| 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 | 鼓风加热器的燃烧装置 | CN95101499.4 | 1995-01-28 | CN1120151A | 1996-04-10 | 金寅圭; 金英秀; 金硕准; 沈成勋 |
| 一种鼓风煤油加热器的燃烧装置，它可防止焦油积聚在汽化器内并能提高煤油和空气的混合效率。该燃烧装置包括一个喷射易燃物料的喷射装置；在易燃物料燃烧之前使所喷射的易燃物料汽化的汽化装置；以及一个位于汽化装置中的分离装置，用于使所喷射的易燃物料分流并使分流的易燃物料在彼此相反的方向上产生旋流。 | ||||||
| 2 | 用于给储能器加热装置充电的设备、用于该设备的喷嘴以及用于产生热能的方法 | CN200980151298.3 | 2009-12-18 | CN102256819B | 2014-11-26 | 伯恩哈德·阿特尔斯梅尔; 莱因霍尔德·芬克; 赫尔穆特·普夫吕格尔迈尔; 安德烈亚斯·普里林格; 金特·斯克拉斯基 |
| 本发明涉及一种用于给储能器(2)充电的充电设备(1)，其具有发电装置(3)、充电单元(4)以及其他部件，其中发电装置(3)由热源形成，发电装置(3)包括至少一个连接至燃料供应管线(10)的燃烧器(8)和热电元件(9)，以及用于这种充电设备(1)的燃烧器(8)、加热部件(31)和喷嘴(20)。根据本发明，能实现恒定稳定的燃烧并且允许自维持的蒸发过程，其中发电装置(3)、充电单元(4)以及所述其他部件布置于共用壳体(5)中，其中用于所供应燃料的蒸发器(28)布置于燃烧器(8)的燃烧器壳体(19)的下部中并且壳体(5)的后壁(14)设计为用于将热排出的元件。 | ||||||
| 3 | 用于给储能器加热装置充电的设备、用于该设备的喷嘴以及用于产生热能的方法 | CN200980151298.3 | 2009-12-18 | CN102256819A | 2011-11-23 | 伯恩哈德·阿特尔斯梅尔; 莱因霍尔德·芬克; 赫尔穆特·普夫吕格尔迈尔; 安德烈亚斯·普里林格; 金特·斯克拉斯基 |
| 本发明涉及一种用于给储能器(2)充电的充电设备(1)，其具有发电装置(3)、充电单元(4)以及其他部件，其中发电装置(3)由热源形成，发电装置(3)包括至少一个连接至燃料供应管线(10)的燃烧器(8)和热电元件(9)，以及用于这种充电设备(1)的燃烧器(8)、加热部件(31)和喷嘴(20)。根据本发明，能实现恒定稳定的燃烧并且允许自维持的蒸发过程，其中发电装置(3)、充电单元(4)以及所述其他部件布置于共用壳体(5)中，其中用于所供应燃料的蒸发器(28)布置于燃烧器(8)的燃烧器壳体(19)的下部中并且壳体(5)的后壁(14)设计为用于将热排出的元件。 | ||||||
| 4 | 石油燃烧装置 | CN96119255.0 | 1996-10-11 | CN1152091A | 1997-06-18 | 李京植 |
| 本发明提供了既能使石油燃料扩散喷射又能使混合气完全燃烧的石油燃烧装置，该装置具有从一侧向内侧突出以减小内部体积的部分，以便即使用小热量也容易预热侧壁部分的内侧燃烧室本体；用于使石油燃料在上述内侧燃烧室内扩散的喷嘴罩的喷嘴管；用于固定该喷嘴管并导入燃烧用空气的喷嘴本体；固定在该喷嘴上为了通过汾丘里效应使燃烧用空气高速喷射而在内侧上具有由两段喇叭状部分组成的流入口和流出口的汾丘里管。 | ||||||
| 5 | Liquid fuel combustor with an improved burner assembly | US738539 | 1991-07-31 | US5156543A | 1992-10-20 | Seung-Gyo Jeung |
| A liquid fuel combustor comprises a gasification promoter unit housed within a heated burner body for enhancing the gasification capability of the atomized fuel. The gasification promoter unit is provided with a downwardly convex surface. A fuel nozzle has its outlet facing toward that surface to direct fuel thereagainst. A heater is embedded in the promoter unit to heat the fuel particulates emerging from the fuel nozzle. | ||||||
| 6 | Vaporizer for liquid fuel for producing a fuel-air mixture | US888750 | 1986-07-22 | US4758153A | 1988-07-19 | Siegfried Forster |
| A vaporizer for liquid fuel for producing a fuel-air mixture including a orization member for the fuel and which is arranged within a flow chamber for combustion air. The surface of the vaporization member which is streamed against by the combustion air is moistened with fuel. The vaporizer incorporates a vaporizing member arranged within a flow chamber for combustion air, wherein the vaporizing member includes a rotatable or circulating filling or charge of balls whose temperature can be adjusted through heat conduction received from the walls of the flow chamber. Thereby, through the revolving or circulation of the ball filling, and the heat transfer to the balls which are currently at the edge of the ball filling in heat-conductive communication with the temperature-regulated walls of the flow chamber, there takes place a rapid and uniform heating of the ball filling. The large vaporization surface which is made available through the ball filling, additionally allows for the formation of relatively thin fuel films, which can be heated while concurrently avoiding excessive temperatures. The revolving or circulating of the balls additionally provides for a constant movement and displacement of the vaporizing member, as a result of which there can be avoided striated or streaky flows which lead to a non-uniform or irregular formation of the fuel-air mixture. | ||||||
| 7 | Machinery for molding headpiece for collapsible tube including a chilled wiper | US326325 | 1981-12-01 | US4492548A | 1985-01-08 | Warren N. Hubert |
