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1. 发明授权

US4890793A Atomizer nozzle 失效
标题翻译：雾化喷嘴
公开(公告)号：US4890793A
公开(公告)日：1990-01-02
申请号：US151612
申请日：1988-02-02
申请人： Cornel Fuglistaller , Jakob Keller , Thomas Sattelmayer
发明人： Cornel Fuglistaller , Jakob Keller , Thomas Sattelmayer
IPC分类号： B05B7/04 , B05B7/08 , F23D11/10
CPC分类号： B05B7/0892 , B05B7/0458 , B05B7/0475 , B05B7/0491 , B05B7/08 , F23D11/102
摘要： The atomizer nozzle exhibits an internal chamber (1) and an external chamber (2) which surrounds the latter in the form of a jacket, which chambers are provided with several outlet openings (9, 10 and 11, 12) which are in alignment in each case. A proportion of the atomizer air supplied via an air duct (5) flows into the internal chamber (1) and is essentially used there for uniformly distributing a liquid fuel, which is also flowing into the internal chamber (1) from a fuel duct (3), to its outlet openings (9, 10). The remaining greater proportion of the atomizer air flows around the internal chamber (1) through the external chamber (2) and is concentrically mixed in with the coarsely atomized fuel emerging from the outlet openings (9, 10) of the internal chamber (1). This prevents liquid fuel fragments from coming into contact with the walls of the outlet openings (11, 12) of the external chamber (2), and a high atomization quality is achieved.
摘要翻译：雾化器喷嘴具有内部腔室（1）和外部腔室（2），外部腔室（2）以外壳的形式围绕腔室（2），该腔室设置有若干出口开口（9,10和11,12）每个案例。通过空气管道（5）供应的雾化器空气的一部分流入内部室（1），并且基本上在那里用于均匀分配液体燃料，其也从燃料管道流入内部室（1） 3）到其出口（9,10）。剩余的较大比例的雾化器空气通过外部室（2）流过内部室（1），并与从内部室（1）的出口（9,10）排出的粗糙雾化燃料同心地混合，。这防止液体燃料碎片与外部室（2）的出口（11,12）的壁接触，并且实现高雾化质量。

2. 发明授权

US4850194A Burner system 失效
标题翻译：燃烧器系统
公开(公告)号：US4850194A
公开(公告)日：1989-07-25
申请号：US129172
申请日：1987-12-07
申请人： Cornel Fuglistaller , Jakob Keller , Thomas Sattelmayer
发明人： Cornel Fuglistaller , Jakob Keller , Thomas Sattelmayer
IPC分类号： F23R3/12 , F02C7/232 , F23D11/00 , F23D14/02 , F23D14/26 , F23R3/28
CPC分类号： F23D14/26 , F23D11/00 , F23D14/02 , Y02E20/344
摘要： The present invention relates to a burner system, in particular for a gas turbine, with a main supply channel (2), debouching into a combustion chamber (1), for a fuel/air mixture having a swirler (5) and a burner lance (3) which passes through the swirler (5). To improve the transverse ignition properties between several such burner systems, optionally disposed on the burner chamber (1), and also to increase the flame stability, the burner lance (3) has, on the combustion chamber side with respect to the swirler (5) exit openings (12, 16) for fuel supplied to its interior or for a fuel-rich fuel/air mixture supplied to, or formed in, its interior.
摘要翻译：本发明涉及一种燃烧器系统，特别是燃气轮机，具有主供应通道（2），用于具有旋流器（5）和燃烧器喷枪（5）的燃料/空气混合物（3），其通过旋流器（5）。为了改善多个这样的燃烧器系统之间的横向点火性能，任选地设置在燃烧器室（1）上，并且还增加火焰稳定性，燃烧器喷枪（3）在相对于旋流器（5）的燃烧室侧）出口开口（12,16），用于供应到其内部的燃料或供应到其内部或形成在其内部的富燃料燃料/空气混合物。

