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1.发明申请COMMUNICATING STRUCTURE BETWEEN COMBUSTOR AND TURBINE PORTION AND GAS TURBINE 有权燃油机与涡轮机和气体涡轮机之间的通讯结构公开(公告)号：US20120247125A1
公开(公告)日：2012-10-04
申请号：US13500009
申请日：2010-05-14
Applicant: Rosic Budmir , Yasuro Sakamoto , Sumiu Uchida , Eisaku Ito , Tsuyoshi Kitamura , Satoshi Hada , Sosuke Nakamura
Inventor： Rosic Budmir , Yasuro Sakamoto , Sumiu Uchida , Eisaku Ito , Tsuyoshi Kitamura , Satoshi Hada , Sosuke Nakamura
Abstract: In a communicating structure between combustors that generates combustion gas inside pipe pieces and a turbine portion that generates a rotational driving force by making the combustion gas sequentially pass through a turbine stage formed of turbine stator vanes and turbine rotor blades, at least some of the first-stage turbine stator vanes closest to the combustor among the turbine stator vanes are disposed downstream of sidewalls of one pipe piece and another pipe piece that are adjacent to each other, and the distance from leading edges of the first-stage turbine stator vanes disposed downstream of the sidewalls of the pipe pieces to end portions of the sidewalls closer to the turbine portion is equal to or less than a spacing between an internal surface of the sidewall of the one pipe piece and an internal surface of the sidewall of the other pipe piece.
Abstract translation: 在通过使燃烧气体依次通过由涡轮机定子叶片和涡轮机转子叶片形成的涡轮级而产生旋转驱动力的燃烧器之间的通气结构中产生燃烧气体的至少一部分的第一 在涡轮定子叶片中最接近燃烧器的台阶涡轮机定子叶片设置在彼此相邻的一个管件和另一个管件的侧壁的下游，并且距离设置在下游的第一级涡轮机定子叶片的前缘的距离 所述管件的侧壁的靠近所述涡轮部的所述侧壁的端部的距离等于或小于所述一个管件的侧壁的内表面与所述另一个管件的侧壁的内表面之间的间隔 。
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2.发明申请PROJECTION OPTICAL SYSTEM, EXPOSURE APPARATUS, AND DEVICE MANUFACTURING METHOD 失效投影光学系统，曝光装置和装置制造方法公开(公告)号：US20100214546A1
公开(公告)日：2010-08-26
申请号：US12710246
申请日：2010-02-22
Applicant: Akihiro Yamada , Atsushi Shigenobu , Tsuyoshi Kitamura
Inventor： Akihiro Yamada , Atsushi Shigenobu , Tsuyoshi Kitamura
CPC classification number: G02B5/32 , G02B13/24 , G03F7/70266
Abstract: A system includes a plurality of optical elements, a deformation unit configured to deform a deformable optical element satisfying a following conditional formula included in the plurality of optical elements by applying a force to the deformable optical element: 0.75
Abstract translation: 一种系统包括多个光学元件，变形单元被配置为通过向可变形光学元件施加力来使包含在多个光学元件中的满足以下条件公式的可变形光学元件变形：0.75
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公开(公告)号：US07300251B2
公开(公告)日：2007-11-27
申请号：US10544844
申请日：2004-03-03
Applicant: Tsuyoshi Kitamura , Kenichiro Takeishi , Masaaki Matsuura , Ryoma Nogami
Inventor： Tsuyoshi Kitamura , Kenichiro Takeishi , Masaaki Matsuura , Ryoma Nogami
IPC: F01D5/18
CPC classification number: F01D5/189 , F01D5/186 , F05D2260/201 , Y02T50/676
Abstract: A cooled blade of a small gas turbine engine can enhance cooling performance without increasing the amount of cooling air in a simple configuration. A cooled turbine blade is provided with a cooling passageway 12 formed inside thereof, making the cooling air flow therein. Film-cooling holes 13 penetrate from an inner wall surface 111 to an external wall surface 112 and form a cooling film. An impingement cooling member 2 has a multiple number of small holes 21 ejecting the cooling air. A gap t made by the inner wall surface 111 and the impingement cooling member 2 has a sealing portion 14 mounted thereon which divides the gap in a blade chord direction.
Abstract translation: 小型燃气涡轮发动机的冷却叶片可以在不以简单的结构增加冷却空气量的情况下提高冷却性能。 冷却的涡轮叶片设置有形成在其内部的冷却通道12，使得冷却空气流入其中。 薄膜冷却孔13从内壁面111穿过外壁面112形成冷却膜。 冲击冷却构件2具有多个排出冷却空气的小孔21。 由内壁面111和冲击冷却部件2构成的间隙t具有安装在其上的密封部14，该密封部14沿着叶片弦方向分隔间隙。
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公开(公告)号：US5530928A
公开(公告)日：1996-06-25
申请号：US446128
申请日：1995-05-22
Applicant: Charles E. Wheatley, III , Tohru Izumiyama , Tsuyoshi Kitamura , Mitsunari Okazaki
Inventor： Charles E. Wheatley, III , Tohru Izumiyama , Tsuyoshi Kitamura , Mitsunari Okazaki
CPC classification number: H03D7/1433 , H03D7/1408 , H03D7/1425 , H03D7/1458 , H03C1/542 , H03D2200/0043
Abstract: A balanced mixer is used as a switch. In digital mode, the balanced mixer receives a digital mode analog waveform and a local oscillator (L.O.). The balanced mixer mixes the waveform and the L.O. to provide a resultant output signal. In analog mode, the L.O. is modulated to contain the communication information. No analog signal is present on the port of the mixer which received the digital mode analog waveform in digital mode. The desired output of the mixer is the modulated L.O. In order to pass the L.O. through the mixer, a DC bias is applied to one of the waveform terminals of the mixer to unbalance it. A diode attenuator is added to the output of the mixer to provide scaling of the analog mode output.
