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1. 发明授权

US08079802B2 Gas turbine 有权
标题翻译：燃气轮机
公开(公告)号：US08079802B2
公开(公告)日：2011-12-20
申请号：US12164786
申请日：2008-06-30
申请人： Keita Takamura , Shinya Hashimoto , Masanori Yuri
发明人： Keita Takamura , Shinya Hashimoto , Masanori Yuri
IPC分类号： F01D5/14 , F03D11/00 , F04D29/38
CPC分类号： F02C7/141 , F01D5/085 , F01D5/087 , F05D2240/12 , F05D2240/61 , F05D2260/20
摘要： A gas turbine includes a shaft directional passage provided to a rotating member that rotates along a central axis of a rotor, which is a rotating axis of the rotating member, about the central axis, or a rotating axis of the rotating member, and in which cooling air flows along a direction of the rotating axis of the rotor, a plurality of radial directional passages provided in a circumferential direction of the rotating member, and compressing the cooling air by being provided outwardly from the center of the rotor, in which one end of each of the radial directional passages is communicated with the shaft directional passage and the other end is communicated with exterior of the rotating member.
摘要翻译：燃气轮机包括轴向通道，其设置在旋转部件上，该旋转部件沿着作为旋转部件的旋转轴线的转子的中心轴线，绕中心轴线或旋转部件的旋转轴线旋转，冷却空气沿着转子的旋转轴线的方向流动，多个径向通路设置在旋转构件的圆周方向上，并且通过从转子的中心向外设置来压缩冷却空气，其中一端每个径向通路与轴定向通道连通，另一端与旋转构件的外部连通。

2. 发明授权

US08079803B2 Gas turbine and cooling air supply structure thereof 有权
标题翻译：燃气轮机及其冷却空气供应结构
公开(公告)号：US08079803B2
公开(公告)日：2011-12-20
申请号：US12164793
申请日：2008-06-30
申请人： Keita Takamura , Shinya Hashimoto , Masanori Yuri
发明人： Keita Takamura , Shinya Hashimoto , Masanori Yuri
IPC分类号： F01D5/14 , F03D11/00 , F04D29/38
CPC分类号： F01D9/065 , F01D5/081 , F01D5/087 , F01D11/001 , F02C7/18 , F02C7/28
摘要： The present invention includes an introducing passage that is provided within a turbine stationary blade fixed within a turbine casing and that communicates an interior of the turbine casing with an exterior thereof; a nozzle that is provided in an inner circumference of the turbine stationary blade in a manner that the nozzle communicates with the introducing passage and that includes an outlet facing the opening of the rotor cavity and a swirler at the outlet; and a pressurizing passage that communicates a cooling passage with a rotor cavity. In this arrangement, the outlet of the nozzle and the connecting opening of the pressurizing passage are arranged so that distances of the outlet and of the connecting opening from the central axis line in the radial direction of the rotor are the same distance r.
摘要翻译：本发明包括一个引入通道，其设置在固定在涡轮机壳体内的涡轮机固定叶片内，并将涡轮机壳体的内部与其外部连通; 喷嘴，其以所述喷嘴与所述引导通道连通并且包括面向所述转子腔的开口的出口和所述出口处的旋流器的方式设置在所述涡轮静止叶片的内周中; 以及将冷却通路与转子腔连通的加压通路。在这种布置中，喷嘴的出口和加压通道的连接开口被布置成使得出口和连接开口在转子的径向方向上与中心轴线的距离是相同的距离r。

3. 发明申请

US20090324386A1 GAS TURBINE 有权
标题翻译：燃气轮机
公开(公告)号：US20090324386A1
公开(公告)日：2009-12-31
申请号：US12164786
申请日：2008-06-30
申请人： Keita Takamura , Shinya Hashimoto , Masanori Yuri
发明人： Keita Takamura , Shinya Hashimoto , Masanori Yuri
IPC分类号： F02C7/141
CPC分类号： F02C7/141 , F01D5/085 , F01D5/087 , F05D2240/12 , F05D2240/61 , F05D2260/20
摘要： A gas turbine includes a shaft directional passage provided to a rotating member that rotates along a central axis of a rotor, which is a rotating axis of the rotating member, about the central axis, or a rotating axis of the rotating member, and in which cooling air flows along a direction of the rotating axis of the rotor, a plurality of radial directional passages provided in a circumferential direction of the rotating member, and compressing the cooling air by being provided outwardly from the center of the rotor, in which one end of each of the radial directional passages is communicated with the shaft directional passage and the other end is communicated with exterior of the rotating member.
摘要翻译：燃气轮机包括轴向通道，其设置在旋转部件上，该旋转部件沿着作为旋转部件的旋转轴线的转子的中心轴线，绕中心轴线或旋转部件的旋转轴线旋转，冷却空气沿着转子的旋转轴线的方向流动，多个径向通路设置在旋转构件的圆周方向上，并且通过从转子的中心向外设置来压缩冷却空气，其中一端每个径向通路与轴定向通道连通，另一端与旋转构件的外部连通。

