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    • 41. 发明授权
    • Gas turbine blade
    • 燃气轮机叶片
    • US06257830B1
    • 2001-07-10
    • US09230983
    • 1999-06-02
    • Masaaki MatsuuraKiyoshi SuenagaSunao AokiKazuo UematsuHiroki FukunoYasuoki Tomita
    • Masaaki MatsuuraKiyoshi SuenagaSunao AokiKazuo UematsuHiroki FukunoYasuoki Tomita
    • F01D518
    • F01D5/147F01D5/187F05D2260/2322
    • In a steam cooling system proposed heretofore, high-pressure steam is supplied into an internal space of a blade for effecting cooling thereof with the high-pressure steam to thereby recover heat energy. This system however suffers from problems concerning the strength of the blade and the like. The present invention solves these problems and provides a gas-turbine blade which does not suffer from problems concerning the strength thereof nor problems concerning the flow of high-pressure steam. To this end, a coolant flow passage is formed within the blade extending in the longitudinal direction of the blade, and reinforcing ribs which interconnects a dorsal wall and a ventral wall of the blade is disposed within the coolant flow passage so as to extend in the flow direction of the coolant. Hence, the strength of the blade can be ensured without any obstacle to the flow of the coolant.
    • 在迄今为止提出的蒸汽冷却系统中,将高压蒸汽供应到叶片的内部空间中,以利用高压蒸汽冷却,从而回收热能。 然而,该系统存在关于叶片等的强度的问题。 本发明解决了这些问题,提供了一种不存在与强度相关的问题的燃气轮机叶片,也不会涉及高压蒸汽的流动问题。 为此,在刀片的纵向延伸的叶片内形成冷却剂流动通道,并且将与叶片的背壁和腹壁相互连接的加强筋设置在冷却剂流动通道内,以便在 冷却液的流动方向。 因此,可以确保叶片的强度,而不会妨碍冷却剂的流动。
    • 42. 发明授权
    • Steam-cooling type gas turbine
    • 蒸汽式燃气轮机
    • US06224327B1
    • 2001-05-01
    • US09250733
    • 1999-02-16
    • Sunao AokiKatsunori TanakaKazuharu HirokawaRintaro Chikami
    • Sunao AokiKatsunori TanakaKazuharu HirokawaRintaro Chikami
    • F04D2958
    • F01D5/085F02C7/16F05D2260/2322
    • A steam-cooling gas turbine in which cooling steam is fed from a center portion of a rotating shaft and recovered through passages disposed at the outer side of the center portion with steam leaking through a seal portion from a feeding steam being effectively recovered. Feed steam (30) serving as coolant is supplied to a cavity (27) from a inner cylinder (10) and hence fed to moving blades (11, 12) through recesses (40) formed in a coupling portion (26) interposed between a final-stage disk (24) and a turbine shaft (1), steam feeding pipes (15) and steam feeding passages (11a, 12a). After cooling of the moving blades, steam (31) is recovered through steam recovering passages (11b, 12b), steam recovering pipes (16), radial steam-recovering passages (17), axial steam-recovering passages (18) and outlet openings (5a). The coupling portion (26) is forced to hermetically close under thermal stress, whereby leakage of the feed steam (30) is prevented. Steam leaking through a seal portion constituted by stationary and rotatable seal fin assemblies (4a, 4b) can be effectively recovered. The inner cylinder (10) can move in the axial direction through cooperation of piston rings (43) and a centering piece (6) adapted for absorbing thermal stress induced in the inner cylinder (10). Upstream tip end portions of steam feeding pipes (15) and steam recovering pipes (16) are secured onto a side surface of the first-stage disk (21) through sleeves removably fitted thereto.
    • 一种蒸汽冷却燃气轮机,其中冷却蒸汽从旋转轴的中心部分进给并通过设置在中心部分的外侧的通道被回收,蒸汽通过密封部分从进料蒸汽泄漏得到有效回收。 作为冷却剂的进料蒸汽(30)从内筒(10)供给到空腔(27),从而通过形成在连接部分(26)中的连接部分(26)的凹部(40)供给到活动叶片(11,12) 末级盘(24)和涡轮轴(1),蒸汽供给管(15)和蒸汽供给通道(11a,12a)。 在运动叶片冷却后,蒸汽(31)通过蒸汽回收通道(11b,12b),蒸汽回收管(16),径向蒸汽回收通道(17),轴向蒸汽回收通道(18)和出口 (5a)。 耦合部分(26)在热应力下被迫气密地闭合,从而防止进料蒸汽(30)的泄漏。 可以有效地回收通过由固定和可旋转的密封翅片组件(4a,4b)构成的密封部分泄漏的蒸汽。 内筒(10)可以通过活塞环(43)和适于吸收在内筒(10)中感应的热应力的定心件(6)的配合而沿轴向移动。 蒸汽供给管(15)和蒸汽回收管(16)的上游末端部分通过可移除地装配在其上的套筒固定在第一级盘(21)的侧表面上。
    • 45. 发明授权
    • Gas turbine tip shroud blade cavity
    • 燃气涡轮机顶端护罩叶片腔
    • US6068443A
    • 2000-05-30
    • US23566
    • 1998-02-13
    • Sunao AokiEisaku Ito
    • Sunao AokiEisaku Ito
    • F01D5/20F01D5/22F01D11/02F01D11/08F02C7/28
    • F01D5/225F01D11/08
    • The invention relates to a cavity constituted by a casing of a gas turbine and a moving blade with a tip shroud, by which a cavity space is made to a necessary minimum size, a main flow gas is prevented from being entrained and a pressure loss is reduced. A tip shroud (6) is mounted on a tip end portion of a moving blade (4), a fin (7) is mounted thereon, a recess-like cavity (15) narrower than the conventional one is formed by portions (12a) and (12b) of a casing (12) and the fin (7), and further a projecting portion (16) is provided to an upstream end portion of the tip shroud (6). The projecting portion (16) is at a position (13a) at a time of a cold start and is at a position (13b) at a time of a hot start run, even if a thermal expansion occurs, thus the projecting portion (16) is not in contact with the recess portion, a main flow gas (1) is less entrained within the cavity (15), and a pressure loss is reduced because of no swirl, so that a performance of the gas turbine is enhanced.
