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公开(公告)号：US20090007543A1
公开(公告)日：2009-01-08
申请号：US11198053
申请日：2005-08-04
申请人： Thomas J. Mueller
发明人： Thomas J. Mueller
CPC分类号： F02K9/52 , F23L7/007 , F23L2900/07004 , Y02E20/344
摘要： A bi-propellant rocket engine may include a primary propellant flowing in a central passageway, a secondary propellant flowing in a secondary passageway generally coaxial with central passageway and a pintle tip having a central chamber sidewall coaxial with the primary passageway and surrounding a central chamber, the central chamber sidewall having a first plurality of apertures there through so that some of the primary propellant exits the central chamber transverse to the flow of the secondary propellant in the secondary passageway. The pintle tip may have a secondary chamber sidewall, substantially thicker than the primary chamber sidewall, surrounding a secondary chamber downstream of and in fluid communication with the primary chamber, the secondary chamber sidewall having a second plurality of apertures there through so that some of the primary propellant exits the secondary chamber transverse to the flow of the secondary propellant in the secondary passageway. The pintle tip may have an end wall generally traverse to the flow of the primary propellant in the central passageway and adjacent the secondary chamber sidewall so that the flow of primary propellant through the secondary chamber sidewall cools a downstream face of the end wall during combustion of the mixed propellants adjacent the downstream face of the end wall. The pintle tip may be used for mixing a first liquid with a second liquid.
摘要翻译： 双推进剂火箭发动机可以包括在中心通道中流动的主推进剂，在与中心通道大致同轴的次级通道中流动的次级推进剂和具有与主通道同轴并围绕中心室的中心室侧壁的枢轴端头， 中央室侧壁具有第一多个孔，通过这些孔，使得一些主推进剂在第二通道中横向于二次推进剂的流动而离开中心室。 枢轴端部可以具有基本上比主室侧壁更厚的次级室侧壁，围绕主室的下游并与主室流体连通，次级室侧壁具有穿过第二多个孔的部分， 主推进剂在第二通道中离开辅助室横向于二次推进剂的流动。 枢轴端头可以具有通常在中心通道中并且邻近次级室侧壁的主推进剂流动的端壁，使得通过次级室侧壁的初级推进剂的流动在端壁的燃烧期间冷却端壁的下游面 混合的推进剂邻近端壁的下游面。 针尖可用于将第一液体与第二液体混合。
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公开(公告)号：US20050107652A1
公开(公告)日：2005-05-19
申请号：US10487608
申请日：2003-11-13
IPC分类号： A62D3/38 , A62D101/22 , B01D53/70 , F23G5/12 , F23G5/16 , F23G7/06 , F23J15/04 , F23L7/00 , F23M9/06 , B01J8/04 , A62D3/00 , B01J10/00
CPC分类号： F23L7/00 , A62D3/38 , A62D2101/22 , A62D2203/02 , B01D53/70 , B01D2257/2064 , F23G5/12 , F23G5/16 , F23G7/065 , F23J15/04 , F23J2215/301 , F23L2900/07004 , F23M9/06 , Y02E20/344 , Y10S588/90
摘要： An equipment for making PCB nontoxic comprises: a first burn furnace 10 for burning an oil containing the PCB with auxiliary fuel: a second oxidation reaction unit 12, connecting to the first burn furnace 10 under sealing, comprising a supply source of a solution of metallic phthalocyanine derivatives and a supply source of the solution of the oxygen supply compound.
摘要翻译： 一种用于制造PCB无毒的设备包括：用辅助燃料燃烧含有PCB的油的第一燃烧炉10：在密封下连接到第一燃烧炉10的第二氧化反应单元12，包括金属溶液的供应源 酞菁衍生物和供氧化合物溶液的供应源。
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公开(公告)号：US06212878B1
公开(公告)日：2001-04-10
申请号：US09410872
申请日：1999-10-01
申请人： Alexei Pogosovich Adzhian , Vladimir Jurievich Bogushev , Alexandr Mikhailovich Samsonov , Jury Anatolievich Tjurin
发明人： Alexei Pogosovich Adzhian , Vladimir Jurievich Bogushev , Alexandr Mikhailovich Samsonov , Jury Anatolievich Tjurin
IPC分类号： F02K952
CPC分类号： F02K9/42 , F02K9/52 , F02K9/60 , F23L2900/07004 , F23R3/286 , Y02E20/344
摘要： The invention relates to the field of power machine building and may be used in mixing devices of gas generators for driving gas turbines, in particular, for liquid-propellant rocket engines. A gas generator comprises a cover with a hole, a bottom with a mixing chamber, a housing with an axial duct communicating with the hole in the cover. The housing is fastened in the cover hole and/or in the mixing chamber of the bottom. Grooves are made uniformly along the circumference of the cross section of the housing in the bottom and/or on the housing. The hole in the cover and the axial duct are designed to supply propellant, and the space between the cover and the bottom and the grooves in the bottom and/or on the housing are designed to supply an oxidizer. A propellant space is made in the cover, and the axial duct communicates through the propellant space with the hole in the cover by means of tangential propellant supply holes. An annular oxidizer duct and a cylindrical mixing chamber are additionally made in the module housing. The annular oxidizer duct is placed concentrically to the axial duct and communicates coaxially with the cylindrical mixing chamber, and by tangential oxidizer supply holes communicates with the space between the cover and the bottom.
