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61. 发明申请

US20050021191A1 Environment conservation contribution system 审中-公开
标题翻译：环境保护贡献制度
公开(公告)号：US20050021191A1
公开(公告)日：2005-01-27
申请号：US10864366
申请日：2004-06-10
申请人： Makoto Taniguchi , Akira Kato , Katsunori Tanaka
发明人： Makoto Taniguchi , Akira Kato , Katsunori Tanaka
IPC分类号： F02D29/06 , B60K28/10 , B60L50/15 , B60W10/08 , B60W10/26 , B60W20/00 , B60W30/18 , F02D29/02 , G06F7/00 , G06Q50/00 , G06Q50/26 , H02J7/00 , H02J7/16
CPC分类号： B60W20/15 , B60W10/08 , B60W10/26 , B60W20/00 , B60W30/18127 , Y02T10/52 , Y02T10/84
摘要： An in-vehicle generator is caused to start regenerative generation when the regenerative generation is possible. This regenerative generation can decrease a generation amount under a vehicle traveling state where fuel is consumed and exhaust gas is emitted, thereby decreasing a load of an engine and amounts of fuel consumption and exhaust emission. The fuel consumption or exhaust emission to be decreased is computed and transmitted to a managing center via an in-vehicle wireless terminal. The managing center provides a driver with a reward such as a service corresponding to the decreased amount of fuel consumption or exhaust emission that is computed in the relevant vehicle. This system enables the regenerative generation to be returned to the driver as an economic value, motivating the driver to decrease the fuel consumption or exhaust emission. This thereby contributes to the conservation of global environment.
摘要翻译：当再生发电可能时，使车载发电机启动再生发电。这种再生发电可以减少在燃料消耗和排出气体的车辆行驶状态下的发电量，从而减少发动机的负荷和燃料消耗量和废气排放量。计算要减少的燃料消耗量或废气排放量，并通过车载无线终端发送到管理中心。管理中心向驾驶员提供奖励，例如对应于在相关车辆中计算的燃料消耗量或废气排放量减少的服务。该系统能够将再生发电作为经济价值返回驾驶员，从而激励驾驶员降低燃料消耗或废气排放。从而有助于保护全球环境。

62. 发明授权

US06815864B2 AC generator 失效
标题翻译：交流发电机
公开(公告)号：US06815864B2
公开(公告)日：2004-11-09
申请号：US09839209
申请日：2001-04-23
申请人： Katsunori Tanaka , Yoshihito Asao
发明人： Katsunori Tanaka , Yoshihito Asao
IPC分类号： H02K1922
CPC分类号： H02K21/044
摘要： An ac generator comprising a rotor coil for generating a magnetic flux, a pole core disposed to cover the rotor coil and having pawl-shaped magnetic poles projecting in staggered and alternating relationship, permanent magnets disposed on both side surfaces of the pawl-shaped magnetic poles for reducing the leakage of the magnetic flux, and a fan for cooling. The permanent magnets are samarium-iron alloy magnets containing Ti and B, or plastic magnets made of magnet powder bonded together by a resin, bonded magnets of Sm8.2—Fe75.6—Ti2.3—B0.9—N13. One portion of the side opposing to the pawl-shaped magnetic pole side surfaces of the permanent magnet may be resin-coated. A restricting means for restricting the displacement of the magnetic pole in the radial direction may be disposed in the vicinity of the tips of the magnetic poles.
摘要翻译：一种交流发电机，包括用于产生磁通量的转子线圈，设置成覆盖转子线圈并具有以交错和交替关系突出的棘爪状磁极的磁极铁芯，设置在棘爪状磁极的两侧表面上的永磁体用于减少磁通量的泄漏和用于冷却的风扇。永久磁铁是含有Ti和B的钐 - 铁合金磁体，或由用树脂粘合在一起的磁粉制成的塑料磁体，Sm8.2-Fe75.6-Ti2.3-B0.9-N13的粘结磁体。与永磁体的棘爪状磁极侧面相对的一侧的一部分可以被树脂涂覆。用于限制磁极在径向上的位移的限制装置可以设置在磁极的尖端附近。