4. 发明授权

US08800300B2 Connection structure of exhaust chamber, support structure of turbine, and gas turbine 有权
标题翻译：排气室连接结构，涡轮支架结构和燃气轮机
公开(公告)号：US08800300B2
公开(公告)日：2014-08-12
申请号：US12919530
申请日：2009-01-27
申请人： Shinya Hashimoto , Kenichi Arase
发明人： Shinya Hashimoto , Kenichi Arase
IPC分类号： F02C7/20
CPC分类号： F02C7/20 , F01D25/28 , F01D25/30 , F05D2260/941
摘要： In a gas turbine, an exhaust casing and an exhaust chamber are connected by an exhaust chamber support that can absorb thermal expansion, and the exhaust chamber and an exhaust duct are connected by an exhaust duct support that can absorb thermal expansion. An insulator is mounted on an outer peripheral surface of the exhaust chamber, and the exhaust chamber support and the exhaust duct support are disposed outside the insulator in the form of a plurality of strips. Because the thermal stress at a connection portion of the exhaust chamber is reduced, the durability is enhanced.
摘要翻译：在燃气轮机中，通过能够吸收热膨胀的排气室支撑体将排气室和排气室连接，排气室和排气管通过可吸收热膨胀的排气管道支撑体相连接。绝缘体安装在排气室的外周表面上，排气室支撑件和排气管道支撑件以多个条的形式设置在绝缘体的外侧。由于排气室的连接部的热应力降低，所以耐久性提高。

5. 发明授权

US08638317B2 Display apparatus and method for controlling the same 有权
标题翻译：显示装置及其控制方法
公开(公告)号：US08638317B2
公开(公告)日：2014-01-28
申请号：US12048088
申请日：2008-03-13
申请人： Tsutomu Harada , Shinya Hashimoto , Naoya Okada , Tadashi Maekawa , Kazunori Yamguchi , Mitsuru Tateuchi , Ryoichi Tsuzaki , Yoshiharu Nakajima , Chiaki Kon
发明人： Tsutomu Harada , Shinya Hashimoto , Naoya Okada , Tadashi Maekawa , Kazunori Yamguchi , Mitsuru Tateuchi , Ryoichi Tsuzaki , Yoshiharu Nakajima , Chiaki Kon
IPC分类号： G06F3/042 , G06F3/041 , G09G5/00 , G06F3/038 , G06K11/06 , G08C21/00 , G06K9/40
CPC分类号： G06F1/3203 , G02F1/13338 , G02F2001/13312 , G06F3/0412 , G06F3/042
摘要： Disclosed herein is a display apparatus including: a display panel having a display function and a light-receiving/imaging function; a first image processing section configured to generate a detection signal that indicates whether a to-be-detected object has been detected based on a result of first image processing performed on an image taken by the light-receiving/imaging function; a second image processing section configured to perform second image processing on the image processed by the first image processing section, the second image processing having a heavier processing load than the first image processing; and a control section configured to control an operation of the second image processing section in accordance with the detection signal generated by the first image processing section, and, when it is determined that the processing by the second image processing section is not necessary, control the second image processing section to enter a sleep state.
摘要翻译：这里公开了一种显示装置，包括：具有显示功能和受光/成像功能的显示面板; 第一图像处理部，被配置为基于对由所述光接收/成像功能拍摄的图像执行的第一图像处理的结果生成指示是否已经检测到被检测对象的检测信号; 第二图像处理部，被配置为对由所述第一图像处理部处理的图像执行第二图像处理，所述第二图像处理具有比所述第一图像处理更重的处理负荷; 以及控制部，被配置为根据由第一图像处理部生成的检测信号来控制第二图像处理部的操作，并且当确定不需要第二图像处理部的处理时，控制第二图像处理部分进入睡眠状态。

