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1. 发明授权

US06883730B2 Atomizing nozzle for a burner 失效
标题翻译：用于燃烧器的雾化喷嘴
公开(公告)号：US06883730B2
公开(公告)日：2005-04-26
申请号：US10361301
申请日：2003-02-10
申请人： Günter Eberspach , Walter Blaschke , Michael Humburg , Franz Joos
发明人： Günter Eberspach , Walter Blaschke , Michael Humburg , Franz Joos
IPC分类号： F23D11/24 , B60H1/03 , B60H1/22 , F23D11/10 , F23D11/38 , B05B7/10
CPC分类号： F23D11/107 , F23D2900/11101
摘要： An atomizing nozzle for a burner, especially for a vehicle heater has a flow guide element (16), which provides a flow guide surface (28) and which has an atomizing lip (36) in an end area (34). A fuel feed device (52, 50) is provided for feeding fuel to the flow guide surface (28) at a spaced location from the atomizing lip (36). Provisions are made for the fuel feed device (52, 50) in the flow guide element (16) to comprise a fuel release depression (50), into which opens a fuel feed channel device (52) in a junction area.
摘要翻译：一种用于燃烧器，特别是用于车辆加热器的雾化喷嘴具有一个流动引导元件（16），该引导元件（16）提供一个流动引导表面（28），并且在端部区域（34）中具有雾化唇缘（36）。燃料供给装置（52,50）用于在与雾化唇缘（36）间隔开的位置处将燃料供给到导流表面（28）。对于导流元件（16）中的燃料供给装置（52,50）进行配置以包括在接合区域中打开燃料供给通道装置（52）的燃料释放凹部（50）。

2. 发明授权

US06729142B2 Thermal turbomachine and process for igniting the thermal turbomachine 失效
标题翻译：热涡轮机和点燃热涡轮机的过程
公开(公告)号：US06729142B2
公开(公告)日：2004-05-04
申请号：US10067284
申请日：2002-02-07
申请人： Marcel Stalder , Franz Joos
发明人： Marcel Stalder , Franz Joos
IPC分类号： F02C7264
CPC分类号： F02C7/264 , F23D2900/00014 , F23R3/343
摘要： In a thermal turbomachine with a housing, a combustion chamber, an ignition device, a fuel supply, and an air supply, the ignition device includes an ignition space and an igniter arranged in the ignition space. The fuel supply and the air supply open into the ignition space. The ignition space is connected to the combustion chamber, and the ignition device is arranged outside the housing of the thermal turbomachine. A process is shown for the ignition of the thermal turbomachine outside the housing.
摘要翻译：在具有壳体，燃烧室，点火装置，燃料供应和空气供应的热涡轮机中，点火装置包括点火空间和布置在点火空间中的点火器。燃料供应和供气通向点火空间。点火空间连接到燃烧室，并且点火装置设置在热涡轮机壳体外部。示出了用于在壳体外部点燃热涡轮机的过程。

3. 发明授权

US06402059B1 Fuel lance for spraying liquid and/or gaseous fuels into a combustion chamber, and method of operating such a fuel lance 有权
标题翻译：用于将液体和/或气体燃料喷射到燃烧室中的燃料喷枪，以及操作这种燃料喷枪的方法
公开(公告)号：US06402059B1
公开(公告)日：2002-06-11
申请号：US09503711
申请日：2000-02-14
申请人： Urs Benz , Franz Joos
发明人： Urs Benz , Franz Joos
IPC分类号： F23D1422
CPC分类号： F23D14/22 , F23D11/101 , F23D14/78 , F23D17/002
摘要： In a fuel lance for spraying liquid and/or gaseous fuels into a combustion chamber, which fuel lance is part of a secondary or tertiary burner, around which a hot-gas jet flows in a main flow direction, and comprises a liquid-fuel passage for supplying liquid fuel and first means for spraying the liquid fuel from the liquid-fuel passage into the combustion chamber, operation characterized by reduced addition of water is made possible owing to the fact that the first means comprise a liquid-fuel nozzle, which sprays the liquid fuel essentially parallel to the main flow direction as a plain jet into the combustion chamber.
摘要翻译：在用于将液体和/或气体燃料喷射到燃烧室中的燃料喷枪中，该燃料喷枪是二次或三次燃烧器的一部分，热气流在主流动方向上流动，并且包括液体 - 燃料通道用于供应液体燃料的液体燃料和用于将液体燃料从液体燃料通道喷射到燃烧室中的第一装置，其特征在于减少水分的操作是可能的，这是由于第一装置包括液体燃料喷嘴液体燃料基本上平行于主流动方向，作为平均喷射入燃烧室。

