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公开(公告)号：US5513982A
公开(公告)日：1996-05-07
申请号：US225319
申请日：1994-04-08
IPC分类号： F23R3/12 , B01F5/04 , B01F5/06 , F15D1/02 , F23D11/40 , F23R3/20 , F23R3/30 , F23R3/58 , F23D14/46
CPC分类号： F23D11/408 , B01F5/0451 , B01F5/061 , B01F5/0656 , F15D1/02 , F23R3/20 , B01F2005/0621 , B01F2005/0622
摘要： In a combustion chamber, a gaseous or liquid fuel is injected as a secondary flow into a gaseous, channelized main flow. The main flow is directed to pass over a plurality of vortex generators (9) arranged side by side over the width or circumference of the channel (20) through which the flow passes. The height (h) of the vortex generators is at least 50% of the height (H) of the channel through which the flow passes or of that part of the channel associated with the vortex generators. The secondary flow is introduced into the channel (20) in the immediate vicinity of the vortex generators (9). Longitudinal vortices without any recirculation region are produced in the channel through which the flow passes by means of the new static mixer. Extraordinarily short mixing distances, with a low pressure loss at the same time, are thus achieved in a combustion chamber according to the invention.
摘要翻译： 在燃烧室中，将气态或液态燃料作为二次流注入气态，通道化的主流中。 主要流动是通过在通道（20）的宽度或圆周上并排布置的多个涡流发生器（9），流体通过该涡流发生器。 涡流发生器的高度（h）至少为流经的通道的高度（H）或与涡流发生器相关的通道的那部分的高度（H）的50％。 二次流在涡流发生器（9）附近被引入通道（20）中。 在通过新的静态混合器流动的通道中产生没有任何再循环区域的纵向涡流。 因此，在根据本发明的燃烧室中实现了非常短的混合距离，同时具有低的压力损失。
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公开(公告)号：US5518311A
公开(公告)日：1996-05-21
申请号：US225397
申请日：1994-04-08
申请人： Rolf Althaus , Alexander Beeck , Yau-Pin Chyou , Adnan Eroglu
发明人： Rolf Althaus , Alexander Beeck , Yau-Pin Chyou , Adnan Eroglu
IPC分类号： F23R3/12 , B01F5/00 , B01F5/04 , B01F5/06 , F02K1/38 , F23D14/62 , F23D14/70 , F23R3/16 , F23R3/28 , F23R3/32 , F23R3/34 , B01F15/02
CPC分类号： B01F5/061 , B01F5/0451 , B01F5/0473 , B01F5/0656 , F02K1/386 , F23R3/16 , F23R3/286
摘要： A mixing chamber for introducing a gaseous secondary flow into a gaseous, ducted main flow includes a plurality of vortex generators to facilitate mixing of the flows. The secondary main flow has a substantially smaller mass flow than the main flow. The main flow is guided via the plurality of vortex generators arranged adjacent to one another over the width or the periphery of the duct through which flow takes place. The height (h) of the vortex generators is at least 50% of the height (H) of the duct through which flow takes place. The secondary flow is fed into the duct in the immediate region of tile vortex generators. The mixing chamber according to the invention exhibits extraordinarily short mixing distances in the mixing chamber with a simultaneously low pressure loss.
摘要翻译： 用于将气态二次流引入气体管道主流的混合室包括多个涡流发生器以便于流动的混合。 次要主流体的质量流量大于主流量。 主流通过多个涡流发生器引导，多个涡流发生器彼此相邻布置在通过其流动的管道的宽度或周边上。 涡流发生器的高度（h）至少为发生管道的高度（H）的50％。 二次流在瓦片涡流发生器的直接区域内进入管道。 根据本发明的混合室在混合室中表现出非常短的混合距离，同时具有低的压力损失。
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公开(公告)号：US5490388A
公开(公告)日：1996-02-13
申请号：US310393
申请日：1994-09-22
摘要： In a gas turbine combustion chamber in which for cooling purposes use is made of combinations of convective heat transfer mechanisms whose basic principle is the elimination of heat by flow, the transition from the convective cooling channel (4) to the plenum upstream of the burners (5) is in the form of a small diffuser (6). The total pressure loss in the entire system is thereby reduced, thus leading to improved efficiency with minimum emissions.