| A headpiece for a collapsible tube is a unitary member made up of two different plastics, each plastic providing a different property for the headpiece. The headpiece is formed by extruding on top of one another a first torus like annulus of a first plastic and a second torus like annulus of a second plastic. The two plastic annuli are simultaneously molded to form the headpiece. One plastic forms, primarily, the outer portion of the headpiece and the other plastic forms, primarily, the inner portion of the headpiece.The machine for molding the plastic head includes a work table rotatably indexed from station to station at which various operations are performed. The mandrel which holds the cylindrical body, to which the head is molded, is movable from an inboard position to an outboard position so that operations can be performed relative to it. The molding operation is performed at the inboard position. The loading, extruding, capping and ejection operations are performed at the outboard position. The nozzle of the plastic extruder includes a chilled wiper for wiping an extruded plastic annulus into the mold cavity. | ||||||
| 8 | Liquid fuel burner for burning liquid fuel in gasified form | US41818 | 1979-05-23 | US4247282A | 1981-01-27 | Kingo Miyahara |
| A liquid fuel burner for burning liquid fuel in gasified form including a cylindrical main body having a flame blowoff nozzle and an inner bottom wall at opposite ends, a gas chamber, a combustion plate formed with a multitude of gasified fuel blowing openings, a fuel gasifying member, a fuel diffusing member, an air supply duct, a fuel supply line, an air ejection chamber and a rotary shaft supporting the fuel gasifying member and fuel diffusing member for rotation within the cylindrical main body. An annular wall is secured to and extends inwardly from the inner wall surface of the combustion plate in a position nearer to the inner bottom wall than the gasified fuel blowing openings, and a liquefied fuel flow preventing plate is secured at one end to the inner wall surface of the cylindrical main body in a position near to the flame blowoff nozzle and free at the other end to define a liquefied fuel sump between the inner wall surface of the main body and the liquefied fuel flow preventing plate. The fuel diffusing member is formed at its base with ventilating windows for permitting air to flow therethrough. The fuel supply line has a forward end disposed close to the outer circumferential surface of the fuel diffusing member and spaced apart therefrom by a multiple-dimension fuel supply gap. | ||||||
| 9 | Combustion apparatus | US600378 | 1975-07-30 | US4045159A | 1977-08-30 | Atsuyoshi Nishi; Katuo Yashiro |
| A combustion apparatus having a mixing chamber, a combustion chamber, a flame holes plate disposed therebetween for forming a combustion flame at a flame projecting aperture thereof, a choke plate on the mixing chamber side of the flame holes plate in concentric relation thereto and having a central opening smaller than that of the flame holes plate for the purpose of keeping the velocity of the mixed combustible gas lower at the periphery than at the central parts, and a mixing impeller having central openings for directly passing part of the air provided for combustion to the central part of the choke plate opening for the purpose of increasing the concentration of the mixed combustible gas at the peripheral parts of the flame holes plate in the combustion chamber. | ||||||
| 10 | Recirculating burner | US612670 | 1975-09-12 | US3994665A | 1976-11-30 | Henry J. Young |
