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    • 23. 发明申请
    • GAS TURBINE COMBUSTOR
    • 气体涡轮搅拌机
    • US20100192586A1
    • 2010-08-05
    • US12670207
    • 2008-08-26
    • Yoshitaka TeradaTetsu KonishiKatsuyoshi Omae
    • Yoshitaka TeradaTetsu KonishiKatsuyoshi Omae
    • F23R3/36F02C7/22
    • F23R3/36F23D14/78F23D17/002F23R3/283F23R3/286
    • An object is to provide a low cost gas turbine combustor. The gas turbine combustor comprises main nozzles (3) each having a cylindrical central tube (4) using an interior thereof as an oil fuel path (6) through which oil fuel flows, a cylindrical outer tube (5) disposed on an outermost periphery of the main nozzle (3), and a support tube (8) disposed between the central tube (4) and the outer tube (5), the central tube (4), the outer tube (5) and the support tube (8) each being formed independently. The support tube (8) has such an internal diameter as to form a clearance becoming an insulating air layer (9) between the support tube (8) and an outer periphery of the central tube (4), and includes a plurality of supporting portions (8c) formed on an axially upstream side and radially contacting an inner periphery of the outer tube (5), a plurality of groove portions (7a) formed along an axial direction between the supporting portions (8c), and a cylindrical portion (8b) formed on an axially downstream side and having an external diameter equal to or smaller than an external diameter of the groove portions (7a). Spaces formed by the outer tube (5) and the groove portions (7a), and a space formed by the outer tube (5) and the cylindrical portion (8b) are used as the gas fuel path in which gas fuel flows.
    • 目的在于提供一种低成本燃气轮机燃烧器。 燃气轮机燃烧器包括主喷嘴(3),每个主喷嘴(3)具有一个圆筒形中心管(4),其中使用其内部作为油燃料流动的油燃料通路(6),一个设置在最外周的圆柱形外管(5) 主喷嘴(3)和设置在中心管(4)和外管(5)之间的支撑管(8),中心管(4),外管(5)和支撑管(8) 每个都是独立形成的。 所述支撑管(8)具有形成所述支撑管(8)与所述中心管(4)的外周之间的绝缘空气层(9)的间隙的内径,并且包括多个支撑部 (8c)形成在轴向上游侧并与外筒(5)的内周径向接触的多个槽部(7a),沿支撑部(8c)的轴向形成的多个槽部(7a)和圆筒部 )形成在轴向下游侧并具有等于或小于所述槽部(7a)的外径的外径。 使用由外管(5)和槽部(7a)形成的空间和由外管(5)和圆筒部(8b)形成的空间作为气体燃料流动的气体燃料路径。
    • 24. 发明申请
    • GAS TURBINE COMBUSTOR
    • 气体涡轮搅拌机
    • US20100192584A1
    • 2010-08-05
    • US12670039
    • 2008-08-26
    • Yoshitaka TeradaTetsu KonishiKatsuyoshi Omae
    • Yoshitaka TeradaTetsu KonishiKatsuyoshi Omae
    • F02C7/22
    • F23R3/283F02C7/228F23R3/34F23R3/36F23R3/46
    • An object is to provide a low cost gas turbine combustor. The gas turbine combustor has a plurality of main nozzles annularly supported on a nozzle pipe base (11), and the main nozzles each have an oil fuel path for supplying oil fuel and a gas fuel path for supplying gas fuel. A plurality of the oil fuel paths are provided to penetrate the nozzle pipe base (11), and a plurality of lengths of upright piping (21) are provided to be connected to the oil fuel paths, respectively, and be erected on the nozzle pipe base (11). A plurality of lengths of connection piping (22) for interconnecting the lengths of the upright piping (21) in a polygonal shape at a minimum distance are provided outside the nozzle pipe base (11). An oil fuel supply section (14) is connected to one of the lengths of the connection piping (22) to distribute oil fuel to each of the oil fuel paths.
