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1.发明授权Method and device for minimizing thermoacoustic vibrations in gas-turbine combustion chambers 失效用于最小化燃气轮机燃烧室中的热声振动的方法和装置公开(公告)号：US06170265B2
公开(公告)日：2001-01-09
申请号：US09111869
申请日：1998-07-08
IPC分类号： F02C724
CPC分类号： F23R3/286 , F05B2260/96 , F23M20/005 , F23R3/26 , F23R2900/00014
摘要： In a gas turbine having a device for the fuel injection, which injects fuel into a mixing device (12), the injected fuel being mixed with combustion air in the mixing device (12), and in which the gas turbine also has a combustion chamber (16) arranged downstream of the mixing device (12), the length of the combustion chamber being LBK and the length of the mixing device being LMix, in order to suppress thermoacoustic vibrations the premix combustion chamber (10) containing the combustion chamber (16) and the mixing device (12) is designed in such a way that an acoustic pressure fluctuation which occurs in the premix combustion chamber (10) at the combustion-chamber outlet (20) is superimposed in phase opposition on an entropy-wave-induced pressure fluctuation at a certain frequency to be damped.
摘要翻译： 在具有将燃料喷射到混合装置（12）中的用于燃料喷射的装置的燃气轮机中，喷射的燃料与混合装置（12）中的燃烧空气混合，并且其中燃气涡轮机还具有燃烧室 （16），布置在混合装置（12）的下游，燃烧室的长度为LBK，混合装置的长度为LMix，以便抑制含有燃烧室（16）的预混燃烧室（10）的热声振动 ），并且混合装置（12）被设计成使得在燃烧室出口（20）处的预混合燃烧室（10）中发生的声压波动相对于熵波引起的 压力波动在一定频率被阻尼。
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2.发明授权Method for active suppression of hydrodynamic instabilities in a combustion system and a combustion system for carrying out the method 有权用于主动抑制燃烧系统中的流体动力学不稳定性的方法和用于实施该方法的燃烧系统公开(公告)号：US06343927B1
公开(公告)日：2002-02-05
申请号：US09625041
申请日：2000-07-24
IPC分类号： F23C1100
摘要： A method for active suppression of hydrodynamic instabilities in a combustion system in which liquid or gaseous fuel is premixed with combustion air and the fuel/air mixture is then burnt. The mass flow of the supplied fuel is modulated on the basis of a selected time function. Simplification and increased functional reliability are achieved by the modulation which is carried out using fluidics.
摘要翻译： 一种在燃烧系统中主动抑制流体动力学不稳定性的方法，其中液体或气态燃料与燃烧空气和燃料/空气混合物预混合然后燃烧。 所提供的燃料的质量流量基于所选择的时间函数进行调制。 通过使用流体学进行的调制来实现简化和增加的功能可靠性。
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3.发明授权Method for combustion of a liquid fuel in a combustion system, and a combustion system for carrying out the method 失效燃烧系统中的液体燃料的燃烧方法和用于实施该方法的燃烧系统公开(公告)号：US06336806B1
公开(公告)日：2002-01-08
申请号：US09615950
申请日：2000-07-13
IPC分类号： F23D1132
CPC分类号： F23D11/32 , F23D2210/00
摘要： In a method for burning a liquid fuel in a combustion system (10) which comprises a combustion chamber (11) and at least one injection nozzle (13) through which liquid fuel is injected into the combustion chamber (11) in the form of a fuel spray (16) and is burnt there with combustion air being added, disturbance-free operation in a simple manner is distinguished in that, in order to actively suppress hydrodynamic instabilities in the combustion chamber (11), the injected fuel spray (16) is modulated by having an electrical voltage applied to it during the injection process, governed by a selected time function.
摘要翻译： 在用于燃烧燃料系统（10）中的液体燃料的方法中，所述燃烧系统（10）包括燃烧室（11）和至少一个喷射喷嘴（13），液体燃料通过该燃料室喷射到燃烧室（11）中， 燃料喷雾（16），并在其上燃烧有燃烧空气，其区别在于无扰动操作的特征在于为了主动地抑制燃烧室（11）中的流体动力学不稳定性，喷射的燃料喷雾（16） 通过在注入过程期间施加电压而被调制，由所选时间函数控制。
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4.发明授权Method and apparatus for minimizing thermoacoustic vibrations in gas-turbine combustion chambers 失效用于最小化燃气轮机燃烧室中的热声振动的方法和装置公开(公告)号：US06840046B2
公开(公告)日：2005-01-11
申请号：US09393714
申请日：1999-09-10
CPC分类号： F02C9/28 , F05D2260/96 , F05D2270/14 , F23R2900/00013 , F23R2900/00014
摘要： In a method of minimizing thermoacoustic vibrations in gas-turbine combustion chambers, a modulated spraying of liquid or gaseous premix fuel into a premix burner is carried out. The premix fuel is fed by means of two fuel lines (13, 14), and the modulation of the quantity of fed fuel is effected in each case by one fuel valve per fuel line.
