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公开(公告)号：US4429538A
公开(公告)日：1984-02-07
申请号：US234015
申请日：1981-02-12
申请人： Isao Sato , Yohji Ishibashi , Yoshimitsu Minakawa , Takashi Ohmori , Zensuke Tamura , Yoshihiro Uchiyama , Ryoichiro Ohshima
发明人： Isao Sato , Yohji Ishibashi , Yoshimitsu Minakawa , Takashi Ohmori , Zensuke Tamura , Yoshihiro Uchiyama , Ryoichiro Ohshima
摘要： A gas turbine combustor comprising a combustor inner-pipe for forming a head combustion chamber and a rear combustion chamber having a diameter larger than a diameter of head combustion chamber. A combustor outer-pipe covers the combustor inner-pipe, and a fuel nozzle is disposed at an end part of the head combustion chamber for supplying fuel to said combustor inner pipe. A first group of ports are arranged for swirling and feeding air in an axial direction of the combustor inner-pipe. The first group of ports are around the fuel nozzle. A second group of ports for swirling and feeding air in a radial direction of said combustor inner-pipe are disposed in a side wall of the head combustion chamber near the fuel nozzle. A third group of ports for swirling and feeding air in a radial direction of the combustion inner-pipe and a fourth group of ports for feeding air in a radial direction of the combustor inner-pipe are provided and ar both disposed in a side wall of the head combustion chamber near the said rear combustion chamber. A fifth group of ports are disposed in a side wall of the rear combustion chamber near the head combustion chamber and a sixth group of ports are disposed in a side wall of the rear combustion chamber on a downstream side of the fifth group of ports. Another group of ports for swirling and feeding air into the head combustion chamber are disposed in a vicinity of a central portion of an end part of the head combustion chamber along an inner periphery of the fuel nozzle, with this group of ports and the first group of ports being constructed so that air flowing from both groups of ports has the same swirling direction.
摘要翻译： 一种燃气轮机燃烧器，包括用于形成头部燃烧室的燃烧器内管和具有大于头部燃烧室直径的直径的后燃烧室。 燃烧器外管覆盖燃烧器内管，并且燃料喷嘴设置在头部燃烧室的端部，用于向燃烧器内管供应燃料。 第一组端口布置成在燃烧器内管的轴向上旋转和进给空气。 第一组港口在燃油喷嘴周围。 用于在所述燃烧器内管的径向方向上旋转和进给空气的第二组端口设置在靠近燃料喷嘴的头部燃烧室的侧壁中。 设置有用于在燃烧内管的径向上旋转和进给空气的第三组端口和用于沿着燃烧器内管的径向供给空气的第四组端口，并且ar设置在 靠近所述后燃烧室的头部燃烧室。 第五组端口设置在靠近头部燃烧室的后燃烧室的侧壁中，并且第六组端口设置在第五组端口的下游侧的后燃烧室的侧壁中。 用于将空气旋转并进入头部燃烧室的另一组端口沿着燃料喷嘴的内周设置在头部燃烧室的端部的中心部分的附近，该组端口和第一组 的端口被构造成使得从两组端口流出的空气具有相同的旋转方向。
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公开(公告)号：US4671069A
公开(公告)日：1987-06-09
申请号：US809200
申请日：1985-12-16
申请人： Isao Sato , Yoji Ishibashi , Zensuke Tamura , Takashi Ohmori , Yoshimitsu Minakawa , Hidekazu Fujimura , Yoshihiro Uchiyama
发明人： Isao Sato , Yoji Ishibashi , Zensuke Tamura , Takashi Ohmori , Yoshimitsu Minakawa , Hidekazu Fujimura , Yoshihiro Uchiyama
CPC分类号： F23R3/286 , F23R3/346 , Y02E20/344
摘要： A premixture of compressed air and gaseous fuel is supplied and conbusted into a head combustion chamber of a combustor for gas turbine and main combustion of lean, low flame temperature is carried out in a rear combustion chamber following the heat combustion chamber to prevent the formation of high flame temperature which tends to promote NOx generation.