3. 发明授权

US4838783A Dual burner facility with a fuel oil atomizer 失效
标题翻译：双燃烧器设有燃油雾化器
公开(公告)号：US4838783A
公开(公告)日：1989-06-13
申请号：US184365
申请日：1988-04-21
申请人： Cornel Fuglistaller , Jakob Keller , Thomas Sattelmayer
发明人： Cornel Fuglistaller , Jakob Keller , Thomas Sattelmayer
IPC分类号： F23D11/00 , F23D17/00
CPC分类号： F23D17/002 , F23D11/005 , F23D2900/00008
摘要： The resonance atomizer (4) of the burner facility has, as main components, a resonator ring (16) and a resonator cone (23), which each have an annular groove (25+24, respectively), which together form a resonance chamber (24+25). By a plurality of spacer strips (26) on the resonator ring (16), the resonator ring (16) and the resonator cone (23) are held apart by a distance which creates an annular inflow duct (27) for the oil/atomizing air mixture and outflow ducts (28) on the combustion space side for this mixture atomized in the resonance chamber (24+25). Between the components (16, 23) forming the resonator chamber (24+25) and the oil nozzle (7) there is an atomizing cross (17) with a baffle plate (19).
摘要翻译：燃烧器设备的共振雾化器（4）作为主要部件具有谐振器环（16）和共振器锥体（23），它们分别具有环形槽（25 + 24），它们共同形成共振室（24 + 25）。通过谐振器环（16）上的多个间隔条（26），谐振器环（16）和谐振器锥体（23）被隔开一段距离，该距离形成用于油/雾化的环形流入管道（27）在共振室（24 + 25）中雾化的混合物在燃烧空间侧的空气混合物和流出管道（28）。在形成谐振器室（24 + 25）的组件（16,23）和油嘴（7）之间存在具有挡板（19）的雾化十字（17）。

4. 发明授权

US5193995A Apparatus for premixing-type combustion of liquid fuel 失效
标题翻译：液体燃料预混燃烧装置
公开(公告)号：US5193995A
公开(公告)日：1993-03-16
申请号：US500191
申请日：1990-03-28
申请人： Jakob Keller , Thomas Sattelmayer , Daniel Styner
发明人： Jakob Keller , Thomas Sattelmayer , Daniel Styner
IPC分类号： F23C7/00 , F23D11/40 , F23D17/00 , F23R3/12
CPC分类号： F23D17/002 , F23C7/002 , F23D11/402 , F23R3/12 , F23C2900/07002
摘要： In premixing-type combustion of liquid fuel in a burner without a premixing section, a conical column (5) of liquid fuel is formed in the interior (14) of the burner, which column widens in the direction of flow and is surrounded by a rotating stream (15) of combustion air which flows tangentially into the burner. Ignition of the mixture takes place at the burner outlet, a backflow zone (6) forming in the region of the burner outlet. The burner itself consists of at least two hollow part-cone bodies (1, 2) which are superposed on one another and have a cone angle increasing in the direction of flow. The part-cone bodies (1, 2) are mutually offset, so that tangential air inlet slots (19, 20) are formed. A nozzle (3) placed at the burner head ensures injection of the liquid fuel (12) into the interior (14) of the burner.
摘要翻译：在没有预混合部分的燃烧器中液体燃料的预混合型燃烧中，在燃烧器的内部（14）中形成有液体燃料的锥形柱（5），该塔在流动方向上变宽并且被一个燃烧空气的旋转流（15）切向地流入燃烧器。混合物的点燃发生在燃烧器出口处，形成在燃烧器出口区域中的回流区（6）。燃烧器本身由至少两个彼此重叠并具有在流动方向上增加的锥角的中空部分锥体（1,2）组成。部分锥体（1,2）相互偏移，从而形成切向空气入口槽（19,20）。放置在燃烧器头部的喷嘴（3）确保将液体燃料（12）喷射到燃烧器的内部（14）中。

5. 发明授权

US4932861A Process for premixing-type combustion of liquid fuel 失效
标题翻译：液体燃料预混燃烧方法
公开(公告)号：US4932861A
公开(公告)日：1990-06-12
申请号：US282736
申请日：1988-12-12
申请人： Jakob Keller , Thomas Sattelmayer , Daniel Styner
发明人： Jakob Keller , Thomas Sattelmayer , Daniel Styner
IPC分类号： F23C5/32 , F23C7/00 , F23D11/10 , F23D11/40 , F23D17/00 , F23R3/12
CPC分类号： F23D11/402 , F23C7/002 , F23D17/002 , F23R3/12 , F23C2900/07002
摘要： In premixing-type combustion of liquid fuel in a burner without a premixing section, a conical column (5) of liquid fuel is formed in the interior (14) of the burner, which column widens in the direction of flow and is surrounded by a rotating stream (15) of combustion air which flows tangentially into the burner. Ignition of the mixture takes place at the burner outlet, a backflow zone (6) forming in the region of the burner outlet. The burner itself consists of at least two hollow part-cone bodies (1,2) which are superposed on one another and have a cone angle increasing in the direction of flow. The part-cone bodies (1, 2) are mutually offset, so that tangential air inlet slots (19, 20) are formed. A nozzle (3) placed at the burner head ensures injection of the liquid fuel (2) into the interior (14) of the burner.
摘要翻译：在没有预混合部分的燃烧器中液体燃料的预混合型燃烧中，在燃烧器的内部（14）中形成有液体燃料的锥形柱（5），该塔在流动方向上变宽并且被一个燃烧空气的旋转流（15）切向地流入燃烧器。混合物的点燃发生在燃烧器出口处，形成在燃烧器出口区域中的回流区（6）。燃烧器本身由至少两个中空部分锥体（1,2）组成，它们彼此重叠并且具有在流动方向上增加的锥角。部分锥体（1,2）相互偏移，从而形成切向空气入口槽（19,20）。放置在燃烧器头部的喷嘴（3）确保将液体燃料（2）注入到燃烧器的内部（14）中。