| A recirculating burner for burning a vaporizable liquid fuel comprising a housing, a combustion chamber in the housing, with inlet and outlet, a vaporizing chamber, with inlet and outlet, an air inlet for directing air under pressure into the combustion chamber, a fuel inlet atomizer, adjacent to the vaporizing chamber inlet, for automizing vaporizable liquid fuel and directing the fuel into the vaporizing chamber, a gaseous fuel inlet for feeding gaseous fuel into the combustion chamber, a first passage interconnecting the combustion chamber toward the combustion chamber outlet with the vaporizing chamber inlet, for receiving hot combustion gases from the combustion chamber, a second passage effectively interconnecting the vaporizing chamber outlet with the combustion chamber inlet, the air inlet communicating with the second passage, and a vortex generator at the interface of the fuel inlet atomizer, the first passage, and the vaporizing chamber inlet, the generator being rotatable with respect to the housing between two positions, a first open position in which the generator receives hot gases from the first passage and swirls them into a vortex, into which the fuel atomizer directs atomized fuel, for vaporization of the fuel by the gases in the generator and vaporizing chamber, and the first passage, generator, vaporizing chamber, and second passage together define a recirculation path for hot combustion gases from the combustion chamber, and a second closed position in which the generator blocks the recirculation path, and the gaseous fuel inlet feeds gaseous fuel into the combustion chamber for burning therein. | ||||||
| 11 | Burner for burning liquid fuel in gasified form | US568723 | 1975-04-16 | US3986815A | 1976-10-19 | Kingo Miyahara |
| A burner wherein a fuel gasifying member is non-rotatably mounted in a main body of the burner and maintained in communication with a gas chamber formed in an outer marginal portion of the main body of the burner, and liquid fuel scattering means is rotatably mounted at an open end portion of the fuel gasifying member for scattering a liquid fuel in minuscule particles into the interior of the fuel gasifying member and the main body of the burner through a scattering gap. The liquid fuel thus scattered in the main body is ignited and burns to heat the fuel gasifying member in which the fuel supplied by the liquid fuel scattering means under the influence of an air blast supplied under pressure through an air supply duct is quickly gasified and forms a mixture of gasified fuel and air which is ejected through the gas chamber to sustain combustion of the liquid fuel in gasified form. A cooling chamber may be provided adjacent an inner wall plate of the main body of the burner. Heat dissipating fins may be attached to inner periphery of the non-rotatable fuel gasifying member. A cylindrical air guide may be arranged within the fuel gasifying member and maintained in communication with the air supply duct, with a narrow gasified fuel air mixture passageway being formed between the cylindrical air guide and the fuel gasifying member and connected to the gas chamber. | ||||||
| 12 | Fuel oil gasification burner | US32500863 | 1963-11-20 | US3238991A | 1966-03-08 | OTTO GOLDMANN; HEINRICH-HEINE-STRAS; OTTO HIMSTEDT; ERHARD SCHWARZE |
| 13 | Pressurized | US3123302D | US3123302A | 1964-03-03 | ||
| 14 | Hydrocarbon burner | US71050734 | 1934-02-09 | US2121271A | 1938-06-21 | SZABO BASIL V |
| 15 | Oil-burner | US27128719 | 1919-01-15 | US1327571A | 1920-01-06 | RAY WILLIAM R |
| 16 | Combustion device of fan heater | US380709 | 1995-01-30 | US5628628A | 1997-05-13 | In K. Kim; Young S. Kim; Seock J. Kim; Sung H. Shim |
| Combustion device of a kerosene fan heater, which can inhibit accumulation of tar inside of the carburetor and can improve a mixing efficiency of fuel of kerosene and air.The combustion device includes a spraying means for spraying flammable substance, a vaporizing means for vaporizing the sprayed flammable substance before burning the flammable substance, and a dividing means disposed in the vaporizing means for dividing the sprayed flammable substance and making the divided flammable substance swirl in opposite direction to each other. | ||||||