63. 发明授权

US06662568B2 Hollow structure with flange 有权
标题翻译：空心结构带法兰
公开(公告)号：US06662568B2
公开(公告)日：2003-12-16
申请号：US10378602
申请日：2003-03-05
申请人： Hiroshi Shimizu , Mitsuru Kondo , Hironobu Hakoda , Yukihiro Hashimoto , Katsunori Tanaka , Sousuke Nakamura
发明人： Hiroshi Shimizu , Mitsuru Kondo , Hironobu Hakoda , Yukihiro Hashimoto , Katsunori Tanaka , Sousuke Nakamura
IPC分类号： F02C720
CPC分类号： F01D9/023 , F05D2260/94 , F05D2260/941 , F05D2300/50212 , F16B2200/50 , F16L23/00 , F16L23/24 , F23R2900/00005
摘要： The present invention provides a hollow structure with at least one flange which can eliminate the possibility of creating crackings due to the thermal fatigue, thereby improving the durability thereof. A hollow structure with an flange according to the present invention includes at least one annular flange fixedly attached around the hollow structure which has a temperature gradient in the direction of the thickness of the wall thereof, wherein said at least one annular flange including an outer portion formed of a metal material having a coefficient of linear expansion greater than that of the metal material forming another portion of said at least one annular flange.
摘要翻译：本发明提供具有至少一个凸缘的中空结构，其可以消除由于热疲劳而产生裂纹的可能性，从而提高其耐久性。根据本发明的具有凸缘的中空结构包括至少一个环形凸缘，该环形凸缘固定地附接在中空结构周围，该环形凸缘具有在其壁厚方向上的温度梯度，其中所述至少一个环形凸缘包括外部部分由具有大于形成所述至少一个环形凸缘的另一部分的金属材料的线性膨胀系数的金属材料形成。

64. 发明授权

US06594999B2 Combustor, a gas turbine, and a jet engine 失效
标题翻译：燃烧器，燃气轮机和喷气发动机
公开(公告)号：US06594999B2
公开(公告)日：2003-07-22
申请号：US09908637
申请日：2001-07-20
申请人： Shigemi Mandai , Yutaka Kawata , Atsushi Maekawa , Katsunori Tanaka , Masaharu Nishimura , Soichiro Tomimoto
发明人： Shigemi Mandai , Yutaka Kawata , Atsushi Maekawa , Katsunori Tanaka , Masaharu Nishimura , Soichiro Tomimoto
IPC分类号： F02C300
CPC分类号： F23R3/26 , F23D2210/00 , F23D2900/00008 , F23D2900/14004 , F23R3/14 , F23R3/54 , F23R2900/00014 , Y02T50/675
摘要： A combustor can simultaneously reduce the amount of NOx exhaust and combustion oscillation. The combustor has an internal cylinder which accommodates a premixing nozzle and an external cylinder which accommodates the internal cylinder, and includes an air flow passage which supplies air from a compressor to the premixing nozzle. The air flow passage is provided with a punched metal plate near the maximum velocity fluctuation position whereat the velocity fluctuation of the air flow increases to a maximum.
摘要翻译：燃烧器可以同时减少NOx排放量和燃烧振荡。燃烧器具有内筒，其容纳预混合喷嘴和容纳内筒的外筒，并且包括将空气从压缩机供给到预混合喷嘴的空气流动通道。空气流路在最大速度波动位置附近设置有冲孔金属板，空气流的速度波动最大化。