摘要翻译： 在使燃气轮机燃烧室中的热声振动最小化的方法中，将液体或气体预混合燃料调制喷射到预混燃烧器中。 预混燃料通过两条燃料管路（13,14）进料，并且在每种情况下通过每个燃料管线一个燃料阀实现供给燃料量的调节。
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公开(公告)号：US06634457B2
公开(公告)日：2003-10-21
申请号：US09864395
申请日：2001-05-25
IPC分类号： F02M3500
CPC分类号： F01N1/023 , F01N1/02 , F01N2490/12 , F23D2210/00 , F23M20/005 , F23R2900/00014
摘要： An apparatus for damping acoustic vibrations in a combustor as well as a corresponding combustor arrangement with the apparatus. The apparatus includes a Helmholtz resonator (4) that can be connected via a connecting channel (2) with a combustor (1). The Helmholtz resonator (4) contains a hollow body (6) the volume of which can be changed by adding or draining a fluid via a supply line (5), or is located adjacent to such a hollow body in such a way that the resonance volume (3) of the Helmholtz resonator (4) is changed when the volume of the hollow body (6) is changed. This apparatus makes it possible to adjust the resonance frequency of a Helmholtz resonator arranged inside a pressure container in accordance with the respective current operating point of the combustor to be damped, without having to pass movable components through the pressure container.
摘要翻译： 一种用于抑制燃烧器中的声振动以及与该装置相应的燃烧器装置的装置。 该装置包括可经由连接通道（2）与燃烧器（1）连接的亥姆霍兹共振器（4）。 亥姆霍兹共振器（4）包含中空体（6），其体积可以通过经由供应管线（5）添加或排出流体而改变，或者位于这样的中空体附近，使得共振 当中空体（6）的体积改变时，亥姆霍兹共振器（4）的体积（3）改变。 该装置使得可以根据要抑制的燃烧器的相应的当前工作点来调节设置在压力容器内的亥姆霍兹共振器的谐振频率，而不必通过可移动部件通过压力容器。
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6.发明授权Gas turbine combustion chamber with two stages and enhanced acoustic properties 失效燃气轮机燃烧室具有两级和增强的声学特性
公开(公告)号：US6050078A
公开(公告)日：2000-04-18
申请号：US965865
申请日：1997-11-07
CPC分类号： F23R3/42 , F23R3/16 , F05B2260/96
摘要： In a combustion chamber, the hot gases are prepared sequentially via two stages (20, 40). Arranged at the end of the first stage (20) in the direction of flow is a cross-sectional constriction (30) via which the hot gases (21) prepared in the first stage (20) are passed over into the second stage (40). The Mach number at the outlet (31) of this cross-sectional constriction (30) corresponds to the area ratio of outlet area (A2) over inlet area (A1). This results in a low-reflection configuration in which low-frequency vibrations are absorbed to a significant extent. And acoustic energy reflected from the turbine is substantially reduced.
摘要翻译： 在燃烧室中，依次通过两个阶段（20,40）制备热气体。 在第一阶段（20）结束时在流动方向上排列的是横截面收缩（30），第一阶段（20）中制备的热气体（21）通过该横截面收缩通过第二阶段（40） ）。 该截面缩颈（30）的出口（31）处的马赫数对应于出口面积（A2）与入口面积（A1）的面积比。 这导致低反射配置，其中低频振动被很大程度地吸收。 并且从涡轮机反射的声能大大减小。
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7.发明授权Burner for operating an internal combustion engine, a combustion chamber of a gas turbine group or firing installation 失效用于操作内燃机的燃烧器，燃气轮机组的燃烧室或点火装置
公开(公告)号：US5375995A
公开(公告)日：1994-12-27
申请号：US181438
申请日：1994-01-14
CPC分类号： F23D17/002 , F23C2900/07002
摘要： In a double-cone burner, at least one row of nozzles (10) for a gaseous fuel containing highly reactive components and having a medium calorific value are arranged on the periphery of the partial conical bodies (1, 2) of the burner near the burner outlet at a distance of approximately 30% of the nominal burner diameter. In addition, there is a fuel conduit (11) and a distributing passage (17), placed in the region of the nozzles (10), for the highly reactive fuel. The gaseous fuel (15) containing highly reactive components is injected at high velocity through the nozzles (10), which have a diameter which is smaller than 1% of the nominal burner diameter, into the zones of high air velocity and the penetration depth and the direction of the fuel jets are matched to one another in such a way that ignition only takes place behind the burner, after mixing has occurred.