| 17 | Clean burning burner, particularly for combustion of gasified liquid fuel, such as fuel oil, or of gas | US22721 | 1993-02-24 | US5346391A | 1994-09-13 | Jorg Fullemann; Heinrich Boner |
| To provide gasification of liquid fuel which is admitted by an atomizing nozzle (11, 13) into a gasification space (66). A deflection element (31) is located spaced from an air inlet (55) in order to deflect the mixture of air, recirculated combustion gases and gasified fuel in the gasification space. A flame tube (21) provides for a first (I) recirculation path for hot gases towards a recirculation openings (49). A second recirculation path (II) extends through openings (57, 61, 59) into the deflection element itself which, preferably, is a hollow, essentially shallow conical deflection structure. The deflection element in combination with the flame tube (21) causes recirculation of gases through the first recirculation path (I) back into the gasification space (66). Thus, all structural elements of the gasification space are subjected to recirculated hot combustion gases, so that no droplets from the atomizing burner (13) can adhere, and coke on structural elements. The efficient recirculation together with the complex stream relationships, caused by the braking effect of the recirculation element, and eddies and turbulences arising from over-pressure air supplied by the air inlet (55), result in effectively complete gasification of fuels within the gasification space (66) the end of the flame tube burns blue, with practically no NO.sub.x even if no real gasifier structure is present. The flame, expanding in radial direction due to the deflection element, near formation, and effectively devoid of unburned hydrocarbons. | ||||||
| 18 | Fuel injector for a gas turbine engine | US789276 | 1991-11-08 | US5241818A | 1993-09-07 | Jack R. Shekleton; Robert W. Smith |
| Difficulties with fuel atomization at low fuel flow rates in gas turbine fuel injection systems may be overcome by use of an impingement injector (52) including a cylindrical orifice (64, 94, 114) that is smooth, straight and uninterrupted by burrs or other disturbances having an exit opening (68, 96, 118) transverse to the axis of the orifice (64, 94, 114) and facing an impingement surface (72, 101, 126) that is planar and spaced from the exit opening (68, 96, 118). | ||||||
| 19 | Premixed secondary fuel nozzle with integral swirler | US899586 | 1992-06-18 | US5193346A | 1993-03-16 | Masayoshi Kuwata; Cheryl Mele; Richard J. Borkowicz |
| A dual mode, dual stage low NOx combustor, includes a primary combustion chamber and a secondary combustion chamber separated by a throat region of reduced diameter. Fuel is input into the primary combustors by an annular array of diffusion type nozzles whereas in accordance with the invention, fuel is input into the secondary combustor by a central combination premix and diffusion nozzle. A premix swirler annulus is located upstream of a plurality of fuel distribution tubes of the combined premix and diffusion nozzle. | ||||||
| 20 | Turbine engine with pin injector | US379548 | 1989-07-13 | US5063745A | 1991-11-12 | Jack R. Shekleton; Steven A. Sachrison; Michael W. Sledd |
| Improved fuel atomization for turbine engines operating at low fuel flows and at high altitudes is accomplished in an engine 10 having an annular combustor 12 by utilizing fuel injectors 18 provided with fuel supply tubes 24 disposed within air tubes 20 wherein the fuel supply tubes 24 each have an exit orifice 26 internally of the corresponding air tube 20 and upstream of an exit orifice 22 thereof with a fuel impingement surface 28 being provided within the air tube 20 in confronting relation to the exit orifice 26 of the fuel supply tube 24 to produce a conical fuel film 36 subjected to pressurized air to enhance fuel atomization. | ||||||
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