65. 发明授权

US06593918B2 Matrix-type panel driving circuit and method and liquid crystal display device 失效
标题翻译：矩阵式面板驱动电路及方法及液晶显示装置
公开(公告)号：US06593918B2
公开(公告)日：2003-07-15
申请号：US09093446
申请日：1998-06-08
申请人： Yoshihisa Taguchi , Katsunori Tanaka , Toshiya Onodera , Katsuhiko Kishida , Hirofumi Miyamoto
发明人： Yoshihisa Taguchi , Katsunori Tanaka , Toshiya Onodera , Katsuhiko Kishida , Hirofumi Miyamoto
IPC分类号： G09G500
CPC分类号： G09G5/005 , G09G3/3611 , G09G5/006 , G09G2320/04 , G09G2340/0442 , G09G2360/02
摘要： A driving circuit for a matrix-type panel includes a control circuit which causes image data to be supplied to the matrix-type panel when a synchronization between the image data and an operation of the matrix-type panel is established after a supply of a given timing signal necessary for an operation of the control circuit is stopped and is then restarted.
摘要翻译：用于矩阵型面板的驱动电路包括控制电路，当图像数据和矩阵型面板的操作在给定的供给之后建立时，使图像数据被提供给矩阵型面板停止对控制电路的动作所需的定时信号，然后重新起动。

66. 发明授权

US06553766B2 Cooling structure of a combustor tail tube 有权
标题翻译：燃烧器尾管的冷却结构
公开(公告)号：US06553766B2
公开(公告)日：2003-04-29
申请号：US09832937
申请日：2001-04-12
申请人： Takehiko Shimizu , Satoshi Hada , Kouichi Akagi , Katsunori Tanaka , Ryotaro Magoshi , Mitsuo Hasegawa , Shigemi Mandai , Mitsuru Kondo
发明人： Takehiko Shimizu , Satoshi Hada , Kouichi Akagi , Katsunori Tanaka , Ryotaro Magoshi , Mitsuo Hasegawa , Shigemi Mandai , Mitsuru Kondo
IPC分类号： F23R306
CPC分类号： F23M5/08 , F01D9/023 , F02C7/16 , F05D2260/2322 , F23R3/002
摘要： A cooling structure of a combustor tail tube is capable of avoiding the formation of cracks in the tail tube by lessening thermal stress and preventing thermal deformation, thus extending the service life. A multiplicity of cooling jackets (5) extend in the longitudinal direction of the tail tube of a gas turbine combustor along the entire circumference of the tail tube wall. The passage sectional area of the cooling jackets (5) is varied depending on the metal temperature of parts of the tail tube (4). For example, the passage sectional area of the cooling jackets (5) formed at the rotor side wall and the mutually opposite side walls of the adjacent tail tube is larger than the passage sectional area of the cooling jackets (5) formed at the casing side wall.
摘要翻译：燃烧器尾管的冷却结构能够通过减少热应力和防止热变形来避免尾管中的裂纹的形成，延长使用寿命。多个冷却套（5）沿着尾管壁的整个圆周在燃气轮机燃烧器的尾管的纵向方向上延伸。冷却套（5）的通道截面积根据尾管（4）的部件的金属温度而变化。例如，形成在转子侧壁的冷却套（5）和相邻尾管的相对侧壁的通道截面积大于形成在壳体侧的冷却套（5）的通道截面面积壁。

