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1. 发明申请

US20130055697A1 FLUID COMPOSITION ANALYSIS MECHANISM, CALORIFIC VALUE MEASUREMENT DEVICE AND POWER PLANT 审中-公开
标题翻译：流体成分分析机制，计量值测量装置和发电厂
公开(公告)号：US20130055697A1
公开(公告)日：2013-03-07
申请号：US13482565
申请日：2012-05-29
申请人： Yoshihiro Deguchi , Yosuke Kitauchi , Mitsuru Inada
发明人： Yoshihiro Deguchi , Yosuke Kitauchi , Mitsuru Inada
IPC分类号： G01K17/00 , F02C9/00 , G01J3/44
CPC分类号： G01N21/65 , G01N21/85
摘要： A fluid composition analysis mechanism includes a light source for configured to irradiate excitation light to a sample fluid at a measurement position; a light receiving unit arranged on an extended line of the excitation light for configured to receive and disperse Raman scattering light generated from the sample fluid irradiated with the excitation light; a Raman scattering light collection optical system arranged on an optical path for the excitation light or on the extended line of the excitation light configured to collect the Raman scattering light generated at the measurement position and to cause the condensed Raman scattering light to be incident on the light receiving unit; a calculation unit configured to calculate a composition of the sample fluid based on an output of the light receiving unit; and a light shielding member arranged on the optical path or on the extended line of the excitation light.
摘要翻译：流体组成分析机构包括：光源，用于将测量位置处的激发光照射到样品流体; 配置在所述激发光的延长线上的光接收单元，用于接收和分散由激发光照射的样品流体产生的拉曼散射光; 布置在用于激发光的光路上的激光的延伸线上的拉曼散射光收集光学系统，其被配置为收集在测量位置处产生的拉曼散射光，并使聚光的拉曼散射光入射到光接收单元; 计算单元，被配置为基于所述光接收单元的输出来计算所述样本流体的组成; 以及设置在激发光的光路或延伸线上的遮光部件。

2. 发明授权

US6164075A Steam cooling type gas turbine combustor 有权
标题翻译：蒸汽冷却式燃气轮机燃烧器
公开(公告)号：US6164075A
公开(公告)日：2000-12-26
申请号：US155937
申请日：1999-04-29
申请人： Kiryo Igarashi , Akio Ogose , Kouichi Akagi , Mitsuru Inada
发明人： Kiryo Igarashi , Akio Ogose , Kouichi Akagi , Mitsuru Inada
IPC分类号： F02C7/141 , F02C7/18 , F23M5/08 , F23R3/00 , F23R3/42
CPC分类号： F23R3/005 , F05B2260/205 , F05B2260/233
摘要： This invention concerns the use of pressurized steam as the cooling medium in the combustor wall of a gas turbine combustor. It is distinguished by the following. The combustor wall is configured by 1) a plurality of cooling channels for cooling steam, sealed by an exterior wall panel and a heat-resistant plate which are assembled by soldering or some other method; 2) a supply manifold for supplying the cooling steam into the cooling channels, which is provided on one end of the cooling channels; and 3) a recovery manifold for recovering the cooling steam from the cooling channels, which is provided on another end of the cooling channels. This arrangement can form strong enough steam-channels that do not allow any leakage of the high pressure steam from the cooling system.
摘要翻译： PCT No.PCT / JP98 / 00552 Sec。 371日期1999年4月29日第 102（e）日期1999年4月29日PCT提交1998年2月12日PCT公布。公开号WO98 / 36220 PCT 日期1998年8月20日本发明涉及使用加压蒸汽作为燃气轮机燃烧器的燃烧器壁中的冷却介质。它的区别在于以下内容。燃烧室壁由1个冷却通道构成，冷却通道用于通过焊接或其它方法组装的外壁板和耐热板进行密封; 2）供应歧管，用于将冷却蒸汽供应到设置在冷却通道一端的冷却通道中; 以及3）回收歧管，用于从冷却通道的冷却通道的另一端回收冷却蒸汽。这种布置可以形成足够强的蒸汽通道，其不允许来自冷却系统的高压蒸汽的任何泄漏。