摘要翻译： 供给压缩空气和气态燃料的预混合物，并将其燃烧到用于燃气轮机的燃烧器的燃烧器的头部燃烧室中，并且在燃烧室的后部燃烧室中执行低燃点的主燃烧，以防止形成 易产生NOx的高火焰温度。
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公开(公告)号：US4587809A
公开(公告)日：1986-05-13
申请号：US677244
申请日：1984-12-03
申请人： Takashi Ohmori , Isao Sato , Yoji Ishibashi , Yoshimitsu Minakawa , Michio Kuroda , Zensuke Tamura
发明人： Takashi Ohmori , Isao Sato , Yoji Ishibashi , Yoshimitsu Minakawa , Michio Kuroda , Zensuke Tamura
IPC分类号： F23D14/02 , B01F5/04 , F23C6/04 , F23C15/00 , F23C99/00 , F23D14/62 , F23D14/82 , F23R3/34 , F02C1/00 , F02G3/00
摘要： A premixing swirling burner including a burner body having a swirling member at one end for causing fuel introduced into the burner body to flow in vortical form through the swirling member, a burner outer frame mounting the burner body and communicated with an air line for introducing air into the burner body, and a cylindrical member located in the burner outer frame for enclosing the burner body, with an air passage being defined between the inner periphery of the cylindrical member and an outer periphery of a portion of the burner body. A premixing chamber is defined between an outer periphery of a central portion of the burner body and an inner periphery of the cylindrical member for providing a fuel-air premix flowing toward the swirling member. A fuel chamber introduces fuel into the interior of the burner body, and a fuel ejection nozzle is located along an outer surface of the central portion of the burner body. A channel defined between the inner periphery of an end portion of the cylindrical member and an outer peripheral portion of the burner body formed an inlet for the premixing chamber has a cross-sectional area smaller than a cross-sectional area of the air passage.
摘要翻译： 一种预混合旋转燃烧器，包括一端具有旋转构件的燃烧器主体，用于使引入燃烧器本体的燃料通过旋转构件以涡卷形式流动;燃烧器外框架，其安装燃烧器主体并与用于引入空气的空气管路连通 和位于燃烧器外框架中的圆筒形构件，用于封闭燃烧器主体，空气通道限定在圆柱形构件的内周和燃烧器本体的一部分外周之间。 在燃烧器主体的中心部分的外周和圆柱形部件的内周之间限定预混合室，用于提供朝向旋转部件流动的燃料 - 空气预混物。 燃料室将燃料引入燃烧器本体的内部，并且燃料喷射嘴位于燃烧器本体的中心部分的外表面。 形成在圆筒形构件的端部的内周和形成为预混合室的入口的燃烧器主体的外周部之间的通道的横截面积小于空气通道的横截面面积。
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公开(公告)号：US4898001A
公开(公告)日：1990-02-06
申请号：US144646
申请日：1988-01-11
申请人： Michio Kuroda , Isao Sato , Yoji Ishibashi , Yoshihiro Uchiyama , Takashi Ohmori , Shigeyuki Akatsu , Fumio Kato , Yorihide Segawa , Nobuyuki Iizuka
发明人： Michio Kuroda , Isao Sato , Yoji Ishibashi , Yoshihiro Uchiyama , Takashi Ohmori , Shigeyuki Akatsu , Fumio Kato , Yorihide Segawa , Nobuyuki Iizuka
摘要： A gas turbine combustor for reducing a production of NOx. The combustor includes a head combustion chamber and a rear combustion chamber which is larger in diameter than the head combustion chamber. The head combustion chamber is provided with an axially extending hollow frustoconical tubular member to form an annular combustion space therein, air holes for axially jetting air into the annular combustion chamber, air holes formed on a peripheral wall for injecting air and a plurality of fuel nozzles projected into the annular combustion space for injecting fuel into vortex formed by the air jet and the injected air flow whereby the flame is stabilized and lean combustion can be effected. The rear combustion chamber has a fuel and air supply means on the upstream side which includes air inlets formed by whirling vanes and fuel nozzles disposed in the air inlets so that fuel and air are mixed well. The fuel and air mixture is jetted substantially axially while whirling it so that formation of hot spots is avoided and the NOx formation is extremely limited.
