passages on a downstream side. The valve maintains the fuel supply at a pressure greater than an ambient pressure. The system includes nozzle exits corresponding to the fueling passages, and the fueling passages flow fuel from the valve to each of the nozzle exits monotonically downward. The valve is a check valve or a controlled valve. The valve maintains the fuel supply at a pressure such that fuel in the fuel supply is a continuous fluid phase. The fuel leaves the nozzle exits to the combustion chamber of the turbine engine. | ||||||
| 12 | Turbine engine fuel injector with permanent leakage flow | US14378797 | 2013-02-12 | US09494079B2 | 2016-11-15 | Emilie Charlotte Pousseo; Jose Roland Rodrigues |
| A fuel injector for a turbine engine, the injector including a body including a mechanism for admitting fuel under pressure, a stop valve for feeding a primary fuel circuit, and a metering valve mounted downstream from the stop valve for feeding a secondary fuel circuit. The injector further includes at least one leakage channel, that can be formed by a thread, that extends from a zone situated downstream from the stop valve and upstream from the metering valve to a zone situated downstream from the metering valve to generate a permanent leakage flow in the secondary circuit. | ||||||
| 13 | METHOD AND SYSTEM FOR EFFLUENT COMBUSTION | US15021570 | 2013-09-13 | US20160230988A1 | 2016-08-11 | Vladimir Nikolaevich Ulyanov; Roman Vladimirovich Korkin; Alexander Nikolaevich Cheremisin; Vladimir Konstantinovich Khan |
| Methods and systems of burning a multi-phase hydrocarbon fluid include determining a water content of the multi-phase hydrocarbon fluid, communicating the multiphase hydrocarbon fluid to a fuel port of a burner in a primary fuel flow, initiating a flame at the burner to combust the multi-phase hydrocarbon fluid, communicating an auxiliary fuel source to the burner fuel port in an auxiliary fuel flow, and controlling the primary and auxiliary fuel flows based on the water content of the multi-phase hydrocarbon fluid. | ||||||
| 14 | Combustor fuel control systems with flow divider assemblies | US13159175 | 2011-06-13 | US08464740B2 | 2013-06-18 | Edward Zielinski |
| A flow divider assembly includes a dividing valve and a balancing valve. The dividing valve includes a dividing cavity configured to receive a flow of fuel and a piston device arranged within the dividing cavity and selectively positioned to divide the flow of fuel in the dividing cavity into the first dividing valve port and the second dividing valve port. The balancing valve is fluidly coupled to the dividing valve and configured to receive the first portion and the second portion of the flow. The balancing valve includes a balancing cavity and a balancing device arranged within the balancing cavity and selectively positioned to direct the first portion of the flow into the first balancing cavity port at a third pressure and the second portion of the flow into the second balancing cavity port at a fourth pressure such that the first pressure is approximately equal to the second pressure. | ||||||
| 15 | Digester of oil stove | JP2011516103 | 2009-02-06 | JP2011525964A | 2011-09-29 | キム，ジェフン; キム，ジェホ; キム，チュル |
| The present invention relates to a device for rapidly extinguishing a fixed-wick oil stove by closing off an oil-supply tube when the oil stove is overturned or an earthquake occurs. More specifically, it relates to a device of this type which is formed using just a construction having no need for an electrical power source, which reduces costs, which entails no risk of breakdown, and which after the oil stove has been extinguished can straightforwardly be restored to the state prior to operation. The present invention is a fixed-wick oil burner which comprises: a hexahedral housing (40) provided on a support (10); a lever (50) which is supported in such a way as to be able to perform a seesaw movement on a floor plate (41b) of the housing (40), and which is provided with a resilient support member (53) between its under-surface at one end and the floor plate (41b), and which also has positioned, between its other end and the floor plate (41b), an oil-supply tube (22) formed of a heat-resistant flexible material; a weighting member (60) which is provided between an upper plate (41a) and one end of the lever (50) in such a way that a resilient member (61) is used to force face-to-face contact between facing parts, an upper weighting body (62a) and a lower weighting body (62b), and in such a way that the upper end of the upper weighting body (62a) and the lower end of the lower weighting body (62b) come into face-to-face contact with the upper plate (41a) and one end of the lever (50), and which is arranged in such a way that it gives way when a shock force of more than a certain value is transmitted to one or other of the upper and lower weighting bodies (62a) or (62b); and a restoring rod (70) which is connected to the lever (50), with a free end projecting outside the upper plate (41a). | ||||||