3. 发明授权

US06209326B1 Gas turbine combustor 失效
标题翻译：燃气轮机燃烧器
公开(公告)号：US06209326B1
公开(公告)日：2001-04-03
申请号：US09244030
申请日：1999-02-04
申请人： Shigemi Mandai , Koichi Nishida , Masataka Ota , Tatsuo Ishiguro , Mitsuru Inada , Hideki Haruta
发明人： Shigemi Mandai , Koichi Nishida , Masataka Ota , Tatsuo Ishiguro , Mitsuru Inada , Hideki Haruta
IPC分类号： F02C100
CPC分类号： F23R3/286 , F23C7/004 , F23D14/02 , F23D2205/00 , F23D2206/10 , F23D2900/14021
摘要： To prepare a more homogeneous premixture than that of the device of the prior art thereby to suppress an NOx emission and to lower a fuel feed pressure. A gas turbine combustor comprising: an outer cylinder 106 having main swirlers 101 therein and adapted to be fed with air; and an annular fuel feed manifold 110 disposed at the outer circumference of the outer cylinder 106 on the upstream or downstream side of the main swirlers 101 and having a plurality of nozzle ports 111 communicating with the inside of the outer cylinder 106, so that a fuel is injected from the outer circumference to the center of the air flowing in the outer cylinder 106.
摘要翻译：为了制备比现有技术的装置更均匀的预混合物，从而抑制NOx排放并降低燃料供给压力.1。一种燃气轮机燃烧器，包括：外筒106，其中具有主旋流器101，并适于供给空气; 以及环形燃料供给歧管110，其设置在主旋流器101的上游侧或下游侧的外筒106的外周，并具有与外筒106的内部连通的多个喷嘴口111，从外圆周喷射到在外筒106中流动的空气的中心。

4. 发明授权

US06173561B1 Steam cooling method for gas turbine combustor and apparatus therefor 有权
标题翻译：燃气轮机燃烧器的蒸汽冷却方法及其设备
公开(公告)号：US06173561B1
公开(公告)日：2001-01-16
申请号：US09155938
申请日：1999-04-29
申请人： Minoru Sato , Yuichi Kobayashi , Kouichi Akagi , Mitsuru Inada
发明人： Minoru Sato , Yuichi Kobayashi , Kouichi Akagi , Mitsuru Inada
IPC分类号： F23R342
CPC分类号： F02C7/18 , F05D2260/205 , F05D2260/2322 , F23R3/005
摘要： This invention concerns the use of pressurized steam as the cooling medium for a gas turbine combustor. It is distinguished by the following. Steam supply manifolds or ports for the cooling steam are provided on the gas inlet and outlet sides of the combustion chamber in the gas turbine combustor. A steam exhaust manifold or port for the cooling steam is provided between the gas inlet and outlet sides, in approximately the center of the chamber. Cooling channels for the steam are created in the external wall panel of the chamber between the steam supply manifolds and the exhaust manifold. The steam supplied into the wall panel through the steam supply manifolds on the gas inlet and outlet sides of the chamber is exhausted to the exterior via the steam exhaust manifold in the center of the chamber. This design allows pressurized steam with a high thermal capacity to be used to effectively cool the wall panels of the combustor, which are exposed to extremely hot combustion gases.
摘要翻译：本发明涉及使用加压蒸汽作为燃气轮机燃烧器的冷却介质。它的区别在于以下内容。用于冷却蒸汽的蒸汽供应歧管或端口设置在燃气轮机燃烧器中的燃烧室的气体入口侧和出口侧。用于冷却蒸汽的蒸汽排气歧管或端口设置在气体入口侧和出口侧之间，大致在室的中心。蒸汽的冷却通道在蒸汽供应歧管和排气歧管之间的室的外壁板中产生。通过腔室的气体入口和出口侧的蒸汽供应歧管向壁板供应的蒸汽通过腔室中心的蒸汽排气歧管排放到外部。这种设计允许具有高热容量的加压蒸汽用于有效地冷却暴露于极热燃烧气体的燃烧器的壁板。

5. 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.

