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1. 发明授权

US07694522B2 Heat exchanging wall, gas turbine using the same, and flying body with gas turbine engine 有权
标题翻译：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：US07694522B2
公开(公告)日：2010-04-13
申请号：US10912565
申请日：2004-08-06
申请人： Tomoyoshi Nakae , Kenichiro Takeishi , Masaaki Matsuura , Tsuyoshi Kitamura , Atsushi Moriwaki
发明人： Tomoyoshi Nakae , Kenichiro Takeishi , Masaaki Matsuura , Tsuyoshi Kitamura , Atsushi Moriwaki
IPC分类号： F02C1/00 , F02G3/00
CPC分类号： F23R3/002 , F23R3/005 , F23R2900/03043 , F28F3/02 , F28F3/022 , F28F13/12 , Y02T50/675
摘要： 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 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 1/10 of the height of the first protrusion in the normal direction.
摘要翻译：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第一突起的高度在正常方向的1/20和1/4之间。更优选地，第二突起在法线方向上的高度是第一突起在法线方向上的高度的1/10。

2. 发明申请

US20050047932A1 Heat exchanging wall, gas turbine using the same, and flying body with gas turbine engine 有权
标题翻译：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
申请人： Tomoyoshi Nakae , Kenichiro Takeishi , Masaaki Matsuura , Tsuyoshi Kitamura , Atsushi Moriwaki
发明人： Tomoyoshi Nakae , Kenichiro Takeishi , Masaaki Matsuura , Tsuyoshi Kitamura , Atsushi Moriwaki
IPC分类号： F23R3/00 , F04B23/00
CPC分类号： F23R3/002 , F23R3/005 , F23R2900/03043 , F28F3/02 , F28F3/022 , F28F13/12 , Y02T50/675
摘要： 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.
摘要翻译：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。

3. 发明授权

US07300251B2 Turbine cooling vane of gas turbine engine 有权
标题翻译：燃气轮机的涡轮冷却叶片
公开(公告)号：US07300251B2
公开(公告)日：2007-11-27
申请号：US10544844
申请日：2004-03-03
申请人： Tsuyoshi Kitamura , Kenichiro Takeishi , Masaaki Matsuura , Ryoma Nogami
发明人： Tsuyoshi Kitamura , Kenichiro Takeishi , Masaaki Matsuura , Ryoma Nogami
IPC分类号： F01D5/18
CPC分类号： F01D5/189 , F01D5/186 , F05D2260/201 , Y02T50/676
摘要： 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.
摘要翻译：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。

4. 发明申请

US20060210399A1 Turbine cooling vane of gas turbine engine 有权
标题翻译：燃气轮机的涡轮冷却叶片
公开(公告)号：US20060210399A1
公开(公告)日：2006-09-21
申请号：US10544844
申请日：2004-03-03
申请人： Tsuyoshi Kitamura , Kenichiro Takeishi , Masaaki Matsuura , Ryoma Nogami
发明人： Tsuyoshi Kitamura , Kenichiro Takeishi , Masaaki Matsuura , Ryoma Nogami
IPC分类号： F01D5/18
CPC分类号： F01D5/189 , F01D5/186 , F05D2260/201 , Y02T50/676
摘要： 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.
摘要翻译：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。