| 16 | Combustor and gas turbine | US13687587 | 2012-11-28 | US09926845B2 | 2018-03-27 | Sosuke Nakamura; Yoshikazu Matsumura; Hikaru Katano; Kenta Taniguchi; Hiroyuki Yamasaki |
| A combustor according to the invention includes a combustor basket to which air A is supplied from the outside, a plurality of first nozzles that are annularly provided along the inner periphery of the combustor basket and that supply premixed gas M of the air and fuel to the inside of the combustor basket, and a transition piece in which the combustor basket is connected to a base end thereof and which burns the premixed gas supplied from the first nozzles, thereby forming a flame front spread to the outer periphery side toward the leading end in an axial direction, wherein each first nozzle supplies the premixed gas with fuel concentration changed around the center axis of the first nozzle such that the flame front has a uniform temperature in the axial direction. | ||||||
| 17 | Supercritical or mixed phase multi-port fuel injector | US13337738 | 2011-12-27 | US09360219B2 | 2016-06-07 | Timothy C. Roesler |
| A system includes a turbine engine with a fueling system including a valve fluidly coupled to a fuel supply on an upstream side and fluidly coupled to fueling passages on a downstream side. The valve maintains the fuel supply at a pressure greater than an ambient pressure. The system includes nozzle exits corresponding to the fueling passages, and the fueling passages flow fuel from the valve to each of the nozzle exits monotonically downward. The valve is a check valve or a controlled valve. The valve maintains the fuel supply at a pressure such that fuel in the fuel supply is a continuous fluid phase. The fuel leaves the nozzle exits to the combustion chamber of the turbine engine. | ||||||
| 18 | COMBUSTOR AND GAS TURBINE | US13687587 | 2012-11-28 | US20130219898A1 | 2013-08-29 | Sosuke Nakamura; Yoshikazu Matsumura; Hikaru Katano; Kenta Taniguchi; Hiroyuki Yamasaki |
| A combustor according to the invention includes a combustor basket to which air A is supplied from the outside, a plurality of first nozzles that are annularly provided along the inner periphery of the combustor basket and that supply premixed gas M of the air and fuel to the inside of the combustor basket, and a transition piece in which the combustor basket is connected to a base end thereof and which burns the premixed gas supplied from the first nozzles, thereby forming a flame front spread to the outer periphery side toward the leading end in an axial direction, wherein each first nozzle supplies the premixed gas with fuel concentration changed around the center axis of the first nozzle such that the flame front has a uniform temperature in the axial direction. | ||||||
| 19 | FIRE-EXTINGUISHING DEVICE FOR AN OIL STOVE | US12997607 | 2009-02-06 | US20110088919A1 | 2011-04-21 | Chul Kim; Jae hoon Kim; Jae ho Kim |
| The present invention relates to a device for rapidly extinguishing a fixed-wick oil stove by closing off an oil-supply tube when the oil stove is overturned or an earthquake occurs. More specifically, it relates to a device of this type which is formed using just a construction having no need for an electrical power source, which reduces costs, which entails no risk of breakdown, and which after the oil stove has been extinguished can straightforwardly be restored to the state prior to operation. The present invention is a fixed-wick oil burner which comprises: a hexahedral housing (40) provided on a support (10); a lever (50) which is supported in such a way as to be able to perform a seesaw movement on a floor plate (41b) of the housing (40), and which is provided with a resilient support member (53) between its under-surface at one end and the floor plate (41b), and which also has positioned, between its other end and the floor plate (41b), an oil-supply tube (22) formed of a heat-resistant flexible material; a weighting member (60) which is provided between an upper plate (41a) and one end of the lever (50) in such a way that a resilient member (61) is used to force face-to-face contact between facing parts, an upper weighting body (62a) and a lower weighting body (62b), and in such a way that the upper end of the upper weighting body (62a) and the lower end of the lower weighting body (62b) come into face-to-face contact with the upper plate (41a) and one end of the lever (50), and which is arranged in such a way that it gives way when a shock force of more than a certain value is transmitted to one or other of the upper and lower weighting bodies (62a) or (62b); and a restoring rod (70) which is connected to the lever (50), with a free end projecting outside the upper plate (41a). | ||||||
| 20 | タービンエンジンの燃料噴射器 | JP2014558177 | 2013-02-12 | JP6195581B2 | 2017-09-13 | プセオ,エミリー・シャルロット; ロドリグ,ジョゼ・ロラン |
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