摘要翻译： 本发明涉及动力机械制造领域，并且可以用于用于驱动燃气轮机的燃气发生器的混合装置，特别是用于液体推进剂火箭发动机。一种气体发生器，包括具有孔的盖，具有混合的底部 室，具有与盖中的孔连通的轴向管道的壳体。 外壳固定在底盖的盖孔和/或混合室中。 槽沿着壳体的底部和/或壳体的横截面的圆周均匀地制成。 盖和轴向管道中的孔被设计成供应推进剂，并且盖和底部之间的空间以及底部和/或壳体上的槽设计成供应氧化剂。 在盖子上形成推进剂空间，并且轴向管道通过切向推进剂供应孔与推进剂空间与盖中的孔连通。 在模块壳体中另外制造环形氧化器管道和圆柱形混合室。 环形氧化器管道同心地放置在轴向管道上并与圆柱形混合室同轴地连通，切向氧化剂供应孔与盖和底部之间的空间连通。
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公开(公告)号：US4488866A
公开(公告)日：1984-12-18
申请号：US404682
申请日：1982-08-03
CPC分类号： F23C6/04 , C10L10/02 , C10L9/02 , F23J7/00 , F23L2900/07004 , Y02E20/344
摘要： A method of minimizing the production of SO.sub.x and NO.sub.x in the burning of a fuel containing significant amounts of SO.sub.x and NO.sub.x precursors in which the fuel is treated to remove significant amounts of SO.sub.x precursors without the removal of significant amounts of NO.sub.x precursors and the fuel is thereafter burned in a two-stage, rich-lean burning step in which significant amounts of the NO.sub.x precursors are converted to N.sub.2. Treating the fuel to remove SO.sub.x precursors is preferrably carried out in the presence of an oxidizing agent, such as H.sub.2 O.sub.2, a reducing agent, such as hydrogen, and/or steam, and still more preferably, the oxidizing agent, the reducing agent and steam are generated by burning an auxiliary fuel and passing the effluent thereof to the step of treating the fuel to remove SO.sub.x precursors.
摘要翻译： 在含有大量SO x和NO x前体的燃料的燃烧中使SO x和NO x的产生最小化的方法，其中处理燃料以除去大量的SO x前体而不除去大量的NO x前体，并且燃料是 然后在两阶段的富稀燃烧步骤中燃烧，其中大量的NOx前体转化为N 2。 处理除去SOx前体的燃料优选在氧化剂如H 2 O 2，还原剂如氢气和/或蒸汽存在下进行，更优选氧化剂，还原剂和蒸汽 通过燃烧辅助燃料并使其流出物进入处理燃料以除去SO x前体的步骤而产生。
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公开(公告)号：US08079845B2
公开(公告)日：2011-12-20
申请号：US11311069
申请日：2005-12-19
申请人： Ken Nowak , Rick Nowak , Chuck Noeding , Mark Pastore
发明人： Ken Nowak , Rick Nowak , Chuck Noeding , Mark Pastore
CPC分类号： F23J7/00 , F23K5/08 , F23L2900/07004 , Y02E20/344
摘要： There is a process for operating a utility boiler. The process has the following steps: a) continuously adding one or more slag control agents, one or more oxygen-generating agents, and a fuel oil to a furnace of the utility boiler; b) providing air to the furnace; c) burning the fuel oil to generate heat and an exhaust gas; d) periodically or continuously varying the dosage rates of the one or more slag control agents and/or the one or more oxygen-generating agents to maintain to substantially maintain one or more emissions variables in the exhaust gas within pre-determined limits. There is also a method for reducing emissions from a utility boiler and a method for reducing slag deposits within a utility boiler.
