-
1.发明申请公开(公告)号：US20050019713A1
公开(公告)日：2005-01-27
申请号：US10725562
申请日：2003-12-03
CPC分类号： F23C9/006 , F23C2900/07002 , F23K2900/05003 , F23M20/005 , F23R2900/00013
摘要： The present invention relates to a method and a device for affecting thermoacoustic oscillations in a combustion system (1) comprising at least one burner (2) and at least one combustor (3), modulated injection of fuel being carried out. In order to improve the action of affecting the thermoacoustic oscillations, the modulated injection of the fuel is carried out into a recirculation zone (7) which forms in the combustor (3).
摘要翻译： 本发明涉及一种用于影响燃烧系统（1）中的热声振荡的方法和装置，该燃烧系统（1）包括至少一个燃烧器（2）和至少一个燃烧器（3），所述燃烧系统（1）被执行调节的燃料喷射。 为了改善影响热声振动的作用，燃料的调节喷射被进入在燃烧器（3）中形成的再循环区（7）。
-
2.发明申请Method and device for affecting thermoacoustic oscillations in combustion systems 审中-公开影响燃烧系统热声振荡的方法和装置公开(公告)号：US20050016181A1
公开(公告)日：2005-01-27
申请号：US10725564
申请日：2003-12-03
CPC分类号： F23R3/28 , F05B2260/96 , F23C2205/10 , F23N5/082 , F23R2900/00014
摘要： The present invention relates to a method and a device (1) for affecting thermoacoustic oscillations in a combustion system (5) comprising at least one burner (6) and at least one combustor (7), a gas flow forming in the region of the burner (6) being excited acoustically and/or modulated injection of fuel being carried out. In order to improve the action of affecting the thermoacoustic oscillations, the acoustic excitations of the gas flow and/or the modulated injections of the fuel are coordinated in order to affect at least two different interference frequencies of the thermoacoustic oscillations.
摘要翻译： 本发明涉及一种用于影响燃烧系统（5）中的热声振荡的方法和装置（1），其包括至少一个燃烧器（6）和至少一个燃烧器（7），在所述燃烧系统 燃烧器（6）被进行声学和/或调制的燃料喷射。 为了改善影响热声振荡的作用，气体流的声学激发和/或调节的燃料喷射被协调以便影响热声振荡的至少两个不同的干扰频率。
-
公开(公告)号：US20050100846A1
公开(公告)日：2005-05-12
申请号：US10954482
申请日：2004-10-01
CPC分类号： F23R3/16 , F23C2900/07002 , F23D2210/00 , F23R3/286 , F23R2900/00014
摘要： A burner 1 for a heat generator comprises an outlet 10 connectable to a combustion chamber 9, wherein at least part of an inner surface of the outlet 10 is provided with corrugations 11 which are adapted to facilitate the production of axial vorticity in the region of the outlet 10.
摘要翻译： 用于热发生器的燃烧器1包括可连接到燃烧室9的出口10，其中出口10的内表面的至少一部分设置有波纹11，其适于促进在该区域中产生轴向涡度 出口10。
-
公开(公告)号：US20050032014A1
公开(公告)日：2005-02-10
申请号：US10725565
申请日：2003-12-03
CPC分类号： F23C7/002 , F23C2900/07002 , F23D14/02 , F23D14/46 , F23D2210/00
摘要： A combustion system for a heat generator, the burner 1 being connected to a combustion chamber 6 by means of an outlet 10, wherein the outlet 10 comprises a multiply stepped transional structure 11 in the direction of flow of fluid 3 in the burner 1 so as to create turbulence in the fluid flow.
摘要翻译： 一种用于热发生器的燃烧系统，燃烧器1通过出口10连接到燃烧室6，其中出口10在燃烧器1中的流体3的流动方向上包括多级的跨导结构11，以便 以在流体流中产生湍流。
-
5.发明申请公开(公告)号：US20050016180A1
公开(公告)日：2005-01-27
申请号：US10725563
申请日：2003-12-03
CPC分类号： F23R3/28 , F05B2260/96 , F23C2205/10 , F23R2900/00014
摘要： The present invention relates to a method and a device (1) for affecting thermoacoustic oscillations in a combustion system (6) comprising at least one burner (70 and at least one combustor (8). In order to improve the action of affecting the thermoacoustic oscillations, a gas flow forming in the e region of the burner (7) is excited acoustically, modulated injection of fuel is carried out, the acoustic excitation of the gas flow and the modulated injection of the fuel are coordinated in order to affect the same interference frequency.
摘要翻译： 本发明涉及一种用于影响包括至少一个燃烧器（70和至少一个燃烧器（8））的燃烧系统（6）中的热声振荡的方法和装置（1）。为了改善影响热声的动作 在燃烧器（7）的e区域形成的气流在振荡中被声学地激励，进行燃料的调制喷射，气流的声学激发和调节的燃料喷射被协调以影响燃烧器 干扰频率。
-
公开(公告)号：US20050210860A1
公开(公告)日：2005-09-29
申请号：US10811219
申请日：2004-03-26
申请人： Ephraim Gutmark , Bryan Callender , Steven Martens
发明人： Ephraim Gutmark , Bryan Callender , Steven Martens
CPC分类号： F02K1/46 , F02K1/34 , F05D2260/96
摘要： A method for operating a gas turbine engine includes channeling compressed air from the gas turbine engine to a noise suppression system, and selectively operating the noise suppression system such that air discharged from the noise suppression system generates a plurality of flow control mechanisms in the gas turbine exhaust flowpath.