摘要翻译： 在双锥形燃烧器中，用于含有高反应性组分并具有中等热值的气态燃料的至少一排喷嘴（10）布置在燃烧器附近的燃烧器的部分圆锥体（1,2）的周边上 燃烧器出口距离标称燃烧器直径的约30％。 此外，在喷嘴（10）的区域中，存在用于高反应性燃料的燃料导管（11）和分配通道（17）。 含有高反应性组分的气体燃料（15）通过直径小于标称燃烧器直径的1％的喷嘴（10）以高速喷射到高空气速度和穿透深度的区域中， 燃料喷嘴的方向彼此匹配，使得在发生混合之后点燃仅发生在燃烧器后面。
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公开(公告)号：US07947119B2
公开(公告)日：2011-05-24
申请号：US12290112
申请日：2008-10-27
IPC分类号： F17C11/00
CPC分类号： C01B3/0005 , B01J2208/00141 , B01J2219/1923 , Y02E60/327 , Y02P20/129
摘要： In a hydrogen reservoir having a housing with a hydrogen storage material arranged in the housing for absorbing and releasing hydrogen as needed, the hydrogen reservoir includes at least one unit having a porous body surrounding a container in which the hydrogen storage material is contained and a method is provided for charging the hydrogen reservoir with hydrogen from a hydrogen filling stations.
摘要翻译： 在具有壳体的壳体中设置有用于根据需要吸收和释放氢气的储氢材料的储氢器，所述储氢器包括至少一个单元，所述至少一个单元具有围绕容纳所述储氢材料的容器的多孔体， 提供用于从氢气加注站向氢气储存器充电氢气。
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公开(公告)号：US20090127137A1
公开(公告)日：2009-05-21
申请号：US12290112
申请日：2008-10-27
CPC分类号： C01B3/0005 , B01J2208/00141 , B01J2219/1923 , Y02E60/327 , Y02P20/129
摘要： In a hydrogen reservoir having a housing with a hydrogen storage material arranged in the housing for absorbing and releasing hydrogen as needed, the hydrogen reservoir includes at least one unit having a porous body surrounding a container in which the hydrogen storage material is contained and a method is provided for charging the hydrogen reservoir with hydrogen from a hydrogen filling stations.
摘要翻译： 在具有壳体的壳体中设置有用于根据需要吸收和释放氢气的储氢材料的储氢器，所述储氢器包括至少一个单元，所述至少一个单元具有围绕容纳所述储氢材料的容器的多孔体， 提供用于从氢气加注站向氢气储存器充电氢气。
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公开(公告)号：US6164058A
公开(公告)日：2000-12-26
申请号：US111779
申请日：1998-07-08
CPC分类号： F23R3/005 , F02C7/045 , F05D2260/96 , F23R2900/00014 , F23R2900/03041
摘要： In an annular combustion chamber for a gas turbine, a combustion-chamber dome (14) is arranged upstream of an air-cooled combustion chamber (10). A first portion of an air flow (46) which comes from the compressor is admixed as combustion air to the combustion operation and cooling ducts (22; 24) feed a second portion of the air flow (46) coming from the compressor as cooling air into the combustion chamber (10). In this case, the cooling ducts (22; 24), which run at least in sections along the combustion chamber (10), have an entry (23; 25) into the combustion-chamber dome (14). The cooling ducts (22; 24) are designed for damping combustion-chamber oscillations in such a way that the acoustic impedance at the entry (23; 25) of the cooling ducts (22; 24) into the combustion-chamber dome (14) is minimized.
摘要翻译： 在用于燃气轮机的环形燃烧室中，燃烧室拱顶（14）布置在空气冷却燃烧室（10）的上游。 将来自压缩机的空气流（46）的第一部分作为燃烧空气混合到燃烧操作中，冷却管道（22; 24）将来自压缩机的空气流（46）的第二部分作为冷却空气 进入燃烧室（10）中。 在这种情况下，至少沿着燃烧室（10）的部分运行的冷却管道（22; 24）具有进入燃烧室拱顶（14）的入口（23; 25）。 冷却管道（22; 24）设计成用于阻止燃烧室振荡，使得冷却管道（22; 24）入口（23; 25）入口（29; 25）内的声阻抗进入燃烧室穹顶（14） 被最小化。
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