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1. 发明申请

US20130098063A1 COOLNG STRUCTURE FOR RECOVERY-TYPE AIR-COOLED GAS TURBINE COMBUSTOR 有权
标题翻译：回收式空气冷却气涡轮机的冷却结构
公开(公告)号：US20130098063A1
公开(公告)日：2013-04-25
申请号：US13806523
申请日：2011-08-10
申请人： Satoshi Mizukami , Tatsuo Ishiguro , Junichiro Masada , Kazumasa Takata , Shunsuke Torii , Yuya Fukunaga , Tetsu Konishi , Yoshiaki Nishimura , Yoshiaki Igarashi , Shinya Ishikawa
发明人： Satoshi Mizukami , Tatsuo Ishiguro , Junichiro Masada , Kazumasa Takata , Shunsuke Torii , Yuya Fukunaga , Tetsu Konishi , Yoshiaki Nishimura , Yoshiaki Igarashi , Shinya Ishikawa
IPC分类号： F02C7/18 , F23R3/06 , F02C7/08
CPC分类号： F02C7/18 , F01D9/023 , F02C7/08 , F02C7/24 , F05D2260/202 , F23R3/005 , F23R3/06 , F23R3/44 , F23R2900/00014
摘要： In a cooling structure for a recovery-type air-cooled gas turbine combustor having a recovery-type air-cooling structure that bleeds, upstream of the combustor, and pressurizes compressed air supplied from a compressor, that uses the bled and pressurized air to cool a wall, and that recovers and reuses the bled and pressurized air as combustion air for burning fuel in the combustor together with a main flow of the compressed air, wall cooling in which cooling air is supplied to cooling air passages formed in the wall of the combustor to perform cooling involves a downstream wall region, closer to a turbine, that is cooled using the bled and pressurized air as the cooling air and an upstream wall region, closer to a burner, that is cooled using, as the cooling air, bled compressed air bled from a main flow of the compressed air through a housing inner space.
摘要翻译：在用于具有回收式空气冷却结构的回收式空气冷却燃气轮机燃烧器的冷却结构中，所述回收型空气冷却结构在燃烧器的上游出来并对从压缩机供给的压缩空气进行加压，所述回收式空气冷却结构使用过滤和加压空气来冷却一个墙壁，并且回收和再利用排放和加压的空气作为用于燃烧燃烧器中的燃料的燃烧空气以及压缩空气的主流，壁冷却，其中冷却空气被供应到冷却空气通道用于进行冷却的燃烧器包括更靠近涡轮机的下游壁区域，其使用作为冷却空气的排放和加压空气以及更靠近燃烧器的上游壁区域冷却，所述上游壁区域作为冷却空气被流出压缩空气从压缩空气的主流流过壳体内部空间。

2. 发明授权

US09512781B2 Cooling structure for recovery-type air-cooled gas turbine combustor 有权
标题翻译：回收式风冷式燃气轮机燃烧器的冷却结构
公开(公告)号：US09512781B2
公开(公告)日：2016-12-06
申请号：US13806523
申请日：2011-08-10
申请人： Satoshi Mizukami , Tatsuo Ishiguro , Junichiro Masada , Kazumasa Takata , Shunsuke Torii , Yuya Fukunaga , Tetsu Konishi , Yoshiaki Nishimura , Yoshiaki Igarashi , Shinya Ishikawa
发明人： Satoshi Mizukami , Tatsuo Ishiguro , Junichiro Masada , Kazumasa Takata , Shunsuke Torii , Yuya Fukunaga , Tetsu Konishi , Yoshiaki Nishimura , Yoshiaki Igarashi , Shinya Ishikawa
IPC分类号： F02C7/12 , F02C6/08 , F02C7/18 , F01D9/02 , F02C7/08 , F02C7/24 , F23R3/00 , F23R3/06 , F23R3/44
CPC分类号： F02C7/18 , F01D9/023 , F02C7/08 , F02C7/24 , F05D2260/202 , F23R3/005 , F23R3/06 , F23R3/44 , F23R2900/00014
摘要： In a cooling structure for a recovery-type air-cooled gas turbine combustor having a recovery-type air-cooling structure that bleeds, upstream of the combustor, and pressurizes compressed air supplied from a compressor, that uses the bled and pressurized air to cool a wall, and that recovers and reuses the bled and pressurized air as combustion air for burning fuel in the combustor together with a main flow of the compressed air, wall cooling in which cooling air is supplied to cooling air passages formed in the wall of the combustor to perform cooling involves a downstream wall region, closer to a turbine, that is cooled using the bled and pressurized air as the cooling air and an upstream wall region, closer to a burner, that is cooled using, as the cooling air, bled compressed air bled from a main flow of the compressed air through a housing inner space.
摘要翻译：在用于具有回收式空气冷却结构的回收式空气冷却燃气轮机燃烧器的冷却结构中，所述回收型空气冷却结构在燃烧器的上游出来并对从压缩机供给的压缩空气进行加压，所述回收式空气冷却结构使用过滤和加压空气来冷却一个墙壁，并且回收和再利用排放和加压的空气作为用于燃烧燃烧器中的燃料的燃烧空气以及压缩空气的主流，壁冷却，其中冷却空气被供应到冷却空气通道用于进行冷却的燃烧器包括更靠近涡轮机的下游壁区域，其使用作为冷却空气的排放和加压空气以及更靠近燃烧器的上游壁区域冷却，所述上游壁区域作为冷却空气被排出压缩空气从压缩空气的主流流过壳体内部空间。

