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1. 发明授权

US06837050B2 Gas turbine combustor 有权
标题翻译：燃气轮机燃烧器
公开(公告)号：US06837050B2
公开(公告)日：2005-01-04
申请号：US10124413
申请日：2002-04-18
申请人： Shigemi Mandai , Kiyoshi Suenaga , Kuniaki Aoyama , Kazufumi Ikeda , Katsunori Tanaka
发明人： Shigemi Mandai , Kiyoshi Suenaga , Kuniaki Aoyama , Kazufumi Ikeda , Katsunori Tanaka
IPC分类号： F02C7/18 , F23M99/00 , F23R3/00 , F23R3/06 , F23R3/10 , F23R3/30 , F02C7/25
CPC分类号： F23R3/06 , F23D2211/00 , F23M20/005 , F23R3/005 , F23R2900/00001 , F23R2900/00014
摘要： A gas turbine combustor includes a side wall, for defining a combustion volume, having upstream and downstream ends, a pilot nozzle, disposed adjacent the upstream end of the side wall, for discharging a pilot fuel to form a diffusion flame in the combustion volume, and a plurality of main nozzles, provided around the pilot nozzles, for discharging a fuel-air mixture to form premixed flames in the combustion volume. Film air is supplied into the combustion volume downstream of the main nozzles along the inner surface of the side wall to reduce the fuel-air ratio in a region adjacent the inner surface of the side wall and to restrain a combustion-driven oscillation in the combustion volume.

2. 发明授权

US06837051B2 Gas turbine combustor 有权
标题翻译：燃气轮机燃烧器
公开(公告)号：US06837051B2
公开(公告)日：2005-01-04
申请号：US10671472
申请日：2003-09-29
申请人： Shigemi Mandai , Kiyoshi Suenaga , Kuniaki Aoyama , Kazufumi Ikeda , Katsunori Tanaka
发明人： Shigemi Mandai , Kiyoshi Suenaga , Kuniaki Aoyama , Kazufumi Ikeda , Katsunori Tanaka
IPC分类号： F02C7/18 , F23M99/00 , F23R3/00 , F23R3/06 , F23R3/10 , F23R3/30 , F02C7/24
CPC分类号： F23R3/06 , F23D2211/00 , F23M20/005 , F23R3/005 , F23R2900/00001 , F23R2900/00014
摘要： A gas turbine combustor includes a side wall, for defining a combustion volume, having upstream and downstream ends, a pilot nozzle, disposed adjacent the upstream end of the side wall, for discharging a pilot fuel to form a diffusion flame in the combustion volume, and a plurality of main nozzles, provided around the pilot nozzles, for discharging a fuel-air mixture to form premixed flames in the combustion volume. Film air is supplied into the combustion volume downstream of the main nozzles along the inner surface of the side wall to reduce the fuel-air ratio in a region adjacent the inner surface of the side wall and to restrain a combustion-driven oscillation in the combustion volume.
摘要翻译：燃气轮机燃烧器包括用于限定具有上游和下游端的燃烧体积的侧壁，邻近侧壁的上游端设置的先导喷嘴，用于排放引燃燃料以在燃烧体积中形成扩散火焰，以及设置在先导喷嘴周围的多个主喷嘴，用于排出燃料 - 空气混合物以在燃烧体积中形成预混合火焰。薄膜空气沿着侧壁的内表面供应到主喷嘴下游的燃烧体积中，以减小邻近侧壁内表面的区域中的燃料空气比，并且抑制燃烧驱动的燃烧驱动卷。

