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1. 发明授权

US07685803B2 Gas turbine system for injecting a mixture of high value hydrocarbons plural distinct fuels into the gas turbine combustion chamber 有权
标题翻译：燃气轮机系统，用于将高价值烃混合物多种不同的燃料喷入燃气轮机燃烧室
公开(公告)号：US07685803B2
公开(公告)日：2010-03-30
申请号：US12110497
申请日：2008-04-28
申请人： Dieter Rebhan , Marcel Stalder
发明人： Dieter Rebhan , Marcel Stalder
IPC分类号： F02C3/20
CPC分类号： F02C3/22 , F02C7/22 , F02C9/40 , F05B2270/337 , F05D2270/082 , F23K5/002 , F23N2037/08 , F23N2041/20 , F23R3/36
摘要： A gas turbine uses a first fuel at full load and an improved emission behavior is achieved by operating the gas turbine (11) at partial load with a second fuel, which has a richer mix of higher-value hydrocarbons (C2+) with 2 and more carbon atoms per molecule like ethane (C2H6) and propane (C3H8).
摘要翻译：燃气轮机使用全负荷时的第一燃料，并且通过用第二燃料以部分负荷操作燃气轮机（11）来实现改进的排放特性，第二燃料具有较高价值的烃类（C2 +）与2及更多的混合物每分子碳原子如乙烷（C 2 H 6）和丙烷（C 3 H 8）。

2. 发明申请

US20050126178A1 Method for operating a gas turbine and gas turbine system for carrying out the method 有权
标题翻译：用于操作燃气轮机和燃气轮机系统以执行该方法的方法
公开(公告)号：US20050126178A1
公开(公告)日：2005-06-16
申请号：US10950648
申请日：2004-09-28
申请人： Dieter Rebhan , Marcel Stalder
发明人： Dieter Rebhan , Marcel Stalder
IPC分类号： F02C3/20 , F02C9/40 , F23K5/00 , F23R3/36
CPC分类号： F02C3/22 , F02C7/22 , F02C9/40 , F05B2270/337 , F05D2270/082 , F23K5/002 , F23N2037/08 , F23N2041/20 , F23R3/36
摘要： A method for operating a gas turbine uses a first fuel at full load. An improved emission behavior is achieved by operating the gas turbine (11) at partial load with a second fuel, which has a richer mix of higher-value hydrocarbons (C2+) with 2 and more carbon atoms per molecule like ethane (C2H6) and propane (C3H8).
摘要翻译：用于操作燃气轮机的方法使用满负荷的第一燃料。通过用第二燃料以部分负荷操作燃气轮机（11）来实现改进的排放特性，该第二燃料具有比乙烷更高的碳氢化合物（C2 +）与更高碳原子的更丰富的混合物（C + 2 H 6 H 6）和丙烷（C 3 H 8）。

3. 发明授权

US06694745B2 Method for running up a gas turbine plant 有权
标题翻译：运行燃气轮机厂的方法
公开(公告)号：US06694745B2
公开(公告)日：2004-02-24
申请号：US10145703
申请日：2002-05-16
申请人： Marcel Stalder , Dieter Rebhan , Thomas Kueenzi , Hans Peter Knoepfel
发明人： Marcel Stalder , Dieter Rebhan , Thomas Kueenzi , Hans Peter Knoepfel
IPC分类号： F02C722
CPC分类号： F02C7/26 , F02C9/28
摘要： A method for running up a gas turbine plant (1) is disclosed. In the method, a fuel (6) is injected into the combustion chamber (5) via a plurality of pilot burners (10) and premix burners (11). During the start-up and in a lower load range, the combustion chamber (5) is operated in the pilot mode, and, at a specific time point, the combustion chamber (5) is changed over from the pilot mode to the premix mode. The changeover time point from the pilot mode to the premix mode depends on a variable changeover temperature (TSWO), and this changeover temperature (TSWO) is determined from pulsations occurring in the flame of the combustion chamber (5).
摘要翻译：公开了一种用于运行燃气轮机设备（1）的方法。在该方法中，经由多个先导燃烧器（10）和预混燃烧器（11）将燃料（6）注入燃烧室（5）。在启动期间和在较低的负载范围内，燃烧室（5）在先导模式下操作，并且在特定时间点，燃烧室（5）从先导模式切换到预混模式。从先导模式到预混模式的切换时间点取决于可变转换温度（TSWO），并且该转换温度（TSWO）由在燃烧室（5）的火焰中发生的脉动确定。