4. 发明授权

US5729967A Method of operating a gas turbine on reformed fuel 失效
标题翻译：在重整燃料上操作燃气轮机的方法
公开(公告)号：US5729967A
公开(公告)日：1998-03-24
申请号：US698592
申请日：1996-08-16
申请人： Franz Joos , Timothy Griffin , Hans Koch
发明人： Franz Joos , Timothy Griffin , Hans Koch
IPC分类号： F01N3/08 , F01N3/24 , F02C3/20 , F02C3/28 , F02C7/26 , F02C9/34 , F23C6/04 , F23C13/00 , F23R3/40
CPC分类号： F23C13/00 , F02C3/28 , F23C6/047 , F23R3/40
摘要： In a method for the operation of a power station installation which essentially comprises a compressor (4), a combustion unit and a turbine (12), the combustion unit comprising a conditioning stage for at least part of the combustion air and a combustion chamber, a portion (13a) of the compressed air (13) from the compressor (4) is passed through the conditioning stage and there first of all mixed with a quantity of fuel (14a). This mixture then passes into a generator (8), in which at least hydrogen is fractionated, this hydrogen then being used in the combustion chamber. The combustion chamber comprises a start-up burner (1), a catalytic stage (2) and a downstream second combustion stage (3). Both the air/fuel mixture (16a) fractionated in the generator (8) and the further compressor air (13) enter the combustion chamber, in which interdependent combustion occurs between the combustion units acting there, relative to the running up of the installation, for the purpose of minimizing pollutant emissions. (FIG. 1)
摘要翻译：在基本上包括压缩机（4），燃烧单元和涡轮机（12）的电站设备操作的方法中，所述燃烧单元包括用于至少部分燃烧空气和燃烧室的调节级，来自压缩机（4）的压缩空气（13）的部分（13a）通过调节阶段，首先与一定量的燃料（14a）混合。然后将该混合物送入发生器（8），其中至少将氢气分馏，然后将该氢气用于燃烧室。燃烧室包括启动燃烧器（1），催化级（2）和下游第二燃烧级（3）。在发电机（8）中分离出的空气/燃料混合物（16a）和另外的压缩机空气（13）进入燃烧室，在燃烧室中，相对于设备的运行在其间作用的燃烧单元之间发生相互依赖的燃烧，以减少污染物排放。（图。1）

5. 发明授权

US5664943A Method and device for operating a combined burner for liquid and gaseous fuels 失效
标题翻译：用于操作液体和气体燃料的组合燃烧器的方法和装置
公开(公告)号：US5664943A
公开(公告)日：1997-09-09
申请号：US450696
申请日：1995-05-25
申请人： Franz Joos , Tino-Martin Marling , Peter Senior
发明人： Franz Joos , Tino-Martin Marling , Peter Senior
IPC分类号： F23D11/40 , F23C7/00 , F23D11/22 , F23D17/00 , F23C5/00
CPC分类号： F23C7/002 , F23D11/22 , F23D17/002 , F23C2900/07002
摘要： A method and device for operating a combined burner for liquid and gaseous fuels for the purpose of generating hot gases functions to raise the lean stability limit of the gas flame without impairing the atomization of the liquid fuel and improve the regulating range of the burner. According to the invention, this is achieved when the inflow rate and/or swirl of the blast air (5) into the inner burner space (16) is controlled. To this end, the blast air (5), during operation with gaseous fuel (6), is throttled back by injection of pilot fuel into the blast air, and additionally swirled by swirl generators in the burner. In addition, active regulation of the blast air inflow rate is effected at the burner inlet during the use of both gaseous fuel and liquid fuel.
摘要翻译：一种用于操作用于液体和气体燃料的组合燃烧器的方法和装置，用于产生热气体的功能，以提高气体火焰的稀薄稳定性极限，而不损害液体燃料的雾化并改善燃烧器的调节范围。根据本发明，当控制喷气（5）进入内部燃烧器空间（16）的流入速率和/或涡流时，实现这一点。为此，在气体燃料（6）运行期间的鼓风空气（5）通过将引燃燃料喷射到鼓风空气中被再次节流，并且还被燃烧器中的涡流发生器旋转。此外，在使用气体燃料和液体燃料期间，在燃烧器入口处进行鼓风空气流入速率的主动调节。