摘要翻译： 在用于冷却目的的燃气轮机燃烧室中，使用的是对流传热机构的组合，其基本原理是通过流动消除热量，从对流冷却通道（4）到燃烧器上游的增压室 5）是小扩散器（6）的形式。 因此，整个系统中的总压力损失减小，从而以最小的排放物提高了效率。
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公开(公告)号：US5615546A
公开(公告)日：1997-04-01
申请号：US323688
申请日：1994-10-17
CPC分类号： F23R3/002 , F05B2260/20 , F05B2260/201
摘要： In a gas turbine combustion chamber cooled by means of impingement and convection cooling or pure convection cooling, a compensating flow of the cooling air is guided between adjacent cooling ducts (2) in such a way that the flow velocity in the cooling duct (2) always exceeds a critical limiting value even downstream of a local damage location (6) so that the temperature is less than a critical limiting value. The compensating flow is led past the combustion chamber outer wall. Connecting openings (5) are arranged between adjacent cooling ducts (2) and are respectively offset on the opposite sides of the cooling duct (2).
摘要翻译： 在通过冲击和对流冷却或纯对流冷却冷却的燃气轮机燃烧室中，冷却空气的补偿流在相邻的冷却管道（2）之间被引导，使得冷却管道（2）中的流速 总是超过临界极限值，甚至在局部损伤位置（6）的下游，使得温度小于临界极限值。 补偿流通过燃烧室外壁。 连接开口（5）设置在相邻的冷却管道（2）之间，并分别偏置在冷却管道（2）的相对侧上。
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公开(公告)号：US5651253A
公开(公告)日：1997-07-29
申请号：US699731
申请日：1996-08-20
CPC分类号： F23R3/002 , F05B2260/20 , F05B2260/201
摘要： In a gas turbine combustion chamber cooled by means of impingement and convection cooling or pure convection cooling, a compensating flow of the cooling air is guided between adjacent cooling ducts (2) in such a way that the flow velocity in the cooling duct (2) always exceeds a critical limiting value even downstream of a local damage location (6) so that the temperature is less than a critical limiting value. The compensating flow is led past the combustion chamber outer wall. Connecting openings (5) are arranged between adjacent cooling ducts (2) and are respectively offset on the opposite sides of the cooling duct (2).
摘要翻译： 在通过冲击和对流冷却或纯对流冷却冷却的燃气轮机燃烧室中，冷却空气的补偿流在相邻的冷却管道（2）之间被引导，使得冷却管道（2）中的流速 总是超过临界极限值，甚至在局部损伤位置（6）的下游，使得温度小于临界极限值。 补偿流通过燃烧室外壁。 连接开口（5）设置在相邻的冷却管道（2）之间，并分别偏置在冷却管道（2）的相对侧上。
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公开(公告)号：US5426943A
公开(公告)日：1995-06-27
申请号：US340454
申请日：1994-11-14
CPC分类号： F23R3/54 , F23R3/02 , F05B2240/32 , F05B2260/222 , F05B2260/2241
摘要： In a gas turbine combustion chamber (1)--having environment-friendly burners (5) which consist of at least two hollow partial conical bodies which are positioned one upon the other in the flow direction and whose longitudinal axes of symmetry extend radially offset relative to one another, by which means tangential opposed-flow air inlet slots are produced for a combustion air flow, at least one nozzle for spraying in the fuel being placed in the hollow conical space formed by the cone-shaped partial conical bodies, and having a cooling duct (4), which is bounded by the combustion chamber inner wall (2) and the combustion chamber outer wall (3), along which the cooling air flows and in which longitudinal and transverse ribs (8) can be arranged--the cooling duct (4) has a continuously decreasing height and/or increasing surface roughness in the flow direction of the cooling air. The total mass flow coming from the compressor (7) is used for pure convective cooling of the combustion chamber inner wall (2) and takes part in the combustion.
摘要翻译： 在燃气轮机燃烧室（1）中，具有环境友好的燃烧器（5），其由至少两个中空部分圆锥体组成，所述至少两个中空部分圆锥体在流动方向上一个一个地定位，并且其纵向对称轴线相对于 通过这种方式，为燃烧空气流产生切向相对流动的空气入口狭槽，至少一个用于喷射在燃料中的喷嘴被放置在由锥形部分圆锥体形成的空心锥形空间中，并具有 冷却管道（4），其由燃烧室内壁（2）和燃烧室外壁（3）限定，冷却空气流过冷却管道，其中可布置纵向和横向肋（8） - 冷却 管道（4）在冷却空气的流动方向上具有连续降低的高度和/或增加的表面粗糙度。 来自压缩机（7）的总质量流量用于燃烧室内壁（2）的纯对流冷却并参与燃烧。
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公开(公告)号：US5313785A
公开(公告)日：1994-05-24
申请号：US38274
申请日：1993-03-29
申请人： Rolf Althaus , Yau-Pin Chyou , Erwin Zauner
发明人： Rolf Althaus , Yau-Pin Chyou , Erwin Zauner
摘要： A dynamic pressure machine with integrated combustion has a cellular wheel containing a number of cells, in which a continuously recurring ignition and combustion process takes place. Neither energy supply from the outside nor a control action should be required to maintain this continuously recurring process. Means are provided for the automatic ignition and combustion of the entering fresh air-fuel mixture, in particular: at least one hot gas pocket disposed on the wall of the cell; a catalytic coating of the cell wall; and, a hot spot in the cell.