67. 发明授权

US06524061B1 Arrangement for sealing a steam-cooled gas turbine 有权
标题翻译：用于密封蒸汽冷却燃气轮机的布置
公开(公告)号：US06524061B1
公开(公告)日：2003-02-25
申请号：US09672311
申请日：2000-09-29
申请人： Kazuharu Hirokawa , Katsunori Tanaka , Kazuo Uematsu
发明人： Kazuharu Hirokawa , Katsunori Tanaka , Kazuo Uematsu
IPC分类号： F01D518
CPC分类号： F01D5/084 , F01D5/085 , F05D2260/2322 , F05D2260/60 , F16B2200/50 , Y10T403/7026
摘要： There is provided a steam-cooled gas turbine with a plurality of blades cooled by a steam supplied from an external steam source. The rotor of the steam-cooled gas turbine is composed of a plurality of rotor disks connected by a plurality of spindle bolt extending through the rotor disks. The rotor includes a steam supply passage extending in the rotor, a steam supply chamber for distributing the steam to the respective blades, a steam recovery chamber for equally receiving the steam used for cooling the blades, and a steam recovery passage for directing the steam from the steam recovery chamber to the outside of the steam-cooled gas turbine. A sealing member in the form of substantially a ring, for sealing the steam leakage between the rotor and the spindle bolts, is disposed about each of the spindle bolts. The rotor includes recesses, disposed coaxially with the respective spindle bolt holes, for receiving the sealing members. A plurality of holding members holds the sealing members in place within the respective recesses by axially clamping the sealing members and engaging with the inner walls of the recesses.
摘要翻译：提供了一种蒸汽冷却的燃气轮机，其具有由从外部蒸汽源供应的蒸汽冷却的多个叶片。蒸汽冷却燃气轮机的转子由多个通过转子盘延伸的主轴螺栓连接的转子盘组成。转子包括在转子中延伸的蒸汽供应通道，用于将蒸汽分配到各个叶片的蒸汽供应室，用于同等地接收用于冷却叶片的蒸汽的蒸汽回收室，以及用于将蒸汽从蒸汽回收室到蒸汽冷却燃气轮机的外部。围绕每个主轴螺栓设置有大致环形密封件，用于密封转子和主轴螺栓之间的蒸汽泄漏。转子包括与相应的主轴螺栓孔同轴设置的用于接收密封构件的凹部。多个保持构件通过轴向夹持密封构件并与凹部的内壁接合而将密封构件保持在各个凹部内的适当位置。

68. 发明授权

US06460339B2 Gas turbine fuel injector with unequal fuel distribution 有权
标题翻译：具有不均等燃料分配的燃气轮机燃油喷射器
公开(公告)号：US06460339B2
公开(公告)日：2002-10-08
申请号：US09828138
申请日：2001-04-09
申请人： Koichi Nishida , Katsunori Tanaka , Shigemi Mandai , Yutaka Kawata , Masataka Ohta
发明人： Koichi Nishida , Katsunori Tanaka , Shigemi Mandai , Yutaka Kawata , Masataka Ohta
IPC分类号： F02G300
CPC分类号： F23R3/343 , F23R3/286
摘要： A gas turbine combustor improves the fuel distribution from a main fuel nozzle, suppressing fluctuations of internal pressure and elevation of inner tube metal temperature, and enhancing the combustion stability and durability of the combustor. The gas turbine combustor is a multi-nozzle type premixing combustor with a nozzle outer tube (7) for forming and injecting a premixed gas of main fuel and combustion air divided and disposed in plural sections around a cone (4) for forming a diffusion flame by reaction between pilot fuel and combustion air disposed in a center of a section of a combustor inner tube (1). Nozzle holes (5a) of a main fuel nozzle (5) are formed in three positions at equal intervals on the nozzle main body wall, and one of them is disposed at the outer periphery of the combustor inner tube (1) on a diametral line linking between the center of the combustor inner tube (1) and the center of the main fuel nozzle (5), whereby the fuel distribution to the outer periphery is decreased.
摘要翻译：燃气轮机燃烧器改善来自主燃料喷嘴的燃料分布，抑制内部压力的波动和内管金属温度升高，提高燃烧器的燃烧稳定性和耐久性。燃气轮机燃烧器是具有喷嘴外管（7）的喷嘴外管（7）的多喷嘴型预混合燃烧器，用于形成并喷射主燃料和燃烧空气的预混合气体，燃烧空气以形成扩散火焰的锥体（4）为中心分成多个部分通过引燃燃料与设置在燃烧器内管（1）的一部分的中心的燃烧空气之间的反应。主燃料喷嘴（5）的喷嘴孔（5a）以等间隔在喷嘴主体壁上形成三个位置，其中一个位于燃烧器内管（1）的外径上，在燃烧器内管（1）的中心与主燃料喷嘴（5）的中心之间连接，从而减少了向外周的燃料分配。