3. 发明授权

US07832211B2 Gas turbine combustor and a gas turbine equipped therewith 有权
标题翻译：燃气轮机燃烧器和配备有燃气轮机的燃气轮机
公开(公告)号：US07832211B2
公开(公告)日：2010-11-16
申请号：US10525004
申请日：2003-11-28
申请人： Kazufumi Ikeda , Shigemi Mandai , Yutaka Kawata , Kuniaki Aoyama , Masaki Ono , Katsunori Tanaka
发明人： Kazufumi Ikeda , Shigemi Mandai , Yutaka Kawata , Kuniaki Aoyama , Masaki Ono , Katsunori Tanaka
IPC分类号： F02C7/24 , F23M5/00
CPC分类号： F23R3/04 , F05B2260/962 , F23M20/005 , F23R2900/00014 , Y02T50/675
摘要： In order to realize a stable decrease in NOx, a gas turbine combustor is supplied which can reduce combustion vibration. A combustor (3) is provided with a first box body (30), which is installed outside an object body (20) such as a combustor basket (6), a transition piece (7) or a bypass duct (11) so as to form a first internal space (31) having a predetermined capacity; and a first throat (32) having a predetermined length which has one end (32a) open to a side wall (20a) of the object body (20) and has the other end (32b) open to a first internal space (31); wherein, a first resistive element (33) having a multiple number of through-holes is inserted and engaged to one end (32a). Fluid particles serving as vibration elements of combustion vibration caused in a combustion region are effectively trapped by the first resistive element (33) and at the same time resonate with the air of the first internal space (31) being connected through the first throat (32) and vibrate in the neighborhood of the first resistive element (33), thereby damping vibration amplitude thereof.
摘要翻译：为了实现NOx的稳定降低，提供能够减少燃烧振动的燃气轮机燃烧器。燃烧器（3）设置有第一箱体（30），其安装在诸如燃烧器筐（6），过渡件（7）或旁通管道（11）的物体（20）的外部，以便以形成具有预定容量的第一内部空间（31）; 以及具有一定长度的第一喉部（32），所述第一喉部（32）的一端（32a）朝向所述物体（20）的侧壁（20a）开口，并且另一端（32b）向第一内部空间（31）开放， ; 其中，具有多个通孔的第一电阻元件（33）被插入并接合到一端（32a）。作为在燃烧区域中产生的燃烧振动的振动元件的流体颗粒被第一电阻元件（33）有效地捕获，同时与通过第一喉部（32）连接的第一内部空间（31）的空气共振）并且在第一电阻元件（33）附近振动，从而阻尼振动振幅。

4. 发明申请

US20050223707A1 Gas turbine combustor, and gas turbine with the combustor 有权
标题翻译：燃气轮机燃烧器和燃气轮机
公开(公告)号：US20050223707A1
公开(公告)日：2005-10-13
申请号：US10525004
申请日：2003-11-28
申请人： Kazufumi Ikeda , Shigemi Mandai , Yutaka Kawata , Kuniaki Aoyama , Masaki Ono , Katsunori Tanaka
发明人： Kazufumi Ikeda , Shigemi Mandai , Yutaka Kawata , Kuniaki Aoyama , Masaki Ono , Katsunori Tanaka
IPC分类号： F23M99/00 , F23R3/04 , F02C7/24
CPC分类号： F23R3/04 , F05B2260/962 , F23M20/005 , F23R2900/00014 , Y02T50/675
摘要： In order to realize a stable decrease in NOx, a gas turbine combustor is supplied which can reduce combustion vibration. A combustor (3) is provided with a first box body (30), which is installed outside an object body (20) such as a combustor basket (6), a transition piece (7) or a bypass duct (11) so as to form a first internal space (31) having a predetermined capacity; and a first throat (32) having a predetermined length which has one end (32a) open to a side wall (20a) of the object body (20) and has the other end (32b) open to a first internal space (31); wherein, a first resistive element (33) having a multiple number of through-holes is inserted and engaged to one end (32a). Fluid particles serving as vibration elements of combustion vibration caused in a combustion region are effectively trapped by the first resistive element (33) and at the same time resonate with the air of the first internal space (31) being connected through the first throat (32) and vibrate in the neighborhood of the first resistive element (33), thereby damping vibration amplitude thereof.
摘要翻译：为了实现NOx的稳定降低，提供能够减少燃烧振动的燃气轮机燃烧器。燃烧器（3）设置有第一箱体（30），其安装在诸如燃烧器筐（6），过渡件（7）或旁通管道（11）的物体（20）的外部，以便以形成具有预定容量的第一内部空间（31）; 以及具有预定长度的第一喉部（32），所述第一喉部（32）具有与所述物体（20）的侧壁（20a）相通的一端（32a），并且另一端（32b）向第一内部空间（31）; 其中，具有多个通孔的第一电阻元件（33）插入并接合到一端（32a）。作为在燃烧区域中产生的燃烧振动的振动元件的流体颗粒被第一电阻元件（33）有效地捕获，同时与通过第一喉部（32）连接的第一内部空间（31）的空气共振）并且在第一电阻元件（33）附近振动，从而阻尼振动振幅。