Abstract translation: 平衡混频器用作开关。 在数字模式下，平衡混频器接收数字模拟模拟波形和本地振荡器（L.O.）。 平衡混合器混合波形和L.O. 以提供结果输出信号。 在模拟模式下，L.O. 被调制以包含通信信息。 在数字模式下接收数字模拟模拟波形的混频器端口上没有模拟信号。 混合器的期望输出是调制的L.O. 为了通过L.O. 通过混频器，将DC偏压施加到混频器的一个波形端子以使其不平衡。 二极管衰减器被添加到混频器的输出端以提供模拟模式输出的缩放。
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公开(公告)号：US09945250B2
公开(公告)日：2018-04-17
申请号：US13515978
申请日：2011-01-17
Applicant: Tsuyoshi Kitamura , Shinichiro Masaki
Inventor： Tsuyoshi Kitamura , Shinichiro Masaki
CPC classification number: F01D25/14 , F01D11/24 , F02C7/18 , F05D2220/323 , F05D2240/11 , F05D2250/185 , F05D2260/205 , Y02T50/675 , Y02T50/676
Abstract: An aircraft gas turbine is constituted by accommodating a compressor (14), a combustor (15), and a turbine (16) in a cylindrical main unit casing (12). A thick wall part (52) is provided on an outer periphery side of rotor blades (34) in the main unit casing. A cooling passage (53), for cooling the thick wall part (52) by circulating compressed air compressed by the compressor, is provided in the thick wall part. Also provided is a discharge passage (55) for discharging compressed air having circulated in the cooling passage to a combustion gas passage A. The structural strength of the thick wall part is ensured by appropriately cooling the thick wall part of the casing, while simplifying the structure and preventing a decrease in efficiency, thereby ensuring effective containment performance and an appropriate clearance between the casing and the rotor blades.
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Patent Agency Ranking
6.发明授权公开(公告)号：US08163467B2
公开(公告)日：2012-04-24
申请号：US12479636
申请日：2009-06-05
Applicant: Tsuyoshi Kitamura , Nobuhiko Yabu
Inventor： Tsuyoshi Kitamura , Nobuhiko Yabu
CPC classification number: G03B27/52 , G03F7/70341 , G03F7/706
Abstract: A dummy light-exposed substrate used for dummy light-exposure in an immersion exposure apparatus which exposes a substrate to light via a projection optical system and a liquid, comprises a lyophilic region, and a liquid repellent region surrounding the lyophilic region.
Abstract translation: 在通过投影光学系统和液体使基板曝光的浸没曝光装置中用于虚拟曝光的虚拟曝光基板包括亲液性区域和围绕亲液性区域的液体排斥区域。
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公开(公告)号：US20060210399A1
公开(公告)日：2006-09-21
申请号：US10544844
申请日：2004-03-03
Applicant: Tsuyoshi Kitamura , Kenichiro Takeishi , Masaaki Matsuura , Ryoma Nogami
Inventor： Tsuyoshi Kitamura , Kenichiro Takeishi , Masaaki Matsuura , Ryoma Nogami
IPC: F01D5/18
CPC classification number: F01D5/189 , F01D5/186 , F05D2260/201 , Y02T50/676
Abstract: The present invention is intended to provide a cooled blade of a small gas turbine engine which can enhance cooling performance without increasing an amount of cooling air although it is in a simple configuration. A cooled turbine blade is provided with a cooling passageway 12 formed inside thereof, making the cooling air flow therein; film-cooling holes 13 formed, penetrating from an inner wall surface 111 to an external wall surface 112 and forming a cooling film; and an impingement cooling member 2 which has a multiple number of small holes 21 ejecting the cooling air. It is characterized by that a gap t made by the inner wall surface 111 and the impingement cooling member 2 has a sealing portion 14 mounted thereon which divides the gap in a blade chord direction.