5. 发明授权

US06290462B1 Gas turbine cooled blade 有权
标题翻译：燃气轮机冷却叶片
公开(公告)号：US06290462B1
公开(公告)日：2001-09-18
申请号：US09272559
申请日：1999-03-19
申请人： Tatsuo Ishiguro , Koji Watanabe , Masaaki Matsuura , Kenichiro Takeishi , Junichiro Masada , Yasuoki Tomita , Kiyoshi Suenaga
发明人： Tatsuo Ishiguro , Koji Watanabe , Masaaki Matsuura , Kenichiro Takeishi , Junichiro Masada , Yasuoki Tomita , Kiyoshi Suenaga
IPC分类号： F01D1100
CPC分类号： F01D5/187 , F05D2250/185 , F05D2260/2212
摘要： A gas turbine cooled blade is constructed without an increase in the number of parts or time requirements, in which seal air is maintained at a lower temperature with the heat exchange rate being suppressed, and the heat transfer rate of the cooling medium in cooling passage is enhanced. A plurality of cooling passages (A, B, C, D, E) is provided in a blade, and the first row cooling passage (A) is covered at the blade inner and outer peripheries and communicates with the second row cooling passage (B) through communication holes (6) and with the main flow gas path through film cooling holes (7). The second row cooling passage (B) communicates with the blade inner peripheral cavity (10) to form a seal air supply passage. A plurality of ribs (31) are disposed on the inner wall of cooling passage (22) with a predetermined pitch (P). The ribs are arranged alternately and are inclined against cooling medium flow with respective higher first end contacting lower side faces of an immediately upstream rib at a position on both side portions of cooling passage (22). High heat transfer rate areas are formed on both side portions of cooling passage (22), and the average heat transfer rate in cooling passage is enhanced.
摘要翻译：在不增加部件或时间要求的情况下构建燃气轮机冷却叶片，其中密封空气在热交换率被抑制下保持在较低温度，并且冷却通道中的冷却介质的传热速率为增强。多个冷却通道（A，B，C，D，E）设置在叶片中，第一排冷却通道（A）被覆盖在叶片的内周和外周，并与第二排冷却通道）通过连通孔（6）并且主流动气体通道通过膜冷却孔（7）。第二排冷却通道（B）与叶片内周腔（10）连通，形成密封空气供给通道。多个肋（31）以预定的间距（P）设置在冷却通道（22）的内壁上。这些肋交替布置并且相对于冷却介质流倾斜，并且在冷却通道（22）的两侧部分的位置处，相应较高的第一端接触紧紧上游的肋的下侧面。在冷却通道（22）的两侧形成有高的传热率区域，并且冷却通路的平均传热率提高。

6. 发明授权

US08061804B2 Printing apparatus and printing apparatus control method 有权
标题翻译：印刷装置和印刷装置的控制方法
公开(公告)号：US08061804B2
公开(公告)日：2011-11-22
申请号：US12333286
申请日：2008-12-11
申请人： Atsushi Shimizu , Masaaki Matsuura , Tsuyoshi Otani , Ken Hoshino
发明人： Atsushi Shimizu , Masaaki Matsuura , Tsuyoshi Otani , Ken Hoshino
IPC分类号： B41J2/165
CPC分类号： B41J29/38 , B41J2/16511
摘要： A method of moving a cap apart from a printhead within a short period of time without damaging a printing apparatus when the cap sticks to the printhead. A cap moving unit is driven to try to move the cap apart from the printhead. When a detection unit for detecting that the cap has moved apart from the printhead detects that the cap has not moved apart from the printhead, it is controlled to slightly reciprocate the carriage while driving the cap moving unit. When the detection unit detects that the cap has moved apart from the printhead under this control, the slight reciprocation of the carriage is forcibly stopped.
摘要翻译：一种在短时间内将盖从打印头分开移动而不会在盖子粘附到打印头时损坏打印装置的方法。驱动盖移动单元以尝试将盖从打印头分开移动。当用于检测盖已经从打印头移开的检测单元检测到盖没有从打印头移开时，控制其在驱动盖移动单元的同时使托架稍微往复运动。当在该控制下检测单元检测到盖已经从打印头移开时，滑架的轻微往复运动被强制停止。

7. 发明授权

US07764432B2 Laser equipment 失效
标题翻译：激光设备
公开(公告)号：US07764432B2
公开(公告)日：2010-07-27
申请号：US11922230
申请日：2006-04-27
申请人： Hirofumi Miyajima , Hirofumi Kan , Takayuki Uchiyama , Masaaki Matsuura , Toshimasa Matsuno
发明人： Hirofumi Miyajima , Hirofumi Kan , Takayuki Uchiyama , Masaaki Matsuura , Toshimasa Matsuno
IPC分类号： G02B27/14 , G02B27/10
CPC分类号： B23K26/0732 , B23K26/0604 , B23K26/0608 , B23K2101/18 , B23K2103/04 , G02B19/0014 , G02B19/0057 , G02B27/0927 , H01S5/005 , H01S5/02252 , H01S5/4012 , H01S5/405
摘要： A laser apparatus (10) has a plurality of light sources (11a to 11c) that include laser array stacks (12a to 12c). Laser beams (32b, 32c) are respectively deflected by a slit mirror (14) and a polarizing beam splitter (16) and synthesized with other laser beams (32a). These laser beams have optical axes that are inclined with respect to each other and slow axis directions that are mutually parallel. A converging optical system (20) converges the laser beams from the respective light sources at positions that are separated along a direction perpendicular to the slow axis directions.
摘要翻译：激光装置（10）具有包括激光阵列（12a〜12c）的多个光源（11a〜11c）。激光束（32b，32c）分别由狭缝镜（14）和偏振分束器（16）偏转并与其它激光束（32a）合成。这些激光束具有彼此相对倾斜的光轴和相互平行的慢轴方向。会聚光学系统（20）将来自各个光源的激光束沿垂直于慢轴方向的方向分离的位置会聚。