5. 发明授权

US07089741B2 Gas turbine combustor 有权
标题翻译：燃气轮机燃烧器
公开(公告)号：US07089741B2
公开(公告)日：2006-08-15
申请号：US10927529
申请日：2004-08-27
申请人： Kazufumi Ikeda , Tatsuo Ishiguro , Katsunori Tanaka , Satoshi Tanimura
发明人： Kazufumi Ikeda , Tatsuo Ishiguro , Katsunori Tanaka , Satoshi Tanimura
IPC分类号： F02C7/24
CPC分类号： F23R3/002 , F23M20/005 , F23R2900/00014
摘要： A gas turbine combustor includes a combustion liner in which a combustion region is formed; and a housing provided for a wall of the combustion liner in a predetermined circumferential region of the combustion liner to form a resonance space between the combustion liner and the housing. The combustion region and the resonance space are connected by a plurality of combustion liner through-holes, and a circumferential length of the housing is longer than a diameter of the combustion liner.
摘要翻译：燃气轮机燃烧器包括其中形成有燃烧区域的燃烧衬套; 以及壳体，其设置在所述燃烧衬套的预定圆周区域中的所述燃烧衬套的壁上，以在所述燃烧衬套和所述壳体之间形成共振空间。燃烧区域和共振空间通过多个燃烧衬套通孔连接，壳体的圆周长度大于燃烧衬套的直径。

6. 发明授权

US06688107B2 Gas turbine combustion device 有权
标题翻译：燃气轮机燃烧装置
公开(公告)号：US06688107B2
公开(公告)日：2004-02-10
申请号：US10023897
申请日：2001-12-21
申请人： Masaki Ono , Masaharu Nishimura , Keizo Ohnishi , Kazufumi Ikeda , Katsunori Tanaka
发明人： Masaki Ono , Masaharu Nishimura , Keizo Ohnishi , Kazufumi Ikeda , Katsunori Tanaka
IPC分类号： F02C724
CPC分类号： F23R3/002 , F23M20/005
摘要： A gas turbine combustion device comprises a plurality of combustion devices. Each combustion device has an inner cylinder and a tail cylinder in a vehicle chamber. An acoustic sleeve is provided between each inner cylinder and a corresponding outer cylinder in the vehicle chamber. An acoustic coupling effect with a vehicle chamber can be reduced.
摘要翻译：燃气轮机燃烧装置包括多个燃烧装置。每个燃烧装置在车室中具有内筒和尾筒。声学套筒设置在车厢内的每个内筒与对应的外筒之间。可以减少与车辆室的声耦合效应。

7. 发明授权

US06907736B2 Gas turbine combustor having an acoustic energy absorbing wall 有权
标题翻译：具有声能吸收壁的燃气轮机燃烧器
公开(公告)号：US06907736B2
公开(公告)日：2005-06-21
申请号：US10032035
申请日：2001-12-31
申请人： Keizo Ohnishi , Kazufumi Ikeda , Masaki Ono , Masaharu Nishimura , Katsunori Tanaka
发明人： Keizo Ohnishi , Kazufumi Ikeda , Masaki Ono , Masaharu Nishimura , Katsunori Tanaka
IPC分类号： F23M99/00 , F23R3/00 , F02C7/24 , F23R3/06
CPC分类号： F23R3/002 , F23M20/005 , F23R2900/00014
摘要： A gas turbine combustor in which a part or all of the wall of the combustor disposed within an intake chamber is formed as an acoustic energy absorbing member that can absorb the acoustic energy of a combustion variation generated within the combustor. The acoustic energy absorbing member is constructed of a thin corrugated plate in a circumferential direction, a high-temperature-proof perforated material, or a back plate disposed at the outside of a perforated plate in a radial direction with a distance from the perforated plate. It is also possible to provide a covering member at the outside of the acoustic energy absorbing member in a radial direction, for covering the acoustic energy absorbing member with a distance from the acoustic energy absorbing member. It is preferable that the acoustic energy-absorbing member and/or the covering member are reinforced with a frame that extends in a circumferential direction and/or a longitudinal direction.
摘要翻译：一种燃气轮机燃烧器，其中设置在进气室内的燃烧器的壁的一部分或全部形成为能够吸收燃烧器内产生的燃烧变化的声能的声能吸收构件。声能吸收构件由圆周方向的薄波纹板，耐高温多孔材料或设置在多孔板的外侧的径向方向上与多孔板的距离构成的背板构成。还可以在声能吸收构件的外侧沿径向方向设置覆盖构件，以覆盖距离声能吸收构件一定距离的声能吸收构件。优选的是，声能吸收构件和/或覆盖构件通过在圆周方向和/或纵向方向上延伸的框架来增强。