4. 发明授权

US06688111B2 Method for operating a combustion chamber 有权
标题翻译：操作燃烧室的方法
公开(公告)号：US06688111B2
公开(公告)日：2004-02-10
申请号：US09987117
申请日：2001-11-13
申请人： Marcel Stalder , Daniel Burri , Urs Benz
发明人： Marcel Stalder , Daniel Burri , Urs Benz
IPC分类号： F02C314
CPC分类号： F23D14/64 , F23D11/402 , F23R3/286
摘要： A combustion chamber includes a mixing zone and a combustion zone within which self-ignition of a fuel and air mixture can occur. Fuel and support air are injected laterally at the sidewall of the mixing zone into hot gases passing through the mixing zone. The operating range of the combustion chamber can be increased while noxious substances are reduced by injecting differently controlled fuel/support air mixture jets into different target spaces within the mixing zone.
摘要翻译：燃烧室包括混合区和燃烧区，在该燃烧区内可能发生燃料和空气混合物的自燃。燃料和支撑空气在混合区的侧壁侧向注入穿过混合区的热气体。可以通过将不同控制的燃料/支持空气混合物射流注入混合区内的不同目标空间来增加燃烧室的操作范围，同时减少有害物质。

5. 发明授权

US06370879B1 Damping device for reducing the vibration amplitude of acoustic waves for a burner 失效
标题翻译：用于减少燃烧器声波振动振幅的阻尼装置
公开(公告)号：US06370879B1
公开(公告)日：2002-04-16
申请号：US09431918
申请日：1999-11-02
申请人： Marcel Stalder , Franz Joos
发明人： Marcel Stalder , Franz Joos
IPC分类号： F02C724
CPC分类号： F23D14/46 , F05B2260/96 , F23C2900/07002 , F23D2210/00 , F23R3/286 , F23R2900/00014
摘要： A damping device for reducing the vibration amplitude of acoustic waves and a burner for operating an internal combustion engine, the burner having a mixing region, in which an air flow and a fuel flow are mixed with one another to form an air/fuel mixture, and a combustion chamber, which in the direction of flow of the fuel/air mixture is arranged downstream of the mixing region, in which the fuel/air mixture can be ignited. A Helmholtz resonator directly connected to the mixing region of the burner such that acoustic waves formed in the burner are suppressed in the Helmholtz resonator and are not reflected back into the burner.
摘要翻译：一种用于减小声波振动振幅的阻尼装置和用于操作内燃机的燃烧器，所述燃烧器具有混合区域，其中空气流和燃料流彼此混合以形成空气/燃料混合物，并且在燃料/空气混合物的流动方向上的燃烧室布置在燃料/空气混合物可以被点燃的混合区域的下游。亥姆霍兹共振器直接连接到燃烧器的混合区域，使得在亥姆霍兹共振器中形成的声波被抑制，并且不被反射回燃烧器。

6. 发明授权

US06322353B1 Ignition appliance for a heat generator 有权
标题翻译：点火装置用于发热体
公开(公告)号：US06322353B1
公开(公告)日：2001-11-27
申请号：US09397511
申请日：1999-09-17
申请人： Marcel Stalder , Günter Sybon
发明人： Marcel Stalder , Günter Sybon
IPC分类号： F02C7264
CPC分类号： F02C7/264
摘要： In an ignition appliance for a heat generator, the supply lines for air (70) and fuel gas (60) are led directly into a flame tube (40). The igniter (51) is arranged in an ignition space (50) remote from the flame tube (40) and connected to the flame tube (40). The ignition space (50) is connected to the air supply passage (70) and the gas supply passage (60) via connecting ducts (55, 56). If the supply passages for air and fuel gas (70, 60) are dimensioned so as to be sufficiently large, the pressure drop between the inside of the ignition space (50) and the feed lines (60, 70) is small. The fuel/air ratio present at the igniter (51) is therefore essentially determined only by the ratio of the cross sections of the connecting ducts (55, 56). The flow relationships in the ignition space (50) are likewise substantially decoupled from the air and fuel gas flows supplied overall to the ignition appliance. In consequence, good conditions for a reliable ignition can be set over a wide operating range of the ignition appliance.
摘要翻译：在用于发热体的点火装置中，将空气供给线（70）和燃料气体（60）直接引导到火焰管（40）中。点火器51配置在远离火焰管40并与火焰管40连接的点火空间50内。点火空间（50）通过连接管（55,56）连接到供气通道（70）和气体供应通道（60）。如果用于空气和燃料气体（70,60）的供应通道的尺寸足够大，则点火空间（50）的内部和进料管线（60,70）之间的压降很小。因此，在点火器（51）处存在的燃料/空气比基本上仅由连接管道（55,56）的横截面的比率决定。点火空间（50）中的流动关系同样基本上与整体提供给点火器具的空气和燃料气体流分离。因此，可以在点火器具的宽的工作范围内设置可靠点火的良好条件。