摘要翻译： 一种用于减少NOx生产的燃气轮机燃烧器。 燃烧器包括头部燃烧室和直径大于头部燃烧室的后部燃烧室。 头部燃烧室设置有轴向延伸的中空截头圆锥形管状构件以在其中形成环形燃烧空间，用于将空气轴向地喷射到环形燃烧室中的气孔，形成在用于喷射空气的周壁上的气孔和多个燃料喷嘴 投射到环形燃烧空间中，用于将燃料喷射到由空气射流和喷射空气流形成的涡流中，从而使火焰稳定并且可以实现贫燃。 后燃烧室在上游侧具有燃料和空气供给装置，其包括由旋转叶片形成的空气入口和设置在空气入口中的燃料喷嘴，使得燃料和空气充分混合。 燃料和空气混合物在旋转时基本上轴向地喷射，从而避免形成热点并且非常限制NOx的形成。
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公开(公告)号：US4598553A
公开(公告)日：1986-07-08
申请号：US375582
申请日：1982-05-06
摘要： A gas turbine combustor comprises an inner cylinder provided with louvers in an outer periphery thereof, defines a head combustion chamber and a main combustion chamber located downstream of and greater in diameter than the head combustion. An outer cylinder surrounds the inner cylinder and defines an air passage therebetween. A first burner communicates with the head combustion chamber and supplies air with gaseous fuel, and a second burner being disposed in the air passage near the head combustion chamber and supplying air and gaseous fuel into the main combustion chamber. The second burner is formed with a plurality of air inlets by a plurality of vanes which are disposed in an annular passage and which swirl the air, and with gaseous fuel jet ports near the inner peripheries of the air inlets. When the flow rate of the supplied fuel is small, the fuel flows along an inner-peripheral surface of the second burner, and when the flow rate is large, the fuel from the air inlets moves from the inner-peripheral surface toward the outer-peripheral surface of the second burner so as to be mixed well with the air supplied into the main combustion chamber. Thus, the production of NO.sub.x, CO, HC etc. can be decreased over the whole operating range of the turbine.
摘要翻译： 燃气轮机燃烧器包括在其外周设置有百叶窗的内筒，限定头部燃烧室和主燃烧室，该主燃烧室和主燃烧室位于头部燃烧的直径以下。 外筒围绕内筒并在其间形成空气通道。 第一燃烧器与头部燃烧室连通并且向空气供应气体燃料，第二燃烧器设置在靠近头部燃烧室的空气通道中并将空气和气体燃料供应到主燃烧室中。 第二燃烧器由多个叶片形成有多个空气入口，多个叶片设置在环形通道中并使空气旋转，并且在空气入口的内周边附近具有气体燃料喷射口。 当供给的燃料的流量小时，燃料沿着第二燃烧器的内周面流动，并且当流量大时，来自空气入口的燃料从内周面朝向外侧面移动， 第二燃烧器的周面，以便与供给主燃烧室的空气充分混合。 因此，可以在涡轮机的整个工作范围内降低NOx，CO，HC等的生产。
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公开(公告)号：US5069029A
公开(公告)日：1991-12-03
申请号：US563191
申请日：1990-08-06
申请人： Michio Kuroda , Seiichi Kirikami , Katsukuni Hisano , Nobuyuki Iizuka , Haruo Urushidani , Isao Sato , Yoji Ishibashi , Takashi Ohmori
发明人： Michio Kuroda , Seiichi Kirikami , Katsukuni Hisano , Nobuyuki Iizuka , Haruo Urushidani , Isao Sato , Yoji Ishibashi , Takashi Ohmori
摘要： A gas turbine combustor comprising a head combustion chamber and a rear combustion chamber connected to a downstream side of the head combustion chamber, a first stage burner for premixing first stage fuel and air and supplying the resultant fuel and air premixture into the head combustion chamber to effect first stage premix combution, a second stage burner for premixing second stage fuel and air and the resultant fuel and air premixture into the rear combustion chamber to effect premix combustion in addition to the first stage premix combustion, and a device for regulating flow rates of combustion air to be premixed with first and second stage fuel. The combustor is further provided with a pilot burner in the head combustion chamber to form pilot flame and stabilize the first stage premix combustion.
