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1. 发明授权

US07694521B2 Installation structure of pilot nozzle of combustor 有权
标题翻译：燃烧器引燃喷嘴安装结构
公开(公告)号：US07694521B2
公开(公告)日：2010-04-13
申请号：US10561927
申请日：2004-03-03
申请人： Masataka Ohta , Shigemi Mandai , Kuniaki Aoyama , Katsunori Tanaka , Shinji Akamatsu , Hisanari Nakajima , Teruya Tachibana , Koichi Nishida , Wataru Akizuki , Yoshikuni Kasai , Jyunji Hashimura
发明人： Masataka Ohta , Shigemi Mandai , Kuniaki Aoyama , Katsunori Tanaka , Shinji Akamatsu , Hisanari Nakajima , Teruya Tachibana , Koichi Nishida , Wataru Akizuki , Yoshikuni Kasai , Jyunji Hashimura
IPC分类号： F02C1/00
CPC分类号： F23R3/343 , F23D2900/00015 , F23R3/286
摘要： Pilot fuel injected from fuel injection ports 21 of a pilot nozzle 2 bumps against an inner wall surface of a tapered portion of an inner circumference of a cone 41 of a pilot cone 4. At this time, the position where a pilot fuel from the fuel injection ports 21 hits is located in a range from a middle of the tapered portion of the inner circumference of a cone 41 to a downstream-side tip thereof.
摘要翻译：从先导喷嘴2的燃料喷射口21喷射的先导燃料抵靠导向锥4的锥体41的内周的锥形部的内壁面。此时，来自燃料的导向燃料的位置喷射口21打击位于从锥体41的内圆周的锥形部分的中部到其下游侧的顶端的范围内。

2. 发明申请

US20070006587A1 Combustor 有权
标题翻译：燃烧器
公开(公告)号：US20070006587A1
公开(公告)日：2007-01-11
申请号：US10561927
申请日：2004-03-03
申请人： Masataka Ohta , Shigemi Mandai , Kuniaki Aoyama , Katsunori Tanaka , Shinji Akamatsu , Hisanari Nakajima , Teruya Tachibana , Koichi Nishida , Wataru Akizuki , Yoshikumi Kasai , Jyunji Hashimura
发明人： Masataka Ohta , Shigemi Mandai , Kuniaki Aoyama , Katsunori Tanaka , Shinji Akamatsu , Hisanari Nakajima , Teruya Tachibana , Koichi Nishida , Wataru Akizuki , Yoshikumi Kasai , Jyunji Hashimura
IPC分类号： F23R3/30
CPC分类号： F23R3/343 , F23D2900/00015 , F23R3/286
摘要： Pilot fuel being injected from fuel injection ports 21 of a pilot nozzle 2 bumps against an inner wall surface of the tapered portion of the inner circumference of a cone 41 of a pilot cone 4. At this time, the position where the pilot fuel from the fuel injection ports 21 hits is located in the range from the middle of the tapered portion of the inner circumference of a cone 41 to the downstream-side tip thereof.
摘要翻译：先导喷嘴2的燃料喷射口21喷射的先导燃料抵靠导向锥4的锥体41的内周的锥形部的内壁面。此时，来自燃料喷射口21的先导燃料的位置位于从锥体41的内周的锥形部的中部到下游侧的前端的范围内。

3. 发明授权

US06668557B2 Pilot nozzle of gas turbine combustor 失效
公开(公告)号：US06668557B2
公开(公告)日：2003-12-30
申请号：US10200165
申请日：2002-07-23
申请人： Masataka Ohta , Kuniaki Aoyama , Mitsuru Inada , Shigemi Mandai , Satoshi Tanimura , Katsunori Tanaka , Koichi Nishida
发明人： Masataka Ohta , Kuniaki Aoyama , Mitsuru Inada , Shigemi Mandai , Satoshi Tanimura , Katsunori Tanaka , Koichi Nishida
IPC分类号： F02C7264
CPC分类号： F23R3/20 , F23R3/343
摘要： A pilot nozzle of a gas turbine combustor comprises a first structure, provided near a main nozzle of a combustor that injects fuel oil, having a flow channel for a fuel gas and an outlet for the fuel gas. The first structure diffusion-injecting the fuel gas obliquely forward through the outlet to maintain a flame and to aid ignition of the fuel oil injected from the main nozzle. There is further provided a second structure which circulates in whirls a combustion gas generated due to the combustion of the fuel gas.

4. 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.

5. 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。

6. 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。

7. 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。

8. 发明授权

US06931854B2 Combustor containing fuel nozzle 有权
标题翻译：含燃料喷嘴的燃烧器
公开(公告)号：US06931854B2
公开(公告)日：2005-08-23
申请号：US10287507
申请日：2002-11-05
申请人： Keijirou Saitoh , Takashi Kawano , Hidemi Niinai , Yutaka Kawata , Shigemi Mandai , Kuniaki Aoyama
发明人： Keijirou Saitoh , Takashi Kawano , Hidemi Niinai , Yutaka Kawata , Shigemi Mandai , Kuniaki Aoyama
IPC分类号： F23D14/02 , F23D14/58 , F23R3/28 , F02C1/00 , F02G3/00
CPC分类号： F23R3/286 , F23D2210/00 , F23D2900/14004 , F23R2900/00014
摘要： There is provided a combustor comprising a fuel nozzle which is comprised of a rodlike body which has a fuel passage and which is located in an air passage; a plurality of hollow members which are connected to the fuel passage and which extend in radial directions from the rodlike body into the air passage; at least one injection port formed in each hollow member to inject a fuel from the fuel passage into the air passage; and a projection which extends from a farmost inner wall of each hollow member that is most distant from an axis of the rodlike body to the injection port that is most distant from the axis. A hole for leaking fuel that is connected to an air passage may be formed in a farmost inner wall of the hollow member that is more distant from an axis of a rodlike body than the injection port that is most distant from the axis, or may be formed to be adjacent to all the injection ports on an upstream or downstream side in the direction of the airflow. Thus, a vortex does not occur in the hollow column.
摘要翻译：提供了一种燃烧器，其包括燃料喷嘴，该燃料喷嘴由具有燃料通道并且位于空气通道中的杆状体构成; 多个中空构件，其连接到燃料通道并且在径向方向上从杆状体延伸到空气通道中; 形成在每个中空构件中的至少一个喷射口，用于将来自燃料通道的燃料喷射到空气通道中; 以及从最远离杆状体的轴线到最远离轴线的喷射口的每个中空构件的农田内壁延伸的突起。连接到空气通道的用于泄漏燃料的孔可以形成在中空构件的农田内壁中，该中空构件的远离轴线的轴线比距离轴线最远的喷射口更远离杆状体的轴线，或者可以是形成为与气流方向上游侧或下游侧的所有喷射口相邻。因此，在中空塔中不会发生涡流。