8. 发明申请

US20060132944A1 VEHICLE SIDE MIRROR ASSEMBLY WITH REARWARD AND FORWARD VIEWING 失效
标题翻译：车辆侧面镜组件具有后期和前瞻性查看
公开(公告)号：US20060132944A1
公开(公告)日：2006-06-22
申请号：US11239216
申请日：2005-09-30
申请人： Masaaki Matsuura , Masahiro Motomiya , Hisaya Suzuki
发明人： Masaaki Matsuura , Masahiro Motomiya , Hisaya Suzuki
IPC分类号： G02B7/182
CPC分类号： B60R1/10 , B60R1/06 , B60R1/082
摘要： Disclosed is an outer mirror in which individual components are easy to assemble and which is superior in durability. An outer mirror includes a mirror base having a protrusion which sticks out outward from a side face of a vehicle body, a shaft being placed on the protrusion, and a mirror housing being coupled to the shaft in a rotatable fashion. Furthermore, the mirror housing includes a mirror for showing an area behind the vehicle body, and an opening on its side that faces the vehicle body.
摘要翻译：公开了一种外镜，其中各个部件易于组装，并且其耐久性优异。外反射镜包括具有突出部的反射镜基座，该突起从车身的侧面向外突出，轴被放置在突起上，反射镜壳体以可旋转的方式联接到轴。此外，镜壳体包括用于显示车体后面的区域的反射镜和面向车体的侧面上的开口。

9. 发明授权

US07055974B1 Vehicle side mirror assembly with rearward and forward viewing 失效
标题翻译：车辆后视镜组件具有向后和向前观察
公开(公告)号：US07055974B1
公开(公告)日：2006-06-06
申请号：US11239216
申请日：2005-09-30
申请人： Masaaki Matsuura , Masahiro Motomiya , Hisaya Suzuki
发明人： Masaaki Matsuura , Masahiro Motomiya , Hisaya Suzuki
IPC分类号： G02B5/08 , B60R1/08 , B60R1/10
CPC分类号： B60R1/10 , B60R1/06 , B60R1/082
摘要： Disclosed is an outer mirror in which individual components are easy to assemble and which is superior in durability. An outer mirror includes a mirror base having a protrusion which sticks out outward from a side face of a vehicle body, a shaft being placed on the protrusion, and a mirror housing being coupled to the shaft in a rotatable fashion. Furthermore, the mirror housing includes a mirror for showing an area behind the vehicle body, and an opening on its side that faces the vehicle body.
摘要翻译：公开了一种外镜，其中各个部件易于组装，并且其耐久性优异。外反射镜包括具有突出部的反射镜基座，该突起从车身的侧面向外突出，轴被放置在突起上，反射镜壳体以可旋转的方式联接到轴。此外，镜壳体包括用于显示车体后面的区域的反射镜和面向车体的侧面上的开口。

10. 发明授权

US06257830B1 Gas turbine blade 有权
标题翻译：燃气轮机叶片
公开(公告)号：US06257830B1
公开(公告)日：2001-07-10
申请号：US09230983
申请日：1999-06-02
申请人： Masaaki Matsuura , Kiyoshi Suenaga , Sunao Aoki , Kazuo Uematsu , Hiroki Fukuno , Yasuoki Tomita
发明人： Masaaki Matsuura , Kiyoshi Suenaga , Sunao Aoki , Kazuo Uematsu , Hiroki Fukuno , Yasuoki Tomita
IPC分类号： F01D518
CPC分类号： F01D5/147 , F01D5/187 , F05D2260/2322
摘要： 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.
摘要翻译：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。

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