3. 发明申请

US20110138818A1 GAS TURBINE AND OPERATING METHOD THEREOF 有权
标题翻译：燃气轮机及其运行方法
公开(公告)号：US20110138818A1
公开(公告)日：2011-06-16
申请号：US13056064
申请日：2009-09-24
申请人： Satoshi Mizukami , Tatsuo Ishiguro , Junichiro Masada , Kazumasa Takata , Yuya Fukunaga , Hiroki Takahashi , Masaki Satoh , Yoshiaki Nishimura , Norio Oogai , Souji Hasegawa , Masato Hayashi
发明人： Satoshi Mizukami , Tatsuo Ishiguro , Junichiro Masada , Kazumasa Takata , Yuya Fukunaga , Hiroki Takahashi , Masaki Satoh , Yoshiaki Nishimura , Norio Oogai , Souji Hasegawa , Masato Hayashi
IPC分类号： F02C7/18 , F02C7/26 , F02C7/12 , F02C6/08
CPC分类号： F01D11/24 , F01D21/00 , F01D21/12 , F02C7/08 , F02C7/12 , F02C7/18 , F05D2260/205 , F05D2260/608
摘要： Provided is a gas turbine capable of achieving high-speed startup of the gas turbine through quick operation control of an ACC system during startup of the gas turbine, improving the cooling efficiency of turbine stationary components, and quickly carrying out an operation required for cat back prevention during shutdown of the gas turbine. Included are a pressurizing device (40) connected to a branching channel (42) branching from the discharge side of a compressor (11) and capable of carrying out an operation for introducing and pressurizing air independently from the compressor (11); a temperature-control-medium supply channel (43) that guides compressed air pressurized at the pressuring device (40) to a turbine-cooling-medium channel (50) provided in stationary components of a turbine (13); and a temperature-control-medium return channel (44) that guides the compressed air that has passed through the turbine-cooling-medium channel (50) to the discharge side of the compressor (11) such that the flows are combined, and the pressurizing device (40) is operated at startup of the gas turbine and in preparation immediately before startup to carry out temperature-raising and cooling by letting the compressed air flow in the turbine-cooling-medium channel (50). The pressurizing device (40) is operated during shutdown of the gas turbine to exhaust the high-temperature gas remaining in the turbine (13).
摘要翻译：提供一种燃气轮机，其能够通过在燃气轮机启动期间ACC系统的快速操作控制来实现燃气轮机的高速启动，提高涡轮机固定部件的冷却效率，并且快速地执行回猫所需的操作在燃气轮机停机期间的预防。包括连接到从压缩机（11）的排出侧分支的分支通道（42）并且能够独立于压缩机（11）执行用于引入和加压空气的操作的加压装置（40）。将压缩装置（40）加压的压缩空气引导到设置在涡轮机（13）的静止部件中的涡轮冷却介质通道（50）的温度控制介质供给通路（43）。以及温度控制介质返回通道（44），其将已经通过所述涡轮冷却介质通道（50）的压缩空气引导到所述压缩机（11）的排出侧，使得所述流合并，并且加压装置（40）在燃气轮机起动时运转，并且在启动之前准备进行，以通过使涡轮机冷却介质通道（50）中的压缩空气流动来进行升温和冷却。加压装置（40）在燃气轮机关闭期间运行，以排出剩余在涡轮机（13）中的高温气体。