6. 发明授权

US5101633A Burner arrangement including coaxial swirler with extended vane portions 失效
标题翻译：燃烧器装置，包括具有扩展的风扇部分的同轴旋翼
公开(公告)号：US5101633A
公开(公告)日：1992-04-07
申请号：US509352
申请日：1990-04-16
申请人： Jakob Keller , Thomas Sattelmayer
发明人： Jakob Keller , Thomas Sattelmayer
IPC分类号： F23D14/02 , F23C7/00 , F23D11/38 , F23D14/22 , F23D14/24 , F23D14/26
CPC分类号： F23C7/004 , F23D14/24 , F23D14/26
摘要： This burner arrangement has a main feed channel (2) for a fuel-air mixture, which channel discharges into a combustion chamber (1). A swirler, which is provided with swirl vanes (5), is penetrated by a burner lance (3), and into which exit openings for the fuel feed discharge, is provided in this main feed channel (2). The aim is to create a burner arrangement in which it is impossible for undesired instances of ignition of the fuel-air mixture to occur outside the combustion chamber (1). This is achieved in that the exit openings are constructed as nozzles (9) which discharge into a region between the swirl vanes (5). In this regard, at least one nozzle is provided between two neighboring swirl vanes (5).
摘要翻译：该燃烧器装置具有用于燃料 - 空气混合物的主进料通道（2），该通道排放到燃烧室（1）中。设置有旋流叶片（5）的旋流器被燃烧器喷枪（3）穿透，并且在该主供给通道（2）中设置有用于燃料供给排出口的出口。目的是创建燃烧器布置，其中燃料 - 空气混合物的不期望的点燃事件不可能发生在燃烧室（1）的外部。这是通过将出口构造成喷射到旋转叶片（5）之间的区域中的喷嘴（9）来实现的。在这方面，在两个相邻的旋流叶片（5）之间提供至少一个喷嘴。

7. 发明授权

US4867674A Method and device for process heat generation 失效
标题翻译：加工发热的方法和装置
公开(公告)号：US4867674A
公开(公告)日：1989-09-19
申请号：US163712
申请日：1988-03-03
申请人： Jakob Keller , Thomas Sattelmayer
发明人： Jakob Keller , Thomas Sattelmayer
IPC分类号： F23C6/04
CPC分类号： F23C6/04
摘要： In the method, a process medium (14) is heated in two stages, in which fuel oil and gas premixed with air in a burner device (1) are partially burnt in a preliminary combustion chamber (12) substoichiometrically with an air coefficient (.lambda.) of approximately 0.7. The partially burnt mixture, which is low in nitrogen oxides, reaches a temperature of 1800.degree.-1900.degree. C., heats the process medium (14), which is already preheated to an intermediate temperature, to its final temperature in a heat exchanger (13) with counter-current flow and is cooled to 700.degree.-900.degree. C. In an air injection region (15) of the process heat generator the partially burnt mixture is mixed with quenching air in a stoichiometric ratio with respect to the unburnt fractions and is thereby completely burnt in a secondary combustion chamber (18) during which practically no nitrogen oxides (NO.sub.x) are produced. It reaches a temperature of 900.degree.-1300.degree. C. and then heats the process medium (14) from its initial temperature to the aforesaid intermediate temperature in a second heat exchanger (19 ). The process medium flows between the two heat exchangers (13, 19) and the process medium discharge line (25) in an annular duct (22) which essentially forms the outer boundary of the process heat generator.
摘要翻译：在该方法中，处理介质（14）分两个阶段进行加热，其中与燃烧器装置（1）中的空气混合的燃料油和气体在预燃烧室（12）中部分地燃烧，其中空气系数（λ ）约0.7。部分燃烧的氮氧化物混合物达到1800〜1900℃的温度，将已经预热至中间温度的工艺介质（14）加热至热交换器的最终温度（ 13），并且冷却至700-900℃。在工艺发热器的空气注入区域（15）中，将部分燃烧的混合物与化学计量比的淬火空气相对于未燃烧部分从而在实际上不产生氮氧化物（NOx）的二次燃烧室（18）中完全燃烧。达到900°-1300℃的温度，然后在第二热交换器（19）中将加工介质（14）从其初始温度加热到上述中间温度。处理介质在基本形成工艺发热体的外边界的环形管道（22）中的两个热交换器（13,19）和处理介质排出管线（25）之间流动。