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公开(公告)号：US4603548A
公开(公告)日：1986-08-05
申请号：US647658
申请日：1984-09-06
申请人： Yoji Ishibashi , Isao Sato , Fumio Kato , Takashi Ohmori , Noriyuki Hayashi
发明人： Yoji Ishibashi , Isao Sato , Fumio Kato , Takashi Ohmori , Noriyuki Hayashi
摘要： A fuel supply method for a gas turbine combustor having first and second stage combustion chambers. The method comprises supplying the fuel from only first stage fuel supply from the start of the gas turbine until its low output range so as to operate only the first stage combustion chamber, supplying the fuel from both first and second stage fuel supply in a high output range of the gas turbine including its maximum output so as to operate both first and second stage combustion chambers. The method makes it possible to reduce NO.sub.x without deteriorating the combustion performance by step-wise supplying a predetermined flow rate of the fuel when the second stage fuel is to be supplied and at the same time, step-wise reducing the same quantity of the fuel that is being supplied from the first stage fuel supply.
摘要翻译： 一种具有第一和第二级燃烧室的燃气轮机燃烧器的燃料供给方法。 该方法包括仅将燃料从燃气轮机的起始点供给燃料，直到其低的输出范围，以便仅操作第一级燃烧室，从第一和第二级燃料供应源的燃料以高输出 包括其最大输出的燃气轮机的范围，以便操作第一和第二级燃烧室。 该方法可以在不降低燃烧性能的同时，通过在供给第二级燃料时逐步提供燃料的预定流量，同时逐步减少相同量的燃料 这是从第一级燃料供应提供的。
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公开(公告)号：US5239831A
公开(公告)日：1993-08-31
申请号：US727116
申请日：1991-07-09
申请人： Michio Kuroda , Nobuyuki Iizuka , Haruo Urushidani , Kazuhiko Kumata , Isao Sato , Tetsuo Sasada , Hajime Toriya , Yoshikazu Moritomo , Yoji Ishibashi , Takashi Ohmori , Shigeru Azuhata
发明人： Michio Kuroda , Nobuyuki Iizuka , Haruo Urushidani , Kazuhiko Kumata , Isao Sato , Tetsuo Sasada , Hajime Toriya , Yoshikazu Moritomo , Yoji Ishibashi , Takashi Ohmori , Shigeru Azuhata
摘要： A burner comprises at least one swirl member for mixing a fuel with an air previously to burning of the fuel, and at least one eddy generating device which is arranged in a flow of a mixture of the fuel and air to generate an eddy flow in the flow so that the eddy flow maintains a shape of a flame of the burned fuel. The at least one eddy generating device is arranged apart from a downstream end of the swirl member by a fixed sufficient distance so that the shape of the flame maintained by the eddy flow is prevented from moving toward the downstream end of the swirler member.
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9.发明授权公开(公告)号：US08232321B2
公开(公告)日：2012-07-31
申请号：US12670181
申请日：2008-07-25
申请人： Takashi Ohmori , Akira Ishikubo , Yuki Sugiyama , Yuko Matsui , Tomoyuki Kawasoe , Yoji Tezuka , Hiroyasu Mizuno , Kei-ichi Maruyama
发明人： Takashi Ohmori , Akira Ishikubo , Yuki Sugiyama , Yuko Matsui , Tomoyuki Kawasoe , Yoji Tezuka , Hiroyasu Mizuno , Kei-ichi Maruyama
CPC分类号： A61Q1/02 , A61K8/86 , A61Q19/00 , C08G65/2609 , C08G65/2615 , C08G65/337 , C08L71/02
摘要： The present invention is to provide a new compound having a rough skin improving effect, excellent in safety, excellent in texture in use, especially free of sticky feeling, excellent in refreshing feeling, and capable to improve the base agent stability as a component. An alkylene oxide derivative is characterized by being represented by the below-described general formula (I): (formula I) Z—{O-[(AO)a-(EO)b]-R}2 (I) (In the formula, Z is the residue obtained by removing hydroxyl groups from the dimer diol, EO is an oxyethylene group, AO is an oxyalkylene group having 3 to 4 carbon atoms, and the addition form is block-type. The symbols a and b are the average addition mole numbers of the above-described oxyalkylene group and the oxyethylene group, respectively, and they are 1≦2 a≦150 and 1≦2 b≦150. The percentage of the oxyethylene groups with respect to the sum of the oxyalkylene groups having 3 to 4 carbon atoms and the oxyethylene groups is 10 to 99 mass %. Rs may be either identical to or different from each other, and they are hydrocarbon groups having 1 to 4 carbon atoms.)