7. 发明授权

US07096670B2 Method for igniting the combustion chamber of a gas turbine unit and an ignition device for carrying out the method 失效
标题翻译：点燃燃气轮机单元的燃烧室的方法和用于实施该方法的点火装置
公开(公告)号：US07096670B2
公开(公告)日：2006-08-29
申请号：US10936486
申请日：2004-09-09
申请人： Franz Joos , Marcel Stalder
发明人： Franz Joos , Marcel Stalder
IPC分类号： F02C7/264 , F02C7/22
CPC分类号： F02C7/264
摘要： In a method for igniting the combustion chamber of a gas turbine unit, a safely working ignition and a long lifetime of the ignition device (10) is achieved by discharging a compressed gas with a supercritical pressure ratio through a nozzle (21) and heating it up to a temperature sufficient to ignite hydrocarbons by interacting with a resonance tube (19) arranged behind said nozzle (21), and using said heated-up gas to directly or indirectly ignite a fuel/air mixture introduced into said combustion chamber.
摘要翻译：在用于点燃燃气轮机单元的燃烧室的方法中，点火装置（10）的安全工作点火和长寿命通过喷嘴（21）以超临界压力比排出并加热它来实现直到足以通过与布置在所述喷嘴（21）后面的共振管（19）相互作用来点燃碳氢化合物的温度，并且使用所述加热气体直接或间接地点燃引入所述燃烧室的燃料/空气混合物。

8. 发明授权

US6128894A Method of operating a burner 失效
标题翻译：操作燃烧器的方法
公开(公告)号：US6128894A
公开(公告)日：2000-10-10
申请号：US984424
申请日：1997-12-03
申请人： Franz Joos , Marcel Stalder
发明人： Franz Joos , Marcel Stalder
IPC分类号： F23D11/38 , F23C99/00 , F23D11/10 , F23D11/22 , F23K5/10 , F23R3/28
CPC分类号： F23D11/22 , F23D11/102 , F23D2206/10
摘要： The invention is directed to a method of operating a burner. The method includes feeding an auxiliary gas into a liquid fuel upstream of an injection orifice during the ignition and during part load of the burner, and interrupting the feeding of the auxiliary gases within high load ranges of the burner.
摘要翻译：本发明涉及一种操作燃烧器的方法。该方法包括在点燃期间和在燃烧器的部分负荷期间将辅助气体供给到喷射孔上游的液体燃料中，并且在燃烧器的高负载范围内中断辅助气体的供给。

9. 发明授权

US5782626A Airblast atomizer nozzle 失效
标题翻译：喷粉喷嘴
公开(公告)号：US5782626A
公开(公告)日：1998-07-21
申请号：US696665
申请日：1996-08-14
申请人： Franz Joos , Marcel Stalder
发明人： Franz Joos , Marcel Stalder
IPC分类号： F23D11/40 , F23D11/00 , F23D11/10 , F23D7/00
CPC分类号： F23D11/007 , F23D11/107 , F23C2900/07002 , F23D2211/00 , F23D2900/11101
摘要： In an airblast atomizer nozzle (2) for the operation of a burner (1) operated with liquid and gaseous fuels (4, 6) the intermediate wall (18) between the inner (14) and outer (13) air duct is held via inner and outer support elements (21) which have a sliding fit (28) and which can be designed as swirl vanes. The atomizer edges (19) of the airblast nozzle (2) are angled in the direction of the nozzle axis (11). The nozzle is distinguished by small dimensions, a low pressure loss and a negligible tendency to coking.
摘要翻译：在用于用液体和气体燃料（4,6）操作的燃烧器（1）的操作的喷气喷雾器喷嘴（2）中，内部（14）和外部（13）空气管道之间的中间壁（18）保持通过内部和外部支撑元件（21），其具有滑动配合（28）并且可被设计为旋转叶片。喷气嘴（2）的雾化器边缘（19）在喷嘴轴线（11）的方向上成角度。喷嘴的特点是尺寸小，压力损失低，焦化倾向可忽略不计。

10. 发明授权

US07380402B2 Method for operating a gas turbine and gas turbine system for carrying out the method 有权
标题翻译：用于操作燃气轮机和燃气轮机系统以执行该方法的方法
公开(公告)号：US07380402B2
公开(公告)日：2008-06-03
申请号：US10950648
申请日：2004-09-28
申请人： Dieter Rebhan , Marcel Stalder
发明人： Dieter Rebhan , Marcel Stalder
IPC分类号： F02C7/22 , F02C7/26
CPC分类号： F02C3/22 , F02C7/22 , F02C9/40 , F05B2270/337 , F05D2270/082 , F23K5/002 , F23N2037/08 , F23N2041/20 , F23R3/36
摘要： A method for operating a gas turbine uses a first fuel at full load. An improved emission behavior is achieved by operating the gas turbine (11) at partial load with a second fuel, which has a richer mix of higher-value hydrocarbons (C2+) with 2 and more carbon atoms per molecule like ethane (C2H6) and propane (C3H8).
摘要翻译：用于操作燃气轮机的方法使用满负荷的第一燃料。通过用第二燃料以部分负荷操作燃气轮机（11）来实现改进的排放特性，该第二燃料具有比乙烷更高的碳氢化合物（C2 +）与更高碳原子的更丰富的混合物（C + 2 H 6 H 6）和丙烷（C 3 H 8）。

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