8. 发明授权

US5081844A Combustion chamber of a gas turbine 失效
标题翻译：燃气轮机的燃烧室
公开(公告)号：US5081844A
公开(公告)日：1992-01-21
申请号：US487112
申请日：1990-03-02
申请人： Jakob Keller , Thomas Sattelmayer
发明人： Jakob Keller , Thomas Sattelmayer
IPC分类号： F23R3/02 , F23C7/00 , F23D11/40 , F23R3/00 , F23R3/12 , F23R3/30 , F23R3/34 , F23R3/44 , F23R3/50
CPC分类号： F23R3/30 , F23C7/002 , F23D11/402 , F23R3/12 , F23R3/34 , F23R3/50 , F23C2900/07002 , Y02E20/348
摘要： In an annular combustion chamber (A), a row of premixed burners (B, C) are located in the peripheral direction at the inlet end. The large premixed burners (B), which are the main burners of the annular combustion chamber (A), and the small premixed burners (C), which are the pilot burners of the annular combustion chamber, are located alternately relative to one another and at a uniform distance apart. Both the main burners (B) and the pilot burners (C) enter into a single annular front wall (10).
摘要翻译：在环形燃烧室（A）中，一排预混合燃烧器（B，C）位于入口端的圆周方向。作为环形燃烧室（A）的主要燃烧器的大型预混燃烧器（B）和作为环形燃烧室的先导燃烧器的小型预混合燃烧器（C）彼此交替地定位，彼此间隔一段距离。主燃烧器（B）和先导燃烧器（C）都进入单个环形前壁（10）。

9. 发明授权

US5400587A Gas turbine annular combustion chamber having radially displaced groups of oppositely swirling burners. 失效
标题翻译：燃气轮机环形燃烧室具有径向移位的相反旋转燃烧器组。
公开(公告)号：US5400587A
公开(公告)日：1995-03-28
申请号：US202687
申请日：1994-02-25
申请人： Jakob Keller , Thomas Sattelmayer , Peter Senior
发明人： Jakob Keller , Thomas Sattelmayer , Peter Senior
IPC分类号： F23R3/28 , F23R3/12 , F23R3/14 , F23R3/46 , F23R3/50
CPC分类号： F23R3/50 , F23R3/12 , F23C2900/07002
摘要： In a gas turbine combustion chamber which surrounds the rotor as an annulus and therefore has the shape of an annular combustion chamber, the front wall (10) is equipped with a number of burners whose ends occupy a uniform plane. These burners form a double ring (10b, 10c) on the front wall (10). In each ring, the same direction of rotation is present in the burners and this is opposite to the adjacent ring. In addition, two burners at a time are alternately displaced outwards and inwards in each ring in order to achieve a favorable flow field for combustion. The number of burners on the front wall (10) is divided into a larger quantity of piloting burners (A1, A2 ) and a smaller quantity of piloted burners (B1, B2).
摘要翻译：在作为环形空间围绕转子并因此具有环形燃烧室的形状的燃气轮机燃烧室中，前壁（10）配备有多个燃烧器，其端部占据统一的平面。这些燃烧器在前壁（10）上形成双环（10b，10c）。在每个环中，相同的旋转方向存在于燃烧器中，并且与相邻的环相反。此外，两个燃烧器一次在每个环中交替地向外和向内偏移，以获得有利的燃烧流场。前壁燃烧器（10）的数量分为大量的引燃燃烧器（A1，A2）和较少数量的先导燃烧器（B1，B2）。

10. 发明授权

US06202402B1 Gas-turbine construction 失效
标题翻译：燃气轮机构造
公开(公告)号：US06202402B1
公开(公告)日：2001-03-20
申请号：US09106095
申请日：1998-06-29
申请人： Thomas Sattelmayer
发明人： Thomas Sattelmayer
IPC分类号： F02C710
CPC分类号： F23R3/40 , F02C7/08 , F23R3/005
摘要： Described are a gas-turbine construction and a method of operating this gas-turbine construction, having an air compressor, a heat exchanger connected downstream of the air compressor, a combustion chamber, and a turbine which can be driven by hot combustion gases and from which the combustion gases are fed to the heat exchanger for heating the compressed supply air coming from the air compressor. The invention is distinguished by the fact that the heat exchanger and the combustion chamber are integrated in a common unit, and that fuel can be added to the supply air before entry into the unit, which fuel can be ignited catalytically in the form of an air/fuel mixture inside the unit, in which a catalyst is provided.
摘要翻译：描述了一种燃气轮机结构和操作该燃气轮机结构的方法，其具有空气压缩机，连接在空气压缩机下游的热交换器，燃烧室和能够被热燃烧气体驱动的涡轮机，这些燃烧气体被供给到热交换器以加热来自空气压缩机的压缩空气。本发明的特征在于，热交换器和燃烧室集成在共同的单元中，并且可以添加燃料在进入该单元之前的供给空气中，该燃料可以以单元内的空气/燃料混合物的形式催化地点燃，其中提供催化剂。

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