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    • 3. 发明授权
    • Burner system and method for damping such a burner system
    • 用于阻尼这种燃烧器系统的燃烧器系统和方法
    • US08631654B2
    • 2014-01-21
    • US13388347
    • 2011-03-07
    • Sven Bethke
    • Sven Bethke
    • F02C7/24
    • F23R3/286F23M20/005F23R3/46F23R3/54F23R2900/00014
    • A burner system is provided that includes at least two adjacent burners that are separate from each other. Each of the two burners has at least one combustion chamber and a head end. The head end includes at least a fuel injection and a fuel-air premix. Each burner has a cap with a cap side and cap upper side, wherein at least the cap upper side is arranged ahead of the head end, seen in the direction of flow. In this manner, a burner plenum is formed between the cap upper side and the head end. The at least two burner plenums thus formed have an acoustic connection. A method for damping such a burner system is also provided.
    • 提供了一种燃烧器系统,其包括彼此分离的至少两个相邻的燃烧器。 两个燃烧器中的每一个具有至少一个燃烧室和头端。 头端至少包括燃料喷射和燃料 - 空气预混物。 每个燃烧器具有帽盖和帽盖的上侧,其中至少帽上侧布置在头端的前方,从流动方向看。 以这种方式,在盖上侧和头端之间形成燃烧器增压室。 如此形成的至少两个燃烧器增压室具有声学连接。 还提供了一种用于阻尼这种燃烧器系统的方法。
    • 5. 发明申请
    • BURNER SYSTEM AND METHOD FOR DAMPING SUCH A BURNER SYSTEM
    • 燃烧器系统和用于阻燃燃烧器系统的方法
    • US20120291438A1
    • 2012-11-22
    • US13388347
    • 2011-03-07
    • Sven Bethke
    • Sven Bethke
    • F02C7/24F23M5/00
    • F23R3/286F23M20/005F23R3/46F23R3/54F23R2900/00014
    • A burner system is provided that includes at least two adjacent burners that are separate from each other. Each of the two burners has at least one combustion chamber and a head end. The head end includes at least a fuel injection and a fuel-air premix. Each burner has a cap with a cap side and cap upper side, wherein at least the cap upper side is arranged ahead of the head end, seen in the direction of flow. In this manner, a burner plenum is formed between the cap upper side and the head end. The at least two burner plenums thus formed have an acoustic connection. A method for damping such a burner system is also provided.
    • 提供了一种燃烧器系统,其包括彼此分离的至少两个相邻的燃烧器。 两个燃烧器中的每一个具有至少一个燃烧室和头端。 头端至少包括燃料喷射和燃料 - 空气预混物。 每个燃烧器具有帽盖和帽盖的上侧,其中至少帽上侧布置在头端的前方,从流动方向看。 以这种方式,在盖上侧和头端之间形成燃烧器增压室。 如此形成的至少两个燃烧器增压室具有声学连接。 还提供了一种用于阻尼这种燃烧器系统的方法。
    • 6. 发明申请
    • Method and Device for Damping Thermoacoustic Oscillations, in Particular in a Gas Turbine
    • 用于阻尼热声振动的方法和装置,特别是在燃气轮机中
    • US20090293481A1
    • 2009-12-03
    • US11991978
    • 2006-08-08
    • Sven Bethke
    • Sven Bethke
    • F02C7/24
    • F02C7/04F05D2260/962F23M20/005F23R2900/00013
    • The invention relates to a method for damping thermo-acoustic oscillations via a resonator having a resonator volume with thermo-acoustic oscillations induced in a cavity inclined to thermo-acoustic oscillations, and at least some of the thermo-acoustic oscillations being output from the cavity and being input into the resonator volume, with damping oscillations produced in the resonator volume, which are matched to the thermo-acoustic oscillations, with at least some of the damping oscillations being input into the cavity such that the damping oscillations and the thermo-acoustic oscillations overlap in an overlap area, and the oscillations being largely cancelled out. The invention relates to an apparatus for damping thermo-acoustic oscillations in a cavity, comprising a resonator with a resonator volume and a cavity. The invention also relates to a combustion chamber together with a method and an apparatus according to the invention, and to a gas turbine having a combustion chamber.
    • 本发明涉及一种用于通过谐振器阻尼热声振荡的方法,所述谐振器具有谐振器体积,其具有在倾斜于热声振荡的空腔中感应的热声振荡,并且至少一些热声振荡从腔体 并且在谐振器体积中输入谐振器体积中产生的阻尼振荡,其与热声振荡匹配,至少一些阻尼振荡被输入到空腔中,使得阻尼振荡和热声 振荡在重叠区域重叠,并且振荡被大大抵消。 本发明涉及一种用于阻尼空腔中的热声振荡的装置,包括具有谐振器体积和空腔的谐振器。 本发明还涉及一种燃烧室以及根据本发明的方法和装置以及具有燃烧室的燃气轮机。
    • 8. 发明授权
    • Method and device for damping thermoacoustic oscillations, in particular in a gas turbine
    • 用于阻尼热声振荡的方法和装置,特别是在燃气轮机中
    • US08919128B2
    • 2014-12-30
    • US11991978
    • 2006-08-08
    • Sven Bethke
    • Sven Bethke
    • F02C7/24F02C7/04
    • F02C7/04F05D2260/962F23M20/005F23R2900/00013
    • The invention relates to a method for damping thermo-acoustic oscillations via a resonator having a resonator volume with thermo-acoustic oscillations induced in a cavity inclined to thermo-acoustic oscillations, and at least some of the thermo-acoustic oscillations being output from the cavity and being input into the resonator volume, with damping oscillations produced in the resonator volume, which are matched to the thermo-acoustic oscillations, with at least some of the damping oscillations being input into the cavity such that the damping oscillations and the thermo-acoustic oscillations overlap in an overlap area, and the oscillations being largely cancelled out. The invention relates to an apparatus for damping thermo-acoustic oscillations in a cavity, comprising a resonator with a resonator volume and a cavity. The invention also relates to a combustion chamber together with a method and an apparatus according to the invention, and to a gas turbine having a combustion chamber.
    • 本发明涉及一种用于通过谐振器阻尼热声振荡的方法,所述谐振器具有谐振器体积,其具有在倾斜于热声振荡的空腔中感应的热声振荡,并且至少一些热声振荡从腔体 并且在谐振器体积中输入谐振器体积中产生的阻尼振荡,其与热声振荡匹配,至少一些阻尼振荡被输入到空腔中,使得阻尼振荡和热声 振荡在重叠区域重叠,并且振荡被大大抵消。 本发明涉及一种用于阻尼空腔中的热声振荡的装置,包括具有谐振器体积和空腔的谐振器。 本发明还涉及一种燃烧室以及根据本发明的方法和装置以及具有燃烧室的燃气轮机。