9. 发明授权

US08312703B2 Solar-thermal gas turbine generator 失效
标题翻译：太阳能燃气轮机发电机
公开(公告)号：US08312703B2
公开(公告)日：2012-11-20
申请号：US13123777
申请日：2010-06-04
申请人： Kuniaki Aoyama , Kei Inoue , Kazuta Kobayashi , Masashi Tagawa , Toshiyuki Osada , Manabu Maeda
发明人： Kuniaki Aoyama , Kei Inoue , Kazuta Kobayashi , Masashi Tagawa , Toshiyuki Osada , Manabu Maeda
IPC分类号： F02C6/00
CPC分类号： F02C6/18 , F01K23/10 , F02C1/05 , F03G6/064 , F03G6/067 , Y02E10/46 , Y02E20/16
摘要： A solar-thermal gas turbine generator is equipped with a compressor, a heat receiver, and a turbine. Additionally, there is a generator that is driven by the solar-thermal gas turbine to generate power; and a steam power generation cycle in which high-temperature air exhausted from the turbine is introduced into a steam generator and in which a steam turbine that is operated with steam generated at the steam generator drives a generator to generator power, wherein a solar-thermal steam generator that generates steam by being heated with heat collected by the light collector is provided upstream of the steam turbine of the steam power generation cycle, and a distribution ratio for distributing the sunlight collected by the light collector to the heat receiver and the solar-thermal steam generator is adjusted in accordance with the sunlight intensity.
摘要翻译：太阳能热燃气涡轮发电机配备有压缩机，热接收器和涡轮机。另外，还有一台发电机由太阳热能燃气轮机驱动，以发电; 以及蒸汽发电循环，其中从涡轮机排出的高温空气被引入到蒸汽发生器中，其中在蒸汽发生器处产生的蒸汽操作的蒸汽涡轮驱动发电机发电机功率，其中太阳能热在蒸汽发电循环的蒸汽涡轮机的上游设置有通过被集光器收集的热量加热而产生蒸汽的蒸汽发生器，并且将由集光器收集的太阳光分配到热接收器和太阳能发电装置的分配比例，热蒸汽发生器根据阳光强度进行调整。

10. 发明授权

US08069673B2 Seal structure for gas turbine combustor 有权
标题翻译：燃气轮机燃烧室密封结构
公开(公告)号：US08069673B2
公开(公告)日：2011-12-06
申请号：US12767055
申请日：2010-04-26
申请人： Nobuhiro Kunitake , Kuniaki Aoyama , Kiyoshi Fujimoto , Masaharu Minami
发明人： Nobuhiro Kunitake , Kuniaki Aoyama , Kiyoshi Fujimoto , Masaharu Minami
IPC分类号： F02C7/20
CPC分类号： F16J15/0887 , F01D9/023 , F01D11/005 , F02C7/28 , F05D2240/57
摘要： Provided is a seal structure, according to the present invention, for sealing opposite surfaces of flanges between adjacent tail ducts, which can be prevented from being worn or aged deteriorated due to a thermal deformation in a high temperature atmosphere or vibration of a gas turbine combustor, and which can maintain a satisfactory sealing function for a long time. The seal structure is characterized in that recess grooves are formed in opposed surfaces of adjacent flanges at the outlet end of tail ducts, striding between the opposed surfaces, a seal assembly composed of a seal member and a leaf spring is inserted in the recess grooves, the seal member has a pair of continuous beads which are arranged facing the inner surfaces, on the combustion gas passage side, of the recess grooves, striding between the opposed surfaces of the flanges within the recess grooves, the leaf spring is arranged so as to be contact with the seal member within the recess grooves so that the beads are pressed against the surfaces on the combustion gas passage side by the resilient force of the leaf spring so as to create seal surfaces.
摘要翻译：根据本发明，提供一种用于密封相邻尾管之间的法兰相对表面的密封结构，其可以防止由于高温气氛中的热变形或燃气轮机燃烧器的振动而被磨损或老化而劣化，长时间保持良好的密封功能。密封结构的特征在于，在尾管的出口端的相邻凸缘的相对的表面上形成凹槽，跨过相对的表面之间，由密封件和片簧组成的密封组件插入凹槽中，所述密封构件具有一对连续的珠，所述一对连续的珠子相对于所述凹槽的燃烧气体通道侧的内表面布置，跨越所述凹槽内的所述凸缘的相对的表面之间，所述板簧布置成与凹槽内的密封构件接触，使得珠被片簧的弹力压靠在燃烧气体通路侧的表面上，从而形成密封面。

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