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51. 发明授权

US08529229B2 Ink jet printing apparatus 有权
标题翻译：喷墨打印设备
公开(公告)号：US08529229B2
公开(公告)日：2013-09-10
申请号：US11839914
申请日：2007-08-16
申请人： Yasuyuki Asai , Masaaki Matsuura
发明人： Yasuyuki Asai , Masaaki Matsuura
IPC分类号： F04B43/08 , F04B43/12
CPC分类号： B41J2/16532
摘要： A tube pump reduced of the burden against pump driving caused by dragging of a tube by a pressurizing roller. Specifically, guide members are disposed in the respective introduction portions at between the guides. Namely, the guide members are arranged nearby the extensions of the circumference of the arcuate guides and radially with respect to the center of the circumference. Due to this, the pump tube, the roller is to drag, is sustained by the guide member, to prevent the tube from increasing its deformation due to dragging. Thus, the tube can be prevented from being dragged in a manner forming a resistance to the roller. As a result, the pump motor, etc. can be prevented from being burdened with an increasing load.
摘要翻译：管泵减少了由加压辊拖动管造成的泵驱动的负担。具体地，引导构件设置在引导件之间的各个引导部分中。即，引导构件布置在弓形引导件的圆周的延伸部附近并且相对于圆周的中心径向地设置。由此，泵管，滚子被拖动，被引导构件保持，以防止管由于拖动而增加其变形。因此，可以防止以阻碍辊的方式拖动管。结果，可以防止泵电动机等因负载增加而负担。

52. 发明申请

US20130149124A1 TURBINE 有权
标题翻译：涡轮
公开(公告)号：US20130149124A1
公开(公告)日：2013-06-13
申请号：US13817893
申请日：2011-09-08
申请人： Yoshihiro Kuwamura , Kazuyuki Matsumoto , Hiroharu Oyama , Yoshinori Tanaka , Masaaki Matsuura , Asaharu Matsuo
发明人： Yoshihiro Kuwamura , Kazuyuki Matsumoto , Hiroharu Oyama , Yoshinori Tanaka , Masaaki Matsuura , Asaharu Matsuo
IPC分类号： F01D9/00
CPC分类号： F01D9/00 , F01D5/225 , F01D11/001 , F01D11/02 , F01D11/08 , F05D2220/31 , F16J15/4472
摘要： The turbine (1) according to the present invention includes: a blade body (50) having a blade (59) provided at one of a rotor rotatably supported and a stator provided around the rotor and extending in a radial direction toward the other side from one side and a shroud (51) extending in a circumferential direction at a tip portion in the radial direction of the blade (59); and an accommodating concave body (11) provided at the other of the rotor and the stator, extending in the circumferential direction, accommodating the shroud (51) with a gap (G) interposed therebetween, and relatively rotating with respect to the blade body (50), wherein leakage flow (L) leaked from main flow (M) flowing along the blade (59) flows into the gap (G); and wherein the shroud is provided with a guide curved surface formed between a peripheral surface (53C) facing the accommodating concave body (11) and a trailing edge end portion (56) formed closer to the main flow (M) side in a downstream of the leakage flow (L) than the peripheral surface (53C) in a downstream of the leakage flow (L), wherein a guide curved surface (57) is configured to guide the leakage flow (L) along the peripheral surface (53C) from the peripheral surface (53C) to the trailing edge end portion (56).
摘要翻译：根据本发明的涡轮机（1）包括：叶片体（50），其具有设置在可转动地支撑的转子中的一个叶片（59）和设置在转子周围的定子，并且沿径向朝向另一侧一侧和在所述叶片（59）的径向方向上的前端部沿圆周方向延伸的护罩（51）; 以及设置在所述转子和所述定子的另一侧的容纳凹体（11），其沿圆周方向延伸，以间隙（G）容纳所述罩（51），并相对于所述叶片体相对旋转 50），其中从所述叶片（59）流动的主流（M）泄漏的泄漏流（L）流入所述间隙（G）; 并且其中所述护罩设置有引导弯曲表面，所述引导弯曲表面形成在面向所述容纳凹形主体（11）的外周表面（53C）和在靠近所述主流（M）侧的下游侧形成的后缘端部所述泄漏流（L）比所述泄漏流（L）的下游侧的所述周面（53C）低，其特征在于，所述引导曲面（57）构成为沿着所述外周面（53C）引导所述泄漏流（L）所述周边表面（53C）到所述后缘端部（56）。