8. 发明授权

US06920758B2 Gas turbine and the combustor thereof 有权
标题翻译：燃气轮机及其燃烧器
公开(公告)号：US06920758B2
公开(公告)日：2005-07-26
申请号：US10231004
申请日：2002-08-30
申请人： Keisuke Matsuyama , Katsunori Tanaka , Yasuhiko Ikegami , Masaki Ono , Kazufumi Ikeda
发明人： Keisuke Matsuyama , Katsunori Tanaka , Yasuhiko Ikegami , Masaki Ono , Kazufumi Ikeda
IPC分类号： F23M99/00 , F23R3/28 , F23R3/34 , F02C3/00
CPC分类号： F23R3/343 , F23M20/005 , F23R3/286 , F23R2900/00014
摘要： The objective is to provide a gas turbine and the combustor thereof in which super high frequency combustion oscillation and the generation of NOx are reduced.The fluctuation in pressure which induces the fluctuation in heat liberation is suppressed in the gas turbine combustor comprising a plurality of main fuel supply nozzles, each having a premixing nozzle at the top end part thereof, by providing in the space upstream from the premixing nozzles partition elements for dividing the space along the axis of the combustor or a honeycomb element having air passages in the axial direction, or by providing premixing nozzles composed of cylindrical elements with many holes.
摘要翻译：目的是提供一种燃气轮机及其燃烧器，其中超高频燃烧振荡和NOx的产生减少。在包括多个主燃料供给喷嘴的燃气轮机燃烧器中抑制导致热释放波动的压力波动，每个主燃料供给喷嘴在其顶端部分具有预混合喷嘴，通过在预混合喷嘴分隔件用于沿着燃烧器的轴线分隔空间的元件或具有沿轴向具有空气通道的蜂窝元件，或者通过提供由具有许多孔的圆柱形元件组成的预混合喷嘴。

9. 发明申请

US20050097890A1 Gas turbine combustor 有权
标题翻译：燃气轮机燃烧器
公开(公告)号：US20050097890A1
公开(公告)日：2005-05-12
申请号：US10927529
申请日：2004-08-27
申请人： Kazufumi Ikeda , Tatsuo Ishiguro , Katsunori Tanaka , Satoshi Tanimura
发明人： Kazufumi Ikeda , Tatsuo Ishiguro , Katsunori Tanaka , Satoshi Tanimura
IPC分类号： F23R3/16 , F02C7/00 , F02C7/24 , F23M99/00 , F23R3/00 , F23R3/12 , F23R3/42
CPC分类号： F23R3/002 , F23M20/005 , F23R2900/00014
摘要： A gas turbine combustor includes a combustion liner in which a combustion region is formed; and a housing provided for a wall of the combustion liner in a predetermined circumferential region of the combustion liner to form a resonance space between the combustion liner and the housing. The combustion region and the resonance space are connected by a plurality of combustion liner through-holes, and a circumferential length of the housing is longer than a diameter of the combustion liner.
摘要翻译：燃气轮机燃烧器包括其中形成有燃烧区域的燃烧衬套; 以及壳体，其设置在所述燃烧衬套的预定圆周区域中的所述燃烧衬套的壁上，以在所述燃烧衬套和所述壳体之间形成共振空间。燃烧区域和共振空间通过多个燃烧衬套通孔连接，壳体的圆周长度大于燃烧衬套的直径。

10. 发明授权

US6094150A System and method of measuring noise of mobile body using a plurality microphones 失效
标题翻译：使用多个麦克风测量移动体噪声的系统和方法
公开(公告)号：US6094150A
公开(公告)日：2000-07-25
申请号：US129945
申请日：1998-08-06
申请人： Keizo Ohnishi , Kazufumi Ikeda , Tetsuya Nagao
发明人： Keizo Ohnishi , Kazufumi Ikeda , Tetsuya Nagao
IPC分类号： G01H3/00 , G01H3/12 , B60Q5/00
CPC分类号： G01H3/125
摘要： In a noise measuring system comprising a microphone array and a directivity forming section for controlling the direction of directivity of the microphone array, the directivity forming section includes delay section and adding section, and the optimal value of a delay time of the delay section is set in such a manner that a noise isolation characteristic for causing any mobile noise generator not targeted for noise measurement to come off a directional plane or a directional line formed in the direction of directivity of the microphone array and a deterioration characteristic of the directivity of the microphone array balance with each other.
摘要翻译：在包括麦克风阵列和用于控制麦克风阵列的方向性方向的方向性形成部分的噪声测量系统中，方向性形成部分包括延迟部分和相加部分，并且设置延迟部分的延迟时间的最佳值以这样的方式，使得用于使得没有针对噪声测量的任何移动噪声发生器脱离在麦克风阵列的方向性方向上形成的方向平面或方向线的噪声隔离特性以及麦克风的方向性的劣化特性阵列相互平衡。

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