    • 目的在于提供一种低成本燃气轮机燃烧器。 燃气轮机燃烧器具有环形地支撑在喷嘴管座(11)上的多个主喷嘴,并且主喷嘴各具有用于供给油燃料的油燃料路径和用于供给气体燃料的气体燃料路径。 设置多个油燃料路径以穿透喷嘴管基座(11),并且分别设置多个长度的直立管道(21),以连接到油燃料路径,并竖立在喷嘴管 基地(11)。 在喷嘴管基部11的外侧设置多个连续配管(22),用于将直立管道(21)的长度以多边形形式以最小距离互连。 油燃料供给部(14)与连接配管(22)的长度方向连接,将油燃料分配到各油路。
    • 28. 发明申请
    • Paint Composition, a Painting and Finishing Method, and Painted Articles
    • 油漆成分,绘画和表面处理方法以及绘画文章
    • US20080177006A1
    • 2008-07-24
    • US11910671
    • 2006-04-11
    • Tetsu KonishiShinji MitsumuneMasayuki TakemotoTakehito ItoHiroyuki TagkagiRui Niimi
    • Tetsu KonishiShinji MitsumuneMasayuki TakemotoTakehito ItoHiroyuki TagkagiRui Niimi
    • C08G65/26
    • C08G18/6237C08G18/7831C09D4/06C09D175/04
    • The provision of a paint composition that affords a paint film of excellent acid rain resistance, contamination resistance, water resistance, weather resistance and painting workability, with particularly excellent resistance to vehicle wash damage; and a painting and finishing method, and painted articles. [Overcoming means] A paint composition, characterized in that it has as indispensable components (A) a hydroxyl group-containing resin that is obtained by the addition and polymerization of (a) a compound that contains one carboxyl group and does not have a radical polymerizable double bond, (b) a lactone compound, and (c) an epoxy group-containing radical polymerizable monomer, and, if necessary, (d) another radical polymerizable monomer, and which has a resin hydroxyl value of from 180 to 400 mgKOH/g and a weight average molecular weight of from 2000 to 30,000, and in which the structural unit based on the lactone compound component (b) is from 20 to 60% by mass of the resin solids content; and (B) a crosslinking agent containing per molecule at least one functional group that reacts with hydroxyl groups.
    • 提供具有优异耐酸雨性,耐污染性,耐水性,耐候性和涂漆加工性的漆膜的涂料组合物,具有特别优异的耐车辆洗涤损伤性; 和一个绘画和整理方法,并绘制文章。 [克服方法]一种涂料组合物,其特征在于,其具有通过(a)含有一个羧基并且不具有自由基的化合物的加成和聚合而获得的含羟基树脂作为不可缺少的成分(A) 可聚合双键,(b)内酯化合物和(c)含环氧基的可自由基聚合的单体,如果需要,(d)另一种可自由基聚合的单体,其树脂羟值为180-400mgKOH / g,重均分子量为2000〜30,000,其中基于内酯化合物成分(b)的结构单元的树脂固含量为20〜60质量% 和(B)每分子含有至少一个与羟基反应的官能团的交联剂。
    • 30. 发明申请
    • GAS TURBINE COMBUSTOR
    • 气体涡轮搅拌机
    • US20100115966A1
    • 2010-05-13
    • US12595160
    • 2008-04-11
    • Tomoto NagaiEigo KatouTetsu Konishi
    • Tomoto NagaiEigo KatouTetsu Konishi
    • F02C7/20F02C7/22
    • F23R3/34F02C7/222F02C7/224F05D2260/20F05D2270/082F23D2211/00F23R3/286F23R3/44F23R2900/00005
    • In a gas turbine combustor, a cavity (49) with which a plurality of first air passages (66) communicates is formed by covering with a cover (62) a concave portion (65) of a top hat main body (61) in which the first air passages (66) are formed along the circumferential direction of the top hat main body (61), a plurality of second fuel passages (67) that communicates with the first fuel passages are formed by connecting an inner ring (63) and an outer ring (64) to the top hat main body (61) and by connecting the inner ring (63) and the outer ring (64) to each other, a peg (52) is fixed on the inner ring (63) to communicate with the second fuel passage (67) through a third air passage (68), and thin wall portions (63b, 64b) that serve as a thermal elongation absorbing unit by which thermal elongation is absorbed are provided on the inner ring (63) and the outer ring (64). Thus, stress that works on joining portions of the top hat portion can be reduced, whereby life of the gas turbine combustor can be extended.
    • 在燃气轮机燃烧器中,多个第一空气通道(66)连通的空腔(49)通过用盖(62)覆盖顶帽主体(61)的凹部(65)而形成,其中 第一空气通道(66)沿着顶帽主体(61)的圆周方向形成,与第一燃料通道连通的多个第二燃料通道(67)通过连接内环(63)和 通过将内圈(63)和外圈(64)连接到顶帽主体(61)的外圈(64),将内圈(63)固定在内圈(63)上, 通过第三空气通道(68)与第二燃料通道(67)连通,并且在内圈(63)上设置用作吸收热伸长率的热伸长率吸收单元的薄壁部分(63b,64b) 和外圈(64)。 因此,可以减少在顶帽部分的接合部分工作的应力,从而可以延长燃气轮机燃烧器的寿命。