6. 发明授权

US4842197A Fuel injection apparatus and associated method 失效
标题翻译：燃油喷射装置及相关方法
公开(公告)号：US4842197A
公开(公告)日：1989-06-27
申请号：US131206
申请日：1987-12-10
申请人： Burkhard Simon , Franz Joos
发明人： Burkhard Simon , Franz Joos
IPC分类号： F23C7/00 , F23C9/00 , F23D11/10 , F23R3/14
CPC分类号： F23C9/006 , F23C7/002 , F23D11/107 , F23R3/14 , F23D2900/11101
摘要： A fuel injection device having three concentric streams of air for the atomization of fuel sprayed onto a sleeve by an injector facing into the sleeve. The inner and outer streams of air are imparted with swirl in opposite direction, while the central stream of air is free of swirl. The two inner streams of air atomize the fuel as a result of shear forces, while the outer stream of air forms a stable recirculation region in a combustion chamber into which the fuel injector device extends.
摘要翻译：一种燃料喷射装置，具有三个同心的空气流，用于通过面向套筒的喷射器喷射到套筒上的燃料雾化。内部和外部空气流在相反方向上被赋予漩涡，而中央空气流没有涡流。两个内部空气流由于剪切力而使燃料雾化，而外部空气流在燃烧室中形成稳定的再循环区域，燃料喷射器装置延伸到燃烧室中。

7. 发明授权

US06581385B2 Combustion device for generating hot gases 有权
公开(公告)号：US06581385B2
公开(公告)日：2003-06-24
申请号：US10237076
申请日：2002-09-09
申请人： Franz Joos , Wolfgang Polifke , Alexander Ni
发明人： Franz Joos , Wolfgang Polifke , Alexander Ni
IPC分类号： F23R300
CPC分类号： F23R3/286 , F23C2900/07002 , F23D2210/00 , F23R2900/00014 , F23R2900/00016
摘要： In a combustion device (10), particularly for driving gas turbines, comprising a plurality of burners (12, . . . , 15) of identical thermal power output, which work parallel to an axis (28) into a common combustion chamber (11), an effective suppression of thermoacoustic combustion instabilities is achieved in a simple way in that the burners (12, . . . , 15) are designed differently from one another in such a way that the flames (24, . . . , 27) or flame fronts generated by them are positioned so as to be distributed along the axis (28).

8. 发明授权

US06325618B1 Fuel lance for spraying liquid and/or gaseous fuels into a combustion chamber 有权
标题翻译：用于将液体和/或气体燃料喷射到燃烧室中的燃料喷枪
公开(公告)号：US06325618B1
公开(公告)日：2001-12-04
申请号：US09503709
申请日：2000-02-14
申请人： Urs Benz , Franz Joos , Adnan Eroglu
发明人： Urs Benz , Franz Joos , Adnan Eroglu
IPC分类号： F23D1700
CPC分类号： F23D17/002 , F23D11/101 , F23D14/22 , F23D2214/00
摘要： A fuel lance for spraying liquid and/or gaseous fuels into a combustion chamber, which fuel lance is provided with first means for the radial spraying of the liquid fuel from the liquid-fuel passage into the combustion chamber. The first means comprise a first guide tube, which, in the radial direction starting from the liquid-fuel passage, runs outward through a gas passage and an air passage. In addition, second means are provided, which comprise a second guide tube, which, in the radial direction starting from the gas passage, runs outward through the air passage and concentrically surrounds the first guide tube at a distance. Both guide tubes open in the region of a shell opening in the lance shell in such a way that the liquid-fuel jet discharging from the first guide tube discharges as a plain jet into the combustion chamber, and the fuel jets discharging from the guide tubes are surrounded in a sheath-like manner by the air flowing out of the air passage through the shell opening.
摘要翻译：用于将液体和/或气体燃料喷射到燃烧室中的燃料喷枪，该燃料喷枪设置有用于将液体燃料从液体燃料通道径向喷射到燃烧室中的第一装置。第一装置包括第一引导管，其沿着从液体燃料通道开始的径向方向通过气体通道和空气通道向外延伸。此外，提供了第二装置，其包括第二引导管，该第二引导管在从气体通道开始的径向方向上穿过空气通道向外延伸并且一直距离围绕第一引导管。两个引导管在喷枪壳体中的壳体开口的区域中打开，使得从第一引导管排出的液体燃料喷射作为普通喷射器排放到燃烧室中，并且燃料喷射从引导管排出通过从壳体开口流出空气通道的空气以鞘状的方式包围。