Abstract translation: 本发明旨在提供一种小型燃气涡轮发动机的冷却叶片，其可以在不增加冷却空气量的情况下提高冷却性能，尽管其处于简单的构造。 冷却的涡轮叶片设置有形成在其内的冷却通道12，使冷却空气流入其中; 形成有从内壁面111向外壁面112贯通并形成冷却膜的薄膜冷却孔13。 以及具有排出冷却空气的多个小孔21的冲击冷却部件2。 其特征在于，由内壁面111和冲击冷却部件2构成的间隙t具有安装在其上的密封部14，该密封部14沿着叶片弦方向分隔间隙。
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8.发明申请Heat exchanging wall, gas turbine using the same, and flying body with gas turbine engine 有权换热墙，采用相同的燃气轮机，带燃气轮机的飞机公开(公告)号：US20050047932A1
公开(公告)日：2005-03-03
申请号：US10912565
申请日：2004-08-06
Applicant: Tomoyoshi Nakae , Kenichiro Takeishi , Masaaki Matsuura , Tsuyoshi Kitamura , Atsushi Moriwaki
Inventor： Tomoyoshi Nakae , Kenichiro Takeishi , Masaaki Matsuura , Tsuyoshi Kitamura , Atsushi Moriwaki
CPC classification number: F23R3/002 , F23R3/005 , F23R2900/03043 , F28F3/02 , F28F3/022 , F28F13/12 , Y02T50/675
Abstract: A heat exchange wall include a base plate; a plurality of first protrusions distributedly provided on a surface of the base plate, and a plurality of second protrusions distributedly provided on the base plate surface. The height of the second protrusion in a normal direction of the base plate is desirably less than ½ of a height of the first protrusion in the normal direction. The height of the second protrusion in the normal direction is desirably between {fraction (1/20)} and ¼ of the height of the first protrusion in the normal direction. More desirably, the height of the second protrusion in the normal direction is {fraction (1/10)} of the height of the first protrusion in the normal direction.
Abstract translation: 热交换壁包括基板; 多个第一突起分布设置在基板的表面上，多个第二突起分布设置在基板表面上。 第二突起在基板的法线方向上的高度优选小于第一突起在法线方向的高度的1/2。 第二突起在法线方向的高度优选为{法线方向的第一突起的高度的1/20〜1/4，更优选地，第二突起在法线方向的高度为{分数（ 第一突起在正常方向的高度的1/10。
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9.发明授权Communicating structure between adjacent combustors and turbine portion and gas turbine 有权相邻燃烧器与涡轮机部分和燃气轮机之间的通信结构公开(公告)号：US09395085B2
公开(公告)日：2016-07-19
申请号：US13500009
申请日：2010-05-14
Applicant: Rosic Budmir , Yasuro Sakamoto , Sumiu Uchida , Eisaku Ito , Tsuyoshi Kitamura , Satoshi Hada , Sosuke Nakamura
Inventor： Rosic Budmir , Yasuro Sakamoto , Sumiu Uchida , Eisaku Ito , Tsuyoshi Kitamura , Satoshi Hada , Sosuke Nakamura
Abstract: In a communicating structure between combustors that generates combustion gas inside pipe pieces and a turbine portion that generates a rotational driving force by making the combustion gas sequentially pass through a turbine stage formed of turbine stator vanes and turbine rotor blades, at least some of the first-stage turbine stator vanes closest to the combustor among the turbine stator vanes are disposed downstream of sidewalls of one pipe piece and another pipe piece that are adjacent to each other, and the distance from leading edges of the first-stage turbine stator vanes disposed downstream of the sidewalls of the pipe pieces to end portions of the sidewalls closer to the turbine portion is equal to or less than a spacing between an internal surface of the sidewall of the one pipe piece and an internal surface of the sidewall of the other pipe piece.
Abstract translation: 在通过使燃烧气体依次通过由涡轮机定子叶片和涡轮机转子叶片形成的涡轮级而产生旋转驱动力的燃烧器之间的通气结构中产生燃烧气体的至少一部分的第一 在涡轮定子叶片中最接近燃烧器的台阶涡轮机定子叶片设置在彼此相邻的一个管件和另一个管件的侧壁的下游，并且距离设置在下游的第一级涡轮机定子叶片的前缘的距离 所述管件的侧壁的靠近所述涡轮部的所述侧壁的端部的距离等于或小于所述一个管件的侧壁的内表面与所述另一个管件的侧壁的内表面之间的间隔 。
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10.发明授权Projection optical system with deformable optical element, exposure apparatus, and device manufacturing method 失效具有可变形光学元件的投影光学系统，曝光装置和器件制造方法公开(公告)号：US08786822B2
公开(公告)日：2014-07-22
申请号：US12710246
申请日：2010-02-22
Applicant: Akihiro Yamada , Atsushi Shigenobu , Tsuyoshi Kitamura
Inventor： Akihiro Yamada , Atsushi Shigenobu , Tsuyoshi Kitamura
IPC: G03B27/68
CPC classification number: G02B5/32 , G02B13/24 , G03F7/70266
Abstract: A system includes a plurality of optical elements, a deformation unit configured to deform a deformable optical element satisfying a following conditional formula included in the plurality of optical elements by applying a force to the deformable optical element: 0.75
Abstract translation: 一种系统包括多个光学元件，变形单元被配置为通过向可变形光学元件施加力来使包含在多个光学元件中的满足以下条件公式的可变形光学元件变形：0.75
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