6. 发明授权

US6068467A Combustor 有权
标题翻译：燃烧器
公开(公告)号：US6068467A
公开(公告)日：2000-05-30
申请号：US244031
申请日：1999-02-04
申请人： Shigemi Mandai , Koichi Nishida , Masataka Ota , Satoshi Tanimura , Kotaro Miyauchi , Mitsuru Inada , Shinji Akamatsu , Hideki Haruta
发明人： Shigemi Mandai , Koichi Nishida , Masataka Ota , Satoshi Tanimura , Kotaro Miyauchi , Mitsuru Inada , Shinji Akamatsu , Hideki Haruta
IPC分类号： F23D14/02 , F23D23/00 , F23C5/00
CPC分类号： F23D23/00 , F23D14/02 , F23D2206/10 , F23D2209/10 , F23D2900/14021
摘要： A combustor has a pilot nozzle 02 arranged at a central portion of an inner cylinder 01 opening at its end into a combustion chamber 018 and includes a plurality of main nozzles 03 arranged around its outer circumference. Along the outer circumference of a flame holding cone 014 for igniting a fuel F injected from the main nozzles 03 there are disposed elliptical extension pipes 016 of an elliptical sectional shape which are extended from the fronts of the main nozzles 03 to have openings at the axial position of the opening of the flame holding cone 014. As a result, a hot premixed flame 013 does not flow back to a main swirler zone 015 of the circumferential edges of the openings of the main nozzles 03 so that mixing between the fuel F and an air flow A can be improved, reducing the Nox emission while eliminating the burning of a base plate 04 and the main nozzles 03.
摘要翻译：燃烧器具有引导喷嘴02，其设置在内筒01的中心部分处，内筒01在其端部处开放到燃烧室018中，并且包括围绕其外圆周布置的多个主喷嘴03。沿着用于点燃从主喷嘴03喷射的燃料F的火焰保持锥体014的外圆周，设置椭圆形截面形状的椭圆形延伸管016，其从主喷嘴03的前面延伸，以在轴向上具有开口火焰保持锥体014的开口的位置。结果，热预混火焰013不流回到主喷嘴03的开口的周缘的主旋流器区域015，使得燃料F和可以改善空气流A，减少Nox排放，同时消除基板04和主喷嘴03的燃烧。

7. 发明授权

US06047551A Multi-nozzle combustor 失效
标题翻译：多喷嘴燃烧器
公开(公告)号：US06047551A
公开(公告)日：2000-04-11
申请号：US35504
申请日：1998-03-05
申请人： Tatsuo Ishiguro , Shigemi Mandai , Mitsuru Inada , Satoshi Tanimura , Kouichi Nishida
发明人： Tatsuo Ishiguro , Shigemi Mandai , Mitsuru Inada , Satoshi Tanimura , Kouichi Nishida
IPC分类号： F23R3/20 , F23C99/00 , F23D11/12 , F23R3/28 , F23R3/34 , F02C7/22
CPC分类号： F23R3/286
摘要： A multi-nozzle combustor comprising a pilot nozzle for flame retention and a plurality of main nozzles arranged around the pilot nozzle, each of the nozzles including an outer cylinder, an inner cylinder, and an annular passage defined between the outer and inner cylinders and forming therein a mixture-evaporation region for a fuel ejected and atomized by an airflow.
摘要翻译：一种多喷嘴燃烧器，包括用于火焰保持的先导喷嘴和围绕引燃喷嘴布置的多个主喷嘴，每个喷嘴包括外筒，内筒和限定在外筒和内筒之间的环形通道，并形成其中用于通过气流喷射和雾化的燃料的混合物蒸发区域。