9. 发明授权

US5593302A Combustion chamber having self-ignition 失效
标题翻译：燃烧室具有自燃
公开(公告)号：US5593302A
公开(公告)日：1997-01-14
申请号：US414725
申请日：1995-03-31
申请人： Rolf Althaus , Yau-Pin Chyou , Franz Joos , Jakob J. Keller
发明人： Rolf Althaus , Yau-Pin Chyou , Franz Joos , Jakob J. Keller
IPC分类号： F23D17/00 , F23C7/02 , F23M9/00 , F23M9/02 , F23D14/02
CPC分类号： F23M9/02 , F23M9/00 , F05B2240/122 , F23R2900/03341
摘要： In a combustion chamber consisting essentially of an inflow zone (5) and a combustion zone (11) and having self-ignition, the inflow zone (5) has vortex generators (100), of which a plurality are arranged next to one another over the periphery of the duct through which flow occurs. A premixing zone (7) follows downstream of the inflow zone (5), into which premixing zone (7) a gaseous and/or liquid fuel (9) is injected as secondary flow into a gaseous main flow (4). Between premixing zone (5) and the downstream combustion zone (11), the transition is characterized by a jump (12) in cross-section which induces the initial cross-section of flow of the combustion zone (11). The fuel (9) is injected via a number of fuel lances (8) distributed over the periphery, the fuel (9) being enriched here with a portion of assisting air
摘要翻译：在基本上由流入区（5）和燃烧区（11）组成并具有自点火的燃烧室中，流入区（5）具有涡流发生器（100），其中多个彼此相邻设置在上管道的外围发生流动。在流入区域（5）的下游的预混合区域（7）之后，预混合区域（7）将气体和/或液体燃料（9）作为次流注入气态主流体（4）。在预混合区（5）和下游燃烧区（11）之间，该过渡的特征在于横截面的跳跃（12），其引起燃烧区（11）的初始流动横截面。燃料（9）通过分布在周边的多个燃料喷枪（8）喷射，这里富含燃料（9）的一部分辅助空气

10. 发明授权

US5357743A Burner for gas turbine engines 失效
标题翻译：燃气涡轮发动机燃烧器
公开(公告)号：US5357743A
公开(公告)日：1994-10-25
申请号：US111481
申请日：1993-08-25
申请人： Nikolaos Zarzalis , Franz Joos
发明人： Nikolaos Zarzalis , Franz Joos
IPC分类号： F23C7/00 , F23R3/14 , F23R3/26 , F02C9/20
CPC分类号： F23R3/26 , F23C7/006 , F23R3/14 , F05B2250/41
摘要： A burner for gas turbine engines is provided in which a ring-shaped swirling device is coaxially assigned to a fuel nozzle. The swirling device forms tangential ducts for an adjustable feeding of combustion air between profiled surfaces arranged along the circumference. Two components, which are axially adjustable relative to one another, are to form, on mutually opposite faces, the ducts between profiles and recesses which are arranged offset relative to one another along the circumference, in such a manner that, when at least one component is adjusted, the profiles can be moved into the recesses for a reduction of the duct cross-sections or can be moved out of the recesses for an enlargement of the duct cross-sections.
摘要翻译：提供了一种用于燃气涡轮发动机的燃烧器，其中环形旋流装置同轴地分配给燃料喷嘴。旋转装置形成切向管道，用于在沿圆周布置的成形表面之间可调节地供给燃烧空气。相对于彼此可轴向调节的两个部件将在相互相对的面上形成轮廓和凹部之间的管道，其沿着圆周相对于彼此偏移地设置，使得当至少一个部件可以将轮廓移动到凹部中以减少管道横截面，或者可以移出凹部以扩大管道横截面。

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