摘要翻译： 具有集成燃烧的动态压力机具有包含多个电池的蜂窝轮，其中发生连续反复的点火和燃烧过程。 不需要外界的能量供应和控制措施来维持这种持续的循环过程。 提供了用于进入新鲜空气燃料混合物的自动点燃和燃烧的装置，特别是设置在电池壁上的至少一个热气袋; 细胞壁的催化涂层; 和电池中的热点。
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公开(公告)号：US5465569A
公开(公告)日：1995-11-14
申请号：US290287
申请日：1994-08-15
申请人： Rolf Althaus , Yau-Pin Chyou , Hans U. Frutschi , Christian Genet , Peter Kamber , Anders Lindvall , Thomas Sattelmayer , Peter Senior , Peter Rufli
发明人： Rolf Althaus , Yau-Pin Chyou , Hans U. Frutschi , Christian Genet , Peter Kamber , Anders Lindvall , Thomas Sattelmayer , Peter Senior , Peter Rufli
CPC分类号： F02C9/34 , F02C6/003 , F23R2900/03341
摘要： A method of establishing part-load operation is proposed for a turbine group. This gas turbine group consists essentially of a compressor unit (1), of an HP combustion chamber (4) downstream of the compressor unit (1), of an HP turbine (5) downstream of this HP combustion chamber (4), of an LP combustion chamber (8) operating by self-ignition and arranged downstream of the HP turbine (5), the hot gases (10) of which LP combustion chamber (8) being admitted to an LP turbine (11). The temperature at outlet from the HP turbine (5) remains essentially the same due to the reduction of the fuel quantity in the LP combustion chamber (8) to zero. Furthermore, the fuel quantity of the HP combustion chamber (4) remains approximately constant during the reduction of the fuel quantity in the LP combustion chamber (8) so that the temperature at inlet to the HP turbine (5) likewise remains constant.
摘要翻译： 对涡轮机组提出了建立部分负荷运行的方法。 该燃气轮机组基本上由在该HP燃烧室（4）下游的HP涡轮机（5）的压缩机单元（1）下游的HP燃烧室（4），HP涡轮机（5）的压缩机单元（1） LP燃烧室（8）通过自点火操作并且布置在HP涡轮机（5）的下游，LP燃烧室（8）的热气体（10）被允许进入LP涡轮机（11）。 由于LP燃烧室（8）中的燃料量减少到零，来自HP涡轮（5）的出口处的温度保持基本相同。 此外，在LP燃烧室（8）中的燃料量的减少期间，HP燃烧室（4）的燃料量保持大致恒定，使得HP涡轮机（5）入口处的温度同样保持恒定。
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公开(公告)号：US5573395A
公开(公告)日：1996-11-12
申请号：US383580
申请日：1995-02-03
申请人： Rolf Althaus , Yau-Pin Chyou
发明人： Rolf Althaus , Yau-Pin Chyou
CPC分类号： F23D14/22 , F23D11/402 , F23D23/00 , F05B2240/122 , F23C2900/07002
摘要： A premixing burner comprises a pilot burner (101) operating on the double-cone principle and a plurality of main burners arranged around the pilot burner. A gaseous and/or liquid fuel is injected into the main burner (52), which has a circular duct (20), as a secondary flow into a gaseous main flow. The main flow is first of all guided over vortex generators (9), a plurality of which are arranged next to one another around the circumference of the duct (20) through which flow takes place.
摘要翻译： 预混合燃烧器包括以双锥原理工作的引燃燃烧器（101）和围绕引燃燃烧器布置的多个主燃烧器。 气体和/或液体燃料被注入具有圆形管道（20）的主燃烧器（52）中，作为二次流入气态主流。 主要流动首先在涡流发生器（9）上引导，多个涡流发生器围绕导管（20）的周边彼此相邻布置，通过该流体发生流动。
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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
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
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