8. 发明授权

US06502399B2 Three-dimensional swirler in a gas turbine combustor 有权
标题翻译：燃气轮机燃烧器中的三维旋流器
公开(公告)号：US06502399B2
公开(公告)日：2003-01-07
申请号：US09794134
申请日：2001-02-28
申请人： Shigemi Mandai , Masataka Ohta , Mitsuru Inada , Shinji Akamatsu
发明人： Shigemi Mandai , Masataka Ohta , Mitsuru Inada , Shinji Akamatsu
IPC分类号： F23R314
CPC分类号： F23R3/14
摘要： A pre-mixture forming swirler in a gas turbine pre-mixed flame type low NOx combustor is improved so as to accelerate mixing of fuel and air and to prevent the occurrence of flame stagnation and burning of components. In particular, a three-dimensional swirler is constructed such that each swirler vane is twisted from a hub side thereof to a tip side so that a fitting angle of the tip side relative to a center axis of a fuel nozzle is larger than an angle of the hub side. Thereby, while the angle of the hub side is set smaller so that flame stagnation and burning of components resulted therefrom may be prevented from occurring, the angle of the tip side may be selected so that the shearing flow necessary for appropriate mixing of fuel and air is obtained. Thus, favorable pre-mixing is achieved, life deterioration due to burning, etc., is prevented and combustion efficiency is enhanced.
摘要翻译：在燃气轮机预混合火焰型低NOx燃烧器中形成旋流器的预混合物得到改善，以加速燃料和空气的混合，并防止部件火焰停滞和燃烧。特别地，三维旋流器被构造成使得每个旋流器叶片从其轮毂侧扭转到尖端侧，使得尖端侧相对于燃料喷嘴的中心轴线的配合角度大于集线器侧。由此，在将轮毂侧的角度设定得较小的同时，能够防止由此引起的部件产生火焰停滞和燃烧的情况下，可以选择前端侧的角度，使得适当地混合燃料和空气所需的剪切流获得。因此，可以实现良好的预混合，防止燃烧等引起的寿命劣化，提高燃烧效率。

9. 发明授权

US06220036B1 Cooling structure for combustor tail pipes 有权
标题翻译：燃烧器尾管的冷却结构
公开(公告)号：US06220036B1
公开(公告)日：2001-04-24
申请号：US09194016
申请日：1998-11-19
申请人： Mitsuru Inada , Kouichi Akagi , Jun Kubota , Koji Watanabe , Yoshichika Sato
发明人： Mitsuru Inada , Kouichi Akagi , Jun Kubota , Koji Watanabe , Yoshichika Sato
IPC分类号： F02C330
CPC分类号： F23R3/005 , F01D9/023 , F01D25/26 , F05D2230/642 , F05D2260/2322 , Y02E20/16 , Y02T50/676
摘要： Gas turbine combustor tail tube cooling structure is improved so that temperature distribution along tail tube axial direction is made gentle and large thermal stress is prevented from occurring resulting in enhancement of safety and reliability of the combustor tail tube. Supply jacket (16) is disposed between upstream side discharge jacket (14) and downstream side discharge jacket (15). The upstream side discharge jacket (14) is disposed apart from tail tube inlet (2) at position close to by-pass passage (10) so as to form non-cooled zone (A) in the vicinity of the tail tube inlet (2). On the downstream side thereof, the supply jacket (16) is disposed at position in tail tube (1) contracting portion and near the downstream side discharge jacket (15) so as to shorten length of cooling pipes there.
摘要翻译：改善了燃气轮机燃烧器尾管冷却结构，使得沿着尾管轴向的温度分布变得平缓，并且防止发生大的热应力，从而提高了燃烧器尾管的安全性和可靠性。电源护套（16）设置在上游侧放电护套（14）和下游侧放电护套（15）之间。上游侧排气套（14）在靠近旁路通道（10）的位置处与尾管入口（2）分开设置，以在尾管入口（2）附近形成非冷却区域（A））。在其下游侧，供气套（16）设置在尾管（1）收缩部分中并位于下游侧排放套（15）附近，以缩短冷却管的长度。

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