摘要翻译： 有一个操作锅炉的过程。 该方法具有以下步骤：a）将一个或多个炉渣控制剂，一种或多种氧发生剂和燃料油连续添加到公用锅炉的炉中; b）向炉内提供空气; c）燃烧燃油以产生热量和废气; d）定期或连续地改变一种或多种炉渣控制剂和/或一种或多种氧发生剂的剂量比率，以维持在排气中的一个或多个排放变量在预定限度内。 还有一种减少公用锅炉排放的方法以及一种减少公用事业锅炉内渣堆积的方法。
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公开(公告)号：US20100043444A1
公开(公告)日：2010-02-25
申请号：US12474390
申请日：2009-05-29
申请人： Amichay H. Gross , Savely Khosid , Arie Peretz
发明人： Amichay H. Gross , Savely Khosid , Arie Peretz
CPC分类号： F02C7/264 , F02C7/27 , F05D2220/50 , F23L2900/07004 , F23R3/00 , Y02E20/344
摘要： A method for implementing a system and a device for enhancing the starting process of a turbine engine by use of at least one solid mass of oxidizing-species-releasing material, ORM, selected as a solid oxidizer, or SO, and/or as an oxidizing-species-releasing burning substance, or ORBS. The ORM is introduced into the combustion chamber of the turbine engine and the starting process of the turbine engine is initiated, by help of the igniter and in association with the mass of ORM, to enhance the starting process. In operation, an ORM selected as an SO releases gaseous oxygen when heated to decompose, while an ORM chosen as an ORBS discharges oxidizing species when ignited to burn. An ORM such as an SO or an ORBS may operate alone or in various combinations of both. The ORM is configured to release a predetermined mass flow rate of oxidizing species or of gaseous oxygen.
摘要翻译： 一种用于实施系统和装置的方法，所述系统和装置通过使用选自固体氧化剂或SO的至少一种固体物质，释放氧化物质的物质，或/或作为 氧化物质释放燃烧物质或ORBS。 ORM被引入到涡轮发动机的燃烧室中，并且通过点火器的帮助并且与ORM的质量相关联来启动涡轮发动机的启动过程，以增强启动过程。 在操作中，作为SO选择的ORM在加热分解时释放气态氧，而被选择为ORBS的ORM在点燃时放出氧化物质燃烧。 诸如SO或ORBS的ORM可以单独操作或以两者的各种组合操作。 ORM被配置为释放氧化物质或气态氧的预定质量流率。
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公开(公告)号：US07196240B2
公开(公告)日：2007-03-27
申请号：US10487608
申请日：2003-11-13
CPC分类号： F23L7/00 , A62D3/38 , A62D2101/22 , A62D2203/02 , B01D53/70 , B01D2257/2064 , F23G5/12 , F23G5/16 , F23G7/065 , F23J15/04 , F23J2215/301 , F23L2900/07004 , F23M9/06 , Y02E20/344 , Y10S588/90
摘要： Methods and equipment are provided for making polybichlorophenyl non-toxic. Methods include a first oxidation step, in which polybichlorophenyl is burned, and a second oxidation step, in which exhaust gas from the first oxidation step is oxidized by contact with metallic phthalocyanines or metallic phthalocyanine derivatives and with an oxygen supply compound. Equipment includes a first furnace for burning a polybichlorophenyl-containing oil with an auxiliary fuel and a second oxidation reaction unit. The second oxidation reaction unit connects to the first furnace under seal, and includes metallic phthalocyanine or metallic phthalocyanine derivative solution supply source and an oxygen supply compound supply source.
摘要翻译： 提供了制备聚二氯苯基无毒的方法和设备。 方法包括其中燃烧聚二氯苯基的第一氧化步骤和第二氧化步骤，其中来自第一氧化步骤的废气通过与金属酞菁或金属酞菁衍生物和供氧化合物接触而被氧化。 设备包括用辅助燃料和第二氧化反应单元燃烧含聚二氯苯基的油的第一炉。 第二氧化反应单元在密封下连接到第一炉，并且包括金属酞菁或金属酞菁衍生物溶液供应源和供氧源供应源。
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公开(公告)号：US20060225422A1
公开(公告)日：2006-10-12
申请号：US11424561
申请日：2006-06-16
申请人： James Prentice
发明人： James Prentice
IPC分类号： F01K13/00
CPC分类号： F23G7/003 , F23G5/006 , F23G5/027 , F23G5/16 , F23G7/12 , F23G2202/101 , F23G2202/103 , F23G2206/203 , F23G2209/20 , F23G2209/28 , F23G2900/7011 , F23L7/00 , F23L2900/07004 , F23L2900/07005 , F23M5/08 , F28F21/083 , Y02E20/12 , Y02E20/14 , Y02E20/344
摘要： Apparatus and processes are provided for combusting hydrocarbon-containing waste fuel with an oxidizer, preferably liquid oxygen, and producing a substantially clean exhaust gas and a separate high purity steam product (e.g., superheated steam) that can be used to generate electrical power. The apparatus includes a plurality of combustion chambers in series with means to control the combustion temperature while facilitating complete combustion. The apparatus and method are useful for transforming waste materials, particularly solid and liquid wastes, such as the rubber from scrap tires into non-hazardous materials and energy.