摘要翻译： 用于操作燃气涡轮发动机的方法包括将来自燃气涡轮发动机的压缩空气引导到噪声抑制系统，并且选择性地操作噪声抑制系统，使得从噪声抑制系统排出的空气在燃气轮机中产生多个流量控制机构 排气流路。
-
公开(公告)号：US06599121B2
公开(公告)日：2003-07-29
申请号：US09932094
申请日：2001-08-20
IPC分类号： F23D1402
CPC分类号： F23C7/002 , F23C2900/07002 , F23D11/402 , F23D14/74 , F23D17/002 , F23D2209/20
摘要： The subject of the invention is a method as well as an apparatus for suppressing flow vortices within a turbo power machine with a premix burner, into which fuel and air are introduced for mixing, which then leave the burner downstream along its burner axis in the form of a fuel/air mixture through a burner outlet and flow into a combustor located downstream from the burner in the flow direction of the fuel/air mixture. The invention is based on the basic idea of—for the fluid-mechanical stabilization of a premix burner, into which at least one combustion air stream (5) is fed tangentially into a burner chamber (6) and is mixed with an injected gaseous and/or liquid fuel (7;8) while forming a swirl flow (9) oriented coaxially to the burner axis and induces a reverse flow zone (15) at a change in the cross-section on a burner mouth (14), that is used during the operation of the burner to stabilize the flame—increasingly, radially deforming the swirl flow (9) within the burner chamber (6) in the direction of the burner mouth (14) and let it enter the combustor (12) in a non-rotation-symmetrical flow cross-section, whereby this deformation is created by reducing the free flow cross-section (18) of the burner chamber (6). The fuel/air mixture flows into the combustor with a non-rotation-symmetrical flow cross-section.
摘要翻译： 本发明的主题是一种方法以及用于在具有预混合燃烧器的涡轮动力机械中抑制流动涡流的装置，燃料和空气被引入燃料和空气中用于混合，然后将燃烧器沿其燃烧器轴向下留下 的燃料/空气混合物通过燃烧器出口流入燃料/空气混合物的流动方向上的燃烧器下游的燃烧器。 本发明基于用于预混合燃烧器的流体 - 机械稳定化的基本思想，其中至少一个燃烧空气流（5）被切向地进料到燃烧器室（6）中并与注入的气体和 /或液体燃料（7; 8），同时形成与燃烧器轴线同轴定向的涡流（9），并且在燃烧器口（14）上的横截面变化时引起反向流动区（15），也就是说 在燃烧器操作期间使用以使燃烧器口（14）的方向上的火焰逐渐变大，使得燃烧器室（6）内的涡流（9）径向变形，并使其进入燃烧器（12） 非旋转对称的流动横截面，由此通过减小燃烧室（6）的自由流动横截面（18）而产生这种变形。 燃料/空气混合物以非旋转对称的流动横截面流入燃烧器。
-
公开(公告)号：US06183240B2
公开(公告)日：2001-02-06
申请号：US09438588
申请日：1999-11-12
IPC分类号： F24C604
CPC分类号： F23C7/002 , F23C2900/07002 , F23D2210/00
摘要： A burner for operating a unit for generating a hot gas consists essentially of at least two hollow partial bodies (1, 2) which are interleaved in the flow direction and whose center lines extend offset relative to one another in such a way that adjacent walls of the partial bodies (1,2) form tangential air inlet ducts (5, 6) for the inlet flow of combustion air (7) into an internal space (8) prescribed by the partial bodies (1, 2). The burner has at least one fuel nozzle (11). In order to control flow instabilities in the burner, the inside of the burner outlet (17) has a plurality of nozzles (32) along the periphery of the burner outlet (17) for introducing axial vorticity into the flow, the nozzles (32) for injecting air (34) being arranged at an angle to the flow direction (30).
摘要翻译： 用于操作用于产生热气体的单元的燃烧器基本上由至少两个在流动方向上交错并且其中心线相对于彼此延伸偏移的中空部分体（1,2）构成，使得相邻的壁 部分主体（1,2）形成用于燃烧空气（7）入口流入由部分主体（1,2）规定的内部空间（8）的切向空气入口管道（5,6）。 燃烧器具有至少一个燃料喷嘴（11）。 为了控制燃烧器中的流动不稳定性，燃烧器出口（17）的内部具有沿着燃烧器出口（17）的周边的多个喷嘴（32），用于将轴向涡流引入流中，喷嘴（32） 用于喷射与流动方向（30）成一定角度排列的空气（34）。
-
公开(公告)号：USH1007H
公开(公告)日：1992-01-07
申请号：US737648
申请日：1985-05-24
摘要： In a solid fuel ramjet in which a fluid flow boundary layer extends along aurning fuel grain and receives combustible material liberated from the grain, exciting oscillations in air flowing toward the grain so that oscillations continue in the boundary layer and promote vortices in the layer to mix the air and the combustible material.
-
10.发明授权公开(公告)号：US07549857B2
公开(公告)日：2009-06-23
申请号：US10725562
申请日：2003-12-03
IPC分类号： F23C5/00
CPC分类号： F23C9/006 , F23C2900/07002 , F23K2900/05003 , F23M20/005 , F23R2900/00013
摘要： The present invention relates to a method and a device for affecting thermoacoustic oscillations in a combustion system (i) comprising at least one burner (2) and at least one combustor (3), modulated injection of fuel being carried out. In order to improve the action of affecting the thermoacoustic oscillations, the modulated injection of the fuel is carried out into a recirculation zone (7) which forms in the combustor (3).
摘要翻译： 本发明涉及一种用于影响燃烧系统（i）中的热声振荡的方法和装置，其包括至少一个燃烧器（2）和至少一个燃烧器（3），所述燃烧系统被执行的调节燃料喷射。 为了改善影响热声振动的作用，燃料的调节喷射被进入在燃烧器（3）中形成的再循环区（7）。
-
-
-
-
-
-
-
-
-
搜索结果
35 条记录 (耗时 0.015 秒)