4. 发明授权

US09255490B2 Gas turbine and operating method thereof 有权
标题翻译：燃气轮机及其运行方法
公开(公告)号：US09255490B2
公开(公告)日：2016-02-09
申请号：US13056064
申请日：2009-09-24
申请人： Satoshi Mizukami , Tatsuo Ishiguro , Junichiro Masada , Kazumasa Takata , Yuya Fukunaga , Hiroki Takahashi , Masaki Satoh , Yoshiaki Nishimura , Norio Oogai , Souji Hasegawa , Masato Hayashi
发明人： Satoshi Mizukami , Tatsuo Ishiguro , Junichiro Masada , Kazumasa Takata , Yuya Fukunaga , Hiroki Takahashi , Masaki Satoh , Yoshiaki Nishimura , Norio Oogai , Souji Hasegawa , Masato Hayashi
IPC分类号： F01D11/24 , F02C7/18 , F01D21/00 , F02C7/12
CPC分类号： F01D11/24 , F01D21/00 , F01D21/12 , F02C7/08 , F02C7/12 , F02C7/18 , F05D2260/205 , F05D2260/608
摘要： Provided is a gas turbine capable of achieving high-speed startup of the gas turbine through quick operation control of an ACC system during startup of the gas turbine, improving the cooling efficiency of turbine stationary components, and quickly carrying out an operation required for cat back prevention during shutdown of the gas turbine. Included are a pressurizing device (40) connected to a branching channel (42) branching from the discharge side of a compressor (11) and capable of carrying out an operation for introducing and pressurizing air independently from the compressor (11); a temperature-control-medium supply channel (43) that guides compressed air pressurized at the pressuring device (40) to a turbine-cooling-medium channel (50) provided in stationary components of a turbine (13); and a temperature-control-medium return channel (44) that guides the compressed air that has passed through the turbine-cooling-medium channel (50) to the discharge side of the compressor (11) such that the flows are combined, and the pressurizing device (40) is operated at startup of the gas turbine and in preparation immediately before startup to carry out temperature-raising and cooling by letting the compressed air flow in the turbine-cooling-medium channel (50). The pressurizing device (40) is operated during shutdown of the gas turbine to exhaust the high-temperature gas remaining in the turbine (13).
摘要翻译：提供一种燃气轮机，其能够通过在燃气轮机启动期间ACC系统的快速操作控制来实现燃气轮机的高速启动，提高涡轮机固定部件的冷却效率，并且快速地执行回猫所需的操作在燃气轮机关闭期间的预防。包括连接到从压缩机（11）的排出侧分支的分支通道（42）并且能够独立于压缩机（11）执行用于引入和加压空气的操作的加压装置（40）。将压缩装置（40）加压的压缩空气引导到设置在涡轮机（13）的静止部件中的涡轮冷却介质通道（50）的温度控制介质供给通路（43）。以及温度控制介质返回通道（44），其将已经通过所述涡轮冷却介质通道（50）的压缩空气引导到所述压缩机（11）的排出侧，使得所述流合并，并且加压装置（40）在燃气轮机起动时运转，并且在启动之前准备进行，以通过使涡轮机冷却介质通道（50）中的压缩空气流动来进行升温和冷却。加压装置（40）在燃气轮机关闭期间运行，以排出剩余在涡轮机（13）中的高温气体。

5. 发明授权

US08593624B2 Refractive index measuring apparatus 有权
$Refractive index measuring apparatus$
标题翻译：折射率测量装置
公开(公告)号：US08593624B2
公开(公告)日：2013-11-26
申请号：US12990547
申请日：2010-01-21
申请人： Yusuke Kusaka , Yohei Takechi , Atsushi Fukui , Seiji Hamano , Kazumasa Takata
发明人： Yusuke Kusaka , Yohei Takechi , Atsushi Fukui , Seiji Hamano , Kazumasa Takata
IPC分类号： G01N21/41
CPC分类号： G01M11/0228
摘要： By using two probe optical systems for measurement by disposing the probe optical systems with a test object sandwiched therebetween, an optical path length of light transmitted through the test object which is identified locally is calculated using an interference signal thereof. In addition, a geometrical thickness of the same part is calculated by measuring positions of the probe optical systems, whereby two calculated values are obtained. Based on the values and a calculated value for a reference object, a refractive index distribution of the test object is obtained.
摘要翻译：通过使用两个探测光学系统进行测量，通过将测试对象夹在其间设置探测光学系统，使用其干扰信号来计算通过本地识别的测试对象传输的光的光路长度。此外，通过测量探针光学系统的位置来计算同一部分的几何厚度，由此获得两个计算值。基于参考对象的值和计算值，获得测试对象的折射率分布。