摘要翻译： 提供了用氧化剂，优选液氧来燃烧含烃废物燃料的装置和方法，并且产生基本上清洁的废气和可用于产生电力的单独的高纯度蒸汽产物（例如过热蒸汽）。 该装置包括与控制燃烧温度同时有助于完全燃烧的装置串联的多个燃烧室。 该设备和方法可用于将废料特别是固体和液体废物（例如废旧轮胎的橡胶）转化成非危险材料和能量。
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9.发明授权Enhanced starting of turbine engines under various ambient conditions using oxidizer 有权涡轮发动机在各种环境条件下使用氧化剂增强起动公开(公告)号：US08402767B2
公开(公告)日：2013-03-26
申请号：US12474390
申请日：2009-05-29
申请人： Amichay H. Gross , Savely Khosid , Arie Peretz
发明人： Amichay H. Gross , Savely Khosid , Arie Peretz
CPC分类号： F02C7/264 , F02C7/27 , F05D2220/50 , F23L2900/07004 , F23R3/00 , Y02E20/344
摘要： At least one solid mass of oxidizing-species-releasing material (ORM), selected as a solid oxidizer (SO), and/or as oxidizing-species-releasing burning substance (ORBS) is used as a device for enhancing the starting process of a turbine engine under various ambient conditions. The ORM is introduced into the combustion chamber of the turbine engine and the starting process of the turbine engine is initiated, by help of the igniter and in association with the ORM to enhance the starting process. In operation, an ORM selected as an SO releases gaseous oxygen when heated to decompose, while an ORM chosen as an ORBS discharges oxidizing species when ignited to burn. An ORM such as an SO or an ORBS may operate alone or in various combinations of both. The ORM is configured to release a predetermined mass flow rate of oxidizing species or of gaseous oxygen.
摘要翻译： 使用选自固体氧化剂（SO）和/或氧化物质释放燃烧物质（ORBS）的至少一种固体物质的氧化物质释放物质（ORM）作为增强起始过程的装置 涡轮发动机在各种环境条件下。 ORM被引入到涡轮发动机的燃烧室中，并且通过点火器的帮助并且与ORM相关联地启动涡轮发动机的起动过程以增强启动过程。 在操作中，作为SO选择的ORM在加热分解时释放气态氧，而被选择为ORBS的ORM在点燃时放出氧化物质燃烧。 诸如SO或ORBS的ORM可以单独操作或以两者的各种组合操作。 ORM被配置为释放氧化物质或气态氧的预定质量流率。
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公开(公告)号：US07503511B2
公开(公告)日：2009-03-17
申请号：US11198053
申请日：2005-08-04
申请人： Thomas J. Mueller
发明人： Thomas J. Mueller
CPC分类号： F02K9/52 , F23L7/007 , F23L2900/07004 , Y02E20/344
摘要： A bi-propellant rocket engine may include a primary propellant flowing in a central passageway, a secondary propellant flowing in a secondary passageway generally coaxial with central passageway and a pintle tip having a central chamber sidewall coaxial with the primary passageway and surrounding a central chamber, the central chamber sidewall having a first plurality of apertures there through so that some of the primary propellant exits the central chamber transverse to the flow of the secondary propellant in the secondary passageway. The pintle tip may have a secondary chamber sidewall, substantially thicker than the primary chamber sidewall, surrounding a secondary chamber downstream of and in fluid communication with the primary chamber, the secondary chamber sidewall having a second plurality of apertures there through so that some of the primary propellant exits the secondary chamber transverse to the flow of the secondary propellant in the secondary passageway. The pintle tip may have an end wall generally traverse to the flow of the primary propellant in the central passageway and adjacent the secondary chamber sidewall so that the flow of primary propellant through the secondary chamber sidewall cools a downstream face of the end wall during combustion of the mixed propellants adjacent the downstream face of the end wall. The pintle tip may be used for mixing a first liquid with a second liquid.
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