69. 发明授权

US06223724B1 High-pressure fuel pump 失效
标题翻译：高压燃油泵
公开(公告)号：US06223724B1
公开(公告)日：2001-05-01
申请号：US09481413
申请日：2000-01-12
申请人： Wakaki Miyaji , Yoshihiko Onishi , Katsunori Tanaka , Kouichi Ojima
发明人： Wakaki Miyaji , Yoshihiko Onishi , Katsunori Tanaka , Kouichi Ojima
IPC分类号： F02M3704
CPC分类号： F04B1/0465 , F02M59/462 , F02M59/464
摘要： A first fuel inlet, a second fuel inlet, a first fuel outlet, and a second fuel outlet of a valve assembly of a high-pressure fuel pump are formed radially outside an aperture portion of a fuel pressurization chamber.
摘要翻译：在燃料加压室的开口部的径向外侧形成有高压燃料泵的阀组件的第一燃料入口，第二燃料入口，第一燃料出口和第二燃料出口。

70. 发明授权

US6152690A Sealing apparatus for gas turbine 有权
标题翻译：燃气轮机密封装置
公开(公告)号：US6152690A
公开(公告)日：2000-11-28
申请号：US242529
申请日：1999-05-19
申请人： Yasuoki Tomita , Hiroki Fukuno , Katsunori Tanaka , Toshiaki Sano
发明人： Yasuoki Tomita , Hiroki Fukuno , Katsunori Tanaka , Toshiaki Sano
IPC分类号： F01D5/30 , F01D11/00 , F01D11/02 , F01D11/04 , F01D11/12 , F02C7/28 , F01D5/00
CPC分类号： F01D11/001 , F01D11/025 , F01D11/127
摘要： A seal ring (1) securing inner shroud members (32) of stationary blades (31) is provided with arm portions (2, 3) projecting along lower surfaces of end portions of the inner shroud members (32). Honeycomb seals (4a, 4b) are mounted on the arm portions (2, 3), respectively. The honeycomb seal (4a) is disposed opposite fins (11a) provided on a rotor arm portion (11) of a platform (22) of a moving blade (21) so that a predetermined clearance (t) can be maintained between the honeycomb seal and the fins. On the other hand, the honeycomb seal (4b) is disposed opposite fins (14b) provided on a seal portion (14a) of a sealing plate (14) of the moving blade (21) so that a predetermined clearance (t) can be maintained between the honeycomb seal and the fins. The inner shroud members (32) undergo deformation after operation of the gas turbine. However, because the honeycomb seals (4a, 4b) are mounted on the arm portions (3, 2), respectively, of the seal ring (1) disposed separately and independently from the inner shroud members (32), the honeycomb seals (4a, 4b) can remain unaffected by the deformation of the inner shroud members (32), whereby the predetermined clearances (t) can be consistently maintained.
摘要翻译： PCT No.PCT / JP98 / 02722 Sec。 371日期1999年5月19日 102（e）日期1999年5月19日PCT提交1998年6月18日PCT公布。 WO98 / 58159 PCT公开日期1998年12月23日固定固定叶片（31）的内罩构件（32）的密封环（1）设置有沿着内护罩构件（32）的端部的下表面突出的臂部（2,3）。蜂窝密封件（4a，4b）分别安装在臂部分（2,3）上。蜂窝密封件4a设置在设置在活动叶片（21）的平台（22）的转子臂部分（11）上的翅片（11a）上，从而可以在蜂窝密封件（4a）之间保持预定的间隙（t）和翅片。另一方面，蜂窝状密封件4b设置在设置在动叶片21的密封板14的密封部14a上的翅片14b上，从而能够使规定的间隙（t）为保持在蜂窝状密封件和翅片之间。内部护罩构件（32）在燃气轮机的操作之后经历变形。然而，由于蜂窝密封件（4a，4b）分别安装在与内侧护罩构件（32）分开且独立设置的密封环（1）的臂部（3,2）上，蜂窝密封件（4a），4b）可以不受内侧护罩构件（32）的变形的影响，由此可以一致地保持预定间隙（t）。

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