53. 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。

54. 发明授权

US07052149B2 Exterior vehicle mirror with auxiliary mirror having position marker indicating position of vehicle 失效
标题翻译：具有辅助镜的外部车辆后视镜具有指示车辆位置的位置标记
公开(公告)号：US07052149B2
公开(公告)日：2006-05-30
申请号：US10722476
申请日：2003-11-28
申请人： Hisaya Suzuki , Masaaki Matsuura , Masahiro Motomiya , Tohru Yamana
发明人： Hisaya Suzuki , Masaaki Matsuura , Masahiro Motomiya , Tohru Yamana
IPC分类号： B60R1/06 , B60R1/08 , G02B7/182
CPC分类号： B60R1/12 , B60R1/06 , B60R1/082 , B60R1/088 , B60R2001/1253 , B60R2001/1261
摘要： The present invention provides an outer mirrors installed in an automobile, that has a capability to be reset into a housing position, features to have auxiliary mirrors to percept and monitor the front wheels and thereabout, has a flexibility for well appreciated apparent design, has no reflection of head lamp lights of oncoming automobiles thereby and is capable to perform the function of the auxiliary mirror in the night or in the dark place. The outer mirror comprises a mirror base extending outward and a mirror housing, being capable to be reset into the housing position, suspended under the mirror base with a rotation capability thereunder and a separation distance from the automobile, wherein a first auxiliary mirror facing obliquely downward is attached to the mirror housing on the surface facing to the automobile body.
摘要翻译：本发明提供了一种安装在汽车中的外镜，其具有被复位到壳体位置的能力，具有用于感知和监视前轮及其附近的辅助镜的特征，具有良好的视觉设计的灵活性，没有因此，迎面而来的汽车的前灯的反射能够在夜间或暗处执行辅助镜的功能。外镜包括向外延伸的反射镜底座和能够被复位到壳体位置的反射镜壳体，其具有悬挂在镜座下面的旋转能力和与汽车的间隔距离，其中第一副镜面向下倾斜附着在面向汽车车身的表面上的镜壳体上。

55. 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。

56. 发明授权

US06808277B2 Inner mirror with built-in antenna 失效
标题翻译：内置内置天线
公开(公告)号：US06808277B2
公开(公告)日：2004-10-26
申请号：US10270012
申请日：2002-10-15
申请人： Masaaki Matsuura , Hidenori Sato
发明人： Masaaki Matsuura , Hidenori Sato
IPC分类号： G02B7182
CPC分类号： B60R1/04 , B60R2001/1261
摘要： The present invention provides an inner mirror with a built-in antenna in which an antenna angle remains unchanged regardless of adjustment of a mirror angle. The upper end of a stay 10 is mounted on a ceiling in a vehicle room. A pivot 14 is formed at the lower end of the stay 10. The pivot 14 is inserted into a mirror body 16 and fitted into a pivot supporting pmember 20 to support the mirror body 16 pivotally in three-dimensional directions. An antenna 34 is mounted on one side of the pivot 14 through shafts 28 and 30. Since the antenna 34 is mounted on the pivot 14, the angle of the antenna 34 remains unchanged, even though the mirror angle adjustment is performed by pivoting the mirror body 16.
摘要翻译：本发明提供一种具有内置天线的内部反射镜，其中天线角度保持不变，而与镜面角度的调节无关。支架10的上端安装在车室的天花板上。枢轴14形成在支柱10的下端。枢轴14被插入镜体16中并且装配到枢轴支撑件20中，以支撑镜体16在三维方向上枢转。天线34通过轴28和30安装在枢轴14的一侧上。由于天线34安装在枢轴14上，天线34的角度保持不变，即使通过使镜子枢转来执行镜面角度调节身体16。

57. 发明授权

US06701713B2 Pilot burner, premixing combustor, and gas turbine 有权
标题翻译：先导燃烧器，预混燃烧器和燃气轮机
公开(公告)号：US06701713B2
公开(公告)日：2004-03-09
申请号：US10195412
申请日：2002-07-16
申请人： Shigemi Mandai , Masaaki Matsuura , Keijirou Saitoh , Katsunori Tanaka , Wataru Akizuki
发明人： Shigemi Mandai , Masaaki Matsuura , Keijirou Saitoh , Katsunori Tanaka , Wataru Akizuki
IPC分类号： F02C726
CPC分类号： F23R3/343 , F23R3/14 , F23R3/286
摘要： A pilot nozzle diffusion-injects a fuel. A pilot swirler swirls a pilot air around the pilot nozzle. An air guide is arranged between the outer surface of the pilot nozzle and the pilot swirler. The air guide extends from the pilot swirler to a tip of the pilot nozzle. The air guide has a tip that protrudes beyond the tip of the pilot nozzle and this the tip of the air guide is bent away from a center of the pilot nozzle.
摘要翻译：先导喷嘴扩散 - 喷射燃料。先导式旋流器在引燃喷嘴周围旋转飞行员空气。在引导喷嘴的外表面和先导旋流器之间布置有空气引导件。空气引导器从先导旋流器延伸到先导喷嘴的尖端。空气引导件具有突出超过引导喷嘴的尖端的尖端，并且空气引导件的尖端远离引导喷嘴的中心弯曲。