6. 发明授权

US07379172B2 Method and apparatus for inspection of optical component 失效
标题翻译：光学部件检查方法和装置
公开(公告)号：US07379172B2
公开(公告)日：2008-05-27
申请号：US11319172
申请日：2005-12-28
申请人： Kazumasa Takata , Hidetoshi Utsuro , Tomotaka Furuta , Takashi Urashima
发明人： Kazumasa Takata , Hidetoshi Utsuro , Tomotaka Furuta , Takashi Urashima
IPC分类号： G01N21/00
CPC分类号： G01M11/0271
摘要： An inspection method for evaluating the performance of an optical component at high precision is provided. According to the inspection method, a first light beam 24 and a second light beam 26 both having different phases are generated from light which has passed through an optical component 18, and are interfered with each other to form an interference region 30. A linear line 66, a linear line 70 and linear lines 72 are set within the interference region 30 so as to determine a distribution of light intensities on each of the linear lines 72. Then, a frequency corresponding to the maximal light intensity is determined. Further, an approximated liner line or an approximated curved line is determined from a plurality of frequencies determined for each of the linear line 72. Then, the aberration of the optical component is evaluated based on the coefficient of the approximated linear or curved line.
摘要翻译：提供了一种用于高精度地评估光学部件的性能的检查方法。根据检查方法，由已经通过光学部件18的光产生具有不同相位的第一光束24和第二光束26，并且彼此干涉以形成干涉区域30。线性线66，线性线70和线性线72设置在干涉区域30内，以便确定每个线性线72上的光强度的分布。然后，确定与最大光强度对应的频率。此外，根据为每个线性线72确定的多个频率来确定近似线性线或近似曲线。然后，基于近似线性或曲线的系数来评价光学部件的像差。

7. 发明授权

US06809829B1 Method and apparatus for evaluating aberrations of optical element and method and apparatus for adjusting optical unit and lens 有权
标题翻译：用于评估光学元件像差的方法和装置以及用于调整光学单元和透镜的方法和装置
公开(公告)号：US06809829B1
公开(公告)日：2004-10-26
申请号：US09573257
申请日：2000-05-18
申请人： Kazumasa Takata , Masahiro Nakajo , Kanji Nishii
发明人： Kazumasa Takata , Masahiro Nakajo , Kanji Nishii
IPC分类号： G01B902
CPC分类号： G01M11/0271 , G01M11/0228
摘要： A lens evaluation method includes diffracting light derived from a lens so that two diffracted rays of different orders (e.g., a 0th-order diffracted ray and a +1st-order diffracted ray) interfere with each other, thereby obtaining a shearing interference figure, and changing phases of the diffracted rays. The method also includes in the shearing interference figure, determining phases of light intensity changes at a plurality of measuring points on a measuring line which passes through a midpoint of a line segment interconnecting optical axes of the two diffracted rays, and determining characteristics (defocus amount, coma, astigmatism, spherical aberration and a higher-order aberration) of the lens based on the phases.
摘要翻译：透镜评价方法包括衍射从透镜衍射的光，使得两个不同阶数的衍射光线（例如，0次衍射光线和+ 1次衍射光线）彼此干涉，从而获得剪切干涉图，并且改变衍射光线的相位。该方法还包括在剪切干涉图中，确定通过互连两个衍射光线的光轴的线段的中点的测量线上的多个测量点处的光强度变化的相位，以及确定特性（散焦量，昏迷，散光，球面像差和高阶像差）。