6. 发明申请

US20120163963A1 STRUCTURE FOR GAS TURBINE CASING 有权
标题翻译：燃气轮机结构
公开(公告)号：US20120163963A1
公开(公告)日：2012-06-28
申请号：US13383637
申请日：2010-09-09
申请人： Yukihiro Hashimoto , Shinya Hashimoto
发明人： Yukihiro Hashimoto , Shinya Hashimoto
IPC分类号： F01D25/24
CPC分类号： F01D25/243 , F05D2240/55 , F05D2260/941
摘要： A structure for a gas turbine casing, capable of preventing gas from leaking when the structure is subjected to pressure. A structure for a gas turbine casing, divided by a horizontal plane at flange sections into two halves comprising an upper-half casing (10) and a lower-half casing (11). The structure is provided with bolts (12) which are disposed in the inner surfaces of the upper-half casing (10) and the lower-half casing (11) so as to bridge therebetween, upper nuts (13) which are disposed in the inner surface of the upper-half casing (10) and attached to the bolts (12), and lower nuts (14) which are disposed in the inner surface of the lower-half casing (11) and attached to the bolts (12).
摘要翻译：一种用于燃气轮机壳体的结构，能够防止当结构受到压力时气体泄漏。一种用于燃气涡轮机壳体的结构，其由凸缘部分处的水平面划分为包括上半壳体（10）和下半壳体（11）的两半。该结构设置有螺栓（12），其设置在上半壳体（10）和下半壳体（11）的内表面中以便在其之间桥接，上螺母（13）设置在上半壳体（10）的内表面并附接到螺栓（12），下螺母（14）设置在下半壳体（11）的内表面中并附接到螺栓（12）上，。

7. 发明授权

US08011717B2 Automotive interior component 有权
标题翻译：汽车内饰件
公开(公告)号：US08011717B2
公开(公告)日：2011-09-06
申请号：US12396543
申请日：2009-03-03
申请人： Toyokazu Endo , Masahiko Hara , Hiroyuki Kojima , Sumiaki Tanaka , Shinya Hashimoto , Noriyuki Koike
发明人： Toyokazu Endo , Masahiko Hara , Hiroyuki Kojima , Sumiaki Tanaka , Shinya Hashimoto , Noriyuki Koike
IPC分类号： B60J5/04 , B60R21/02
CPC分类号： B60J5/0451 , B60R21/0428 , B60R2021/0039
摘要： There is provided an automotive interior component including an impact absorber mounted to an interior side of a side wall panel of a vehicle, and the shape and structure of the impact absorber that can undergo buckling deformation and absorb an impact load in a side collision are improved to increase an impact absorbing function. The impact absorber 30 mounted on a back surface of an impact area IA in the automotive interior component (door trim) 10 is formed as a hollow box body having an opening 31 on one side and a bottom surface wall 32 on the other side, and improvement such as providing corner cut portions 34 at four corner portions of the bottom surface wall 32, forming a chamfered portion 333 at a corner portion of a side wall 33, or forming a cam groove portion 334, a triangular rib 36, or an inner surface rib 321 is made to adjust a reaction force in a side collision to increase an impact absorbing function.
摘要翻译：提供了一种汽车内部部件，其包括安装在车辆的侧壁面板的内侧的冲击吸收件，并且能够经受弯曲变形并且吸收侧面碰撞中的冲击载荷的冲击吸收体的形状和结构得到改善以增加冲击吸收功能。安装在汽车内部部件（车门装饰件）10中的冲击区域IA的后表面上的冲击吸收器30形成为具有一侧的开口31和另一侧的底壁32的中空箱体，在底壁32的四个角部设置角部切割部34，在侧壁33的角部形成倒角部333，或形成凸轮槽部334，三角肋36，内侧制造表面肋321以调节侧面碰撞中的反作用力，以增加冲击吸收功能。