    • 本发明涉及一种由燃气轮机的壳体和具有尖端护罩的活动叶片构成的空腔,通过该空腔将腔空间制成所需的最小尺寸,防止主流动气体夹带,压力损失为 减少 尖端护罩(6)安装在活动叶片(4)的前端部分上,其上安装有翅片(7),比现有技术的凹部(15)窄,部分(12a)形成, 和壳体(12)和翅片(7)的另一个突出部分(16),并且在尖端罩(6)的上游端部设置有突出部分(16)。 即使发生热膨胀,突出部16在冷启动时处于位置(13a),并且在热启动时处于位置(13b),因此突出部16 )不与凹部接触,主流动气体(1)较少夹带在空腔(15)内,并且由于没有涡流而导致压力损失降低,从而提高了燃气轮机的性能。
    • 49. 发明授权
    • Stereoscopic imaging apparatus
    • 立体成像装置
    • US08639109B2
    • 2014-01-28
    • US13365053
    • 2012-02-02
    • Sunao AokiMasahiro Yamada
    • Sunao AokiMasahiro Yamada
    • G03B35/00H04N13/02
    • H04N5/23212H04N13/204H04N13/239H04N13/243
    • A stereoscopic imaging apparatus includes: an objective optical system that forms a subject as a real or virtual image. Light beams of the subject, emitted in different paths of the objective optical system by independent optical systems, are imaged again as a parallax image, which is converted into an image signal. A control unit moves a front-side principal point of each of the imaging optical systems, so that the ratio of the length of a perpendicular line from that front-side principal point to the optical axis of the objective optical system with respect to the length of a line connecting the point at which the perpendicular line and the optical axis intersect and the focal point of the objective optical system becomes constant.
    • 立体成像装置包括:将物体形成为实像或虚像的物镜光学系统。 通过独立光学系统在物镜光学系统的不同路径中发射的被摄体的光束被再次成像为视差图像,其被转换为图像信号。 控制单元移动每个成像光学系统的前侧主点,使得从该前侧主点到目标光学系统的光轴的垂直线的长度相对于长度 连接垂直线和光轴相交的点与物镜光学系统的焦点的线变得恒定。
    • 50. 发明申请
    • SPATIAL IMAGE DISPLAY DEVICE
    • 空间图像显示装置
    • US20120002023A1
    • 2012-01-05
    • US13143031
    • 2010-01-18
    • Masahiro YamadaSunao Aoki
    • Masahiro YamadaSunao Aoki
    • H04N13/04
    • G03B35/18G02B26/004G02B27/2214H04N13/302H04N13/305H04N13/307H04N13/315H04N13/324H04N13/354
    • Provided is a spatial image display device capable of forming more natural spatial images even with a simple configuration. In the spatial image display device 10, a two-dimensional display image corresponding to a video signal is generated by a display section 2. Display image light corresponding to one group of pixels 22 in the display section 2 is collectively subjected to wavefront transformation and collectively deflected by one liquid optical element 41 corresponding to that one group of pixels 22. Therefore, compared with a case where one liquid optical element 41 is provided for one pixel 22, a larger number of various different two-dimensional display image light are to be emitted all at once toward different directions in the horizontal plane, without increasing the frame rate in the display section 2.
    • 提供了即使以简单的配置也能够形成更自然的空间图像的空间图像显示装置。 在空间图像显示装置10中,通过显示部2生成与视频信号对应的二维显示图像。显示部2中的与一组像素22对应的图像光被共同地进行波前变换 由与一组像素22相对应的一个液体光学元件41偏转。因此,与为一个像素22设置一个液体光学元件41的情况相比,更多数量的各种不同的二维显示图像光将被 一次在水平面上向不同方向发射,而不增加显示部分2中的帧速率。