8. 发明授权

US07561350B2 Optical unit and its manufacturing method 有权
标题翻译：光学单元及其制造方法
公开(公告)号：US07561350B2
公开(公告)日：2009-07-14
申请号：US11793234
申请日：2005-12-15
申请人： Yoshiro Kitamura , Seiji Kumazawa , Koji Funami , Kazumasa Takata , Yasuo Nishihara
发明人： Yoshiro Kitamura , Seiji Kumazawa , Koji Funami , Kazumasa Takata , Yasuo Nishihara
IPC分类号： G02B7/02 , G02B15/14
CPC分类号： G11B7/22 , B29C65/14 , B29C65/1406 , B29C65/1416 , B29C65/1483 , B29C65/1609 , B29C65/1616 , B29C65/1632 , B29C65/1635 , B29C65/1638 , B29C65/1654 , B29C65/1664 , B29C65/4845 , B29C65/52 , B29C66/1122 , B29C66/1222 , B29C66/1224 , B29C66/30223 , B29C66/534 , B29C66/65 , B29C66/71 , B29C66/712 , B29C66/73117 , B29C66/73771 , B29C66/73921 , B29C66/91631 , B29C66/91641 , B29C66/919 , B29C2035/0827 , B29K2105/0079 , B29K2995/0039 , B29L2011/0016 , G02B7/025 , G11B7/1372 , B29K2023/00
摘要： A method for manufacturing an optical unit (10) having an optical element (22) and a support member (12) supporting the optical element. According to the method, at least one of the optical element (22) and the support member (12) is deformed, securing the optical element (22) and the support member (12) together.
摘要翻译：一种用于制造具有支撑光学元件的光学元件（22）和支撑构件（12）的光学单元（10）的方法。根据该方法，光学元件（22）和支撑构件（12）中的至少一个变形，将光学元件（22）和支撑构件（12）固定在一起。

9. 发明授权

US5986727A Back light illuminator for liquid crystal display apparatus 失效
标题翻译：背光灯用于液晶显示装置
公开(公告)号：US5986727A
公开(公告)日：1999-11-16
申请号：US833048
申请日：1997-04-03
申请人： Atsushi Fukui , Kanji Nishii , Kenji Takamoto , Masami Ito , Kazumasa Takata
发明人： Atsushi Fukui , Kanji Nishii , Kenji Takamoto , Masami Ito , Kazumasa Takata
IPC分类号： G02B6/00 , B60Q3/04 , F21V8/00 , G02B5/10 , G02F1/1335 , G02F1/13357 , B60Q1/26 , F21V7/04 , F21V9/16
CPC分类号： G02B6/0031 , B60Q3/004 , B60Q3/044 , B60Q3/046 , G02F1/133615
摘要： A back light illuminator for liquid crystal display apparatus comprises a fluorescent lamp, a light guide member, and a reflection plate enclosing the fluorescent lamp and an incident portion of the light guide member so as to reflect light rays toward the incident portion of the light guide member. The reflection plate has at least a curved portion having a parabolic cross-section or a elliptical cross-section so as not to reflect the light rays in a direction to the fluorescent lamp. Thus, absorption of reflected light by the fluorophor of the fluorescent lamp is minimized, and the luminance of the back light illuminator is increased.
摘要翻译：用于液晶显示装置的背光照明器包括荧光灯，导光构件和包围荧光灯的反射板和导光构件的入射部分，以便将光线朝向光导入射部分反射会员。反射板具有至少一个具有抛物面截面或椭圆形横截面的弯曲部分，以便不向与荧光灯的方向反射光线。因此，荧光灯的荧光体的反射光的吸收最小化，背光照射器的亮度增加。

10. 发明授权

US5980054A Panel-form illuminating system 失效
标题翻译：面板式照明系统
公开(公告)号：US5980054A
公开(公告)日：1999-11-09
申请号：US839232
申请日：1997-04-24
申请人： Atsushi Fukui , Kanji Nishii , Kenji Takamoto , Masami Ito , Kazumasa Takata , Ken Tatsuta , Koki Nakabayashi , Hiroshi Watanabe
发明人： Atsushi Fukui , Kanji Nishii , Kenji Takamoto , Masami Ito , Kazumasa Takata , Ken Tatsuta , Koki Nakabayashi , Hiroshi Watanabe
IPC分类号： F21V8/00 , G02B6/00 , F21V7/04
CPC分类号： G02B6/0038 , G02B6/0036 , G02B6/0061 , G02B6/0078 , G02B6/0046 , G02B6/0055 , G02B6/0056 , G02B6/0068
摘要： An efficient, luminous and energy-saving panel-form illuminating system suitable for mass-production, comprising at least a photoconductor, a linear light source at one side of the photoconductor, and a reflector; wherein grooves or protrusions are formed on the bottom surface of the photoconductor.
摘要翻译：一种适用于批量生产的高效，发光和节能的面板式照明系统，包括至少一个光电导体，在感光体一侧的线性光源和反射器; 其中在感光体的底表面上形成有凹槽或凸起。

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