8. 发明申请

US20110020116A1 GAS TURBINE 有权
标题翻译：燃气轮机
公开(公告)号：US20110020116A1
公开(公告)日：2011-01-27
申请号：US12933636
申请日：2009-01-08
申请人： Shinya Hashimoto , Kenichi Arase
发明人： Shinya Hashimoto , Kenichi Arase
IPC分类号： F01D5/08
CPC分类号： F01D25/12 , F01D9/065 , F01D25/162 , F01D25/26 , F01D25/30 , F02C7/18
摘要： A gas turbine including exhaust chamber defined by a cylindrical casing wall and a bearing case that supports a bearing part of a rotor in the casing wall, struts provided at equal intervals in circumferential direction of the bearing case and extending in tangential direction of the bearing case to couple the casing wall and the bearing case, a diffuser unit having an outer diffuser at the inner periphery of the casing wall and an inner diffuser at the outer periphery of the bearing case, a cooling chamber in which the outer diffuser and the inner diffuser are coupled by a strut cover, led to a portion between the casing wall and the outer diffuser, a portion between the bearing case and the inner diffuser, and the insides of the strut cover, and a partition wall that covers the outer periphery of the bearing case.
摘要翻译：一种燃气轮机，包括由圆柱形壳体壁限定的排气室和支撑壳体中的转子的轴承部分的轴承箱，在轴承箱的圆周方向上以等间隔设置的支撑件，并在轴承箱的切线方向上延伸联接壳体壁和轴承箱，在壳体壁的内周具有外扩散器的扩散器单元和在轴承箱的外周处的内扩散器，其中外扩散器和内扩散器通过支柱盖连接，导致壳体壁和外部扩散器之间的部分，轴承壳体和内部扩散器之间的部分以及支柱盖的内部，以及覆盖外部扩散器的外周的分隔壁轴承箱。

9. 发明申请

US20110005234A1 CONNECTION STRUCTURE OF EXHAUST CHAMBER, SUPPORT STRUCTURE OF TURBINE, AND GAS TURBINE 有权
标题翻译：排气室连接结构，涡轮支撑结构和气体涡轮
公开(公告)号：US20110005234A1
公开(公告)日：2011-01-13
申请号：US12919530
申请日：2009-01-27
申请人： Shinya Hashimoto , Kenichi Arase
发明人： Shinya Hashimoto , Kenichi Arase
IPC分类号： F02C7/20
CPC分类号： F02C7/20 , F01D25/28 , F01D25/30 , F05D2260/941
摘要： In a gas turbine, an exhaust casing (27) and an exhaust chamber (14) are connected by an exhaust chamber support (32) that can absorb thermal expansion, and the exhaust chamber (14) and an exhaust duct (31) are connected by an exhaust duct support (33) that can absorb thermal expansion. An insulator (63) is mounted on an outer peripheral surface of the exhaust chamber (14), and the exhaust chamber support (32) and the exhaust duct support (33) are disposed outside the insulator (63) in the form of a plurality of strips. Because the thermal stress at a connection portion of the exhaust chamber is reduced, the durability is enhanced.
摘要翻译：在燃气轮机中，排气室（27）和排气室（14）通过可以吸收热膨胀的排气室支撑（32）连接，排气室（14）和排气管（31）连接通过可以吸收热膨胀的排气管道支撑件（33）。绝缘体（63）安装在排气室（14）的外周面上，排气室支撑件（32）和排气管道支撑件（33）以多个形式设置在绝缘体（63）的外侧的条。由于排气室的连接部的热应力降低，所以耐久性提高。

10. 发明申请

US20100326039A1 GAS TURBINE, DISK, AND METHOD FOR FORMING RADIAL PASSAGE OF DISK 审中-公开
标题翻译：用于形成盘片径向通气的气体涡轮，盘和方法
公开(公告)号：US20100326039A1
公开(公告)日：2010-12-30
申请号：US12865641
申请日：2008-12-24
申请人： Kenichi Arase , Shinya Hashimoto
发明人： Kenichi Arase , Shinya Hashimoto
IPC分类号： F02C3/00 , B23P17/00
CPC分类号： F01D5/081 , F01D5/087 , F05D2230/10 , F05D2250/14 , F05D2250/314 , F05D2260/941 , Y10T29/49229
摘要： A gas turbine includes a disk rotatable about a rotational axis, when turbine rotor blades for receiving combustion gas obtained by burning fuel are connected to the side periphery, and energy of the combustion gas received by the turbine rotor blades is transmitted, and a radial passage that, in a cross-section at a virtual curved plane that is a curved plane about the rotational axis and in which distances from all points on the curved plane to the rotational axis are all equal, is a hole formed to include a portion having a shape in which the length in the circumferential direction of the disk is longer than the length in the direction parallel to the rotational axis, and is formed in the disk from the side of the rotational axis toward the outside of the disk.
摘要翻译：燃气轮机包括可绕旋转轴线旋转的盘，当用于接收燃烧燃料获得的燃烧气体的涡轮转子叶片连接到侧边缘时，由涡轮转子叶片接收的燃烧气体的能量传递，并且径向通道在作为围绕旋转轴线的弯曲平面的虚拟弯曲平面的横截面中，其中从弯曲平面上的所有点到旋转轴线的距离全部相等，是形成为包括具有其中盘的圆周方向的长度比平行于旋转轴的方向的长度长，并且从旋转轴的侧面朝向盘的外侧形成在盘中。

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