58. 发明授权

US06419447B1 Gas turbine equipment and turbine blade 有权
标题翻译：燃气轮机设备和涡轮叶片
公开(公告)号：US06419447B1
公开(公告)日：2002-07-16
申请号：US09685950
申请日：2000-10-12
申请人： Koji Watanabe , Masaaki Matsuura , Kiyoshi Suenaga
发明人： Koji Watanabe , Masaaki Matsuura , Kiyoshi Suenaga
IPC分类号： F01D518
CPC分类号： F01D5/147 , F05D2230/10 , F05D2240/80 , F05D2260/94 , F05D2260/941
摘要： Turbine blade of gas turbine etc. and gas turbine equipment using the turbine blade suppress occurrence of thermal stress caused by temperature difference and provide high reliability. In gas turbine equipment comprising rotational portion of rotor (1) and moving blade (2), stationary portion of casing (3), stationary blade (4), various supporting members, etc. and combustor, thermal stress reducing portion is provided in any one or both of moving blade joint adjacent portion (14a) between moving blade trailing edge portion (14) and platform (15) and stationary blade joint adjacent portion (20a) between stationary blade trailing edge portion (20) and shroud (18, 19). By the thermal stress reducing portion, undesirable thermal stress occurring in the blade joint adjacent portions (14a, 20a) is reduced and reliability of the turbine blade and the gas turbine equipment is enhanced.
摘要翻译：燃气轮机等的涡轮叶片和使用涡轮叶片的燃气轮机设备抑制由温差引起的热应力的发生，并提供高可靠性。在包括转子（1）和活动叶片（2）的旋转部分的燃气轮机设备中，任何一种设置有壳体（3）的固定部分，固定叶片（4），各种支撑构件等以及燃烧室的热应力减小部分活动叶片后缘部分（14）和平台（15）之间的活动叶片接头相邻部分（14a）和固定叶片后缘部分（20）和护罩（18,19）之间的固定叶片接头相邻部分）。通过热应力减少部分，减少了在叶片接头相邻部分（14a，20a）中出现的不期望的热应力，并且提高了涡轮叶片和燃气轮机设备的可靠性。

59. 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。

60. 发明授权

US5561359A Discharge path for a battery compartment of an electric vehicle 失效
标题翻译：电动车辆电池仓的放电路径
公开(公告)号：US5561359A
公开(公告)日：1996-10-01
申请号：US224773
申请日：1994-04-08
申请人： Masaaki Matsuura , Masahiko Kuroki
发明人： Masaaki Matsuura , Masahiko Kuroki
IPC分类号： B60K1/00 , B60K1/04 , B60L11/18 , B62M7/02 , H01M2/10 , H01M2/12 , H01M10/60 , H01M10/615 , H01M10/625 , H01M10/647 , H01M10/6563 , H01M10/667 , H02J7/00 , H01M10/46 , B60R11/00 , B60R16/04
CPC分类号： B60L3/00 , B60K1/04 , H01M10/613 , H01M10/625 , H01M10/6556 , H01M10/6563 , H01M2/1083 , H02J7/0042 , B60L2200/12 , H01M2/12 , Y02T90/16
摘要： Concentration of hydrogen gas generated during a process of electrically recharging a battery of an electric vehicle is maintained by discharging the hydrogen gas during the process. An electric fan is installed inside a control unit box for accommodating a motor, an electric recharger and a control apparatus. The electric fan communicates ambient air to a motor through ducts. The air is further communicated to batteries through a duct and a nozzle member. Air directed by the electric fan during operation of the electric vehicle cools the motor driver and the motor. On the other hand, air communicated by the electric fan during a process of electrically recharging the batteries cools the electric recharger and then flows from the nozzle member to the batteries, blowing off hydrogen gas generated by the batteries during the electrical recharging process.
摘要翻译：通过在该过程中排出氢气来维持在对电动车辆的电池进行充电的过程中产生的氢气的浓度。电风扇安装在用于容纳电动机，充电器和控制装置的控制单元箱内。电风扇通过管道将环境空气连接到电机。空气通过管道和喷嘴构件进一步传递到电池。在电动车辆运行期间由电动风扇引导的空气冷却电动机驱动器和电动机。另一方面，在对电池进行再充电的过程中由电风扇连通的空气冷却电动充电器，然后从喷嘴构件流向电池，在充电过程中吹出由电池产生的氢气。

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