摘要翻译： 本发明提供一种具有粗糙皮肤改善效果，安全性优异，使用质地优异，特别是无粘性，清爽感好，能提高作为成分的基剂稳定性的新化合物。 氧化烯衍生物的特征在于由下述通式（I）表示：（式I）Z- {O - [（AO）a-（EO）b] -R} 2（I） 式中，Z为从二聚二醇中除去羟基得到的残基，EO为氧化乙烯基，AO为碳原子数3〜4的氧化烯基，添加形式为嵌段型，符号a和b为 分别为上述氧化烯基和氧化乙烯基的平均加成摩尔数，它们分别为1和n 1; 2 a＆nlE; 150和1＆nlE; 2 b＆nlE; 150。氧化乙烯基相对于氧化烯基的总和的百分比 具有3〜4个碳原子，氧化乙烯基为10〜99质量％，Rs可以相同也可以不同，为碳原子数1〜4的烃基）
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公开(公告)号：US07625574B2
公开(公告)日：2009-12-01
申请号：US10134441
申请日：2002-04-30
申请人： Takashi Ohmori , Tohru Okamoto , Hiroyuki Kakoki , Reiji Miyahara , Tomiyuki Nanba , Toshihiko Nakane , Yohei Hamano , Eriko Takeoka
发明人： Takashi Ohmori , Tohru Okamoto , Hiroyuki Kakoki , Reiji Miyahara , Tomiyuki Nanba , Toshihiko Nakane , Yohei Hamano , Eriko Takeoka
CPC分类号： A61K8/39 , A61K8/34 , A61K8/347 , A61K8/676 , A61K8/90 , A61K9/0014 , A61K47/08 , A61K47/10 , A61Q5/00 , A61Q15/00 , A61Q19/00 , Y10S514/946 , Y10S514/947
摘要： A skin treatment composition of the present invention is an external composition for skin comprising an alkylene oxide derivative expressed by Formula (I): R1O—[(AO)m(EO)n]—R2 (I) wherein AO is an oxyalkylene group of C3 or C4; EO is an oxyethylene group; m and n are 1≦m≦70 and 1≦n≦70 respectively, wherein EO is 20˜80% by weight with respect to a total of AO and EO; each of R1 and R2 is a hydrogen or a hydrocarbon group having C1-4. The alkylene oxide derivative (I) has a moisturizing effect, a rough skin improving effect, a stickiness improving effect, and a transdermal absorption promoting effect. When a refreshing agent is used together therewith in the composition of the present invention, the refreshing effect lasts for a long time and it is excellent in feeling of use without skin stimulation.
摘要翻译： 本发明的皮肤治疗组合物是皮肤外用组合物，其含有式（I）表示的烯化氧衍生物：R1O - [（AO）m（EO）n] -R2（Ⅰ）其中，AO为氧化烯基 C3或C4; EO是氧乙烯基; m和n分别为1≤m≤70和1≤n≤70，其中EO相对于AO和EO的总和为20〜80重量％ R 1和R 2各自为氢或具有C 1-4的烃基。 氧化烯衍生物（I）具有保湿效果，粗糙的皮肤改善效果，粘着性改善效果和透皮吸收促进效果。 当与本发明的组合物一起使用清新剂时，清爽效果持续很长时间，并且在没有皮肤刺激的情况下使用感觉优异。
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