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公开(公告)号：US06889495B2
公开(公告)日：2005-05-10
申请号：US10382877
申请日：2003-03-07
申请人： Shigeru Hayashi , Hideshi Yamada
发明人： Shigeru Hayashi , Hideshi Yamada
IPC分类号： F23R3/18 , F23D14/70 , F23R3/12 , F23R3/14 , F23R3/20 , F23R3/28 , F23R3/32 , F23R3/34 , F23R3/30
CPC分类号： F23R3/283 , F23D14/70 , F23D2209/20 , F23R3/14 , F23R3/20 , Y02T50/675
摘要： The present invention provides a gas turbine combustor which makes it possible to achieve both a high combustion efficiency and low NOx emissions characteristics over a wide output power range without using a device that can vary the flow rate of the air used for combustion, by burning a lean mixture using high-temperature burned gas. The gas turbine combustor 10 comprises pre-mixture injection tubes 16 which conduct a mixture of fuel and air into a combustion chamber 11. The mixture from the pre-mixture injection tubes 16 is injected toward burned gas 19a present on the downstream side of the flame 19, which is injected from burners 15 that open into the combustion chamber 11, and this mixture is mixed with the burned gas 19a. Even in a mixture which is leaner than the lower limit of inflammability, the radicals in the burned gas 19a are effective in initiating reactions, so that the combustion of the mixture can be started. Since the burned gas has a lower oxygen concentration than fresh mixture, and since the pre-mixture is dispersed in space, the generation of NOx can be suppressed.
摘要翻译： 本发明提供了一种燃气轮机燃烧器，其能够在宽输出功率范围内实现高燃烧效率和低NOx排放特性，而不使用能够改变用于燃烧的空气的流量的装置，通过燃烧 使用高温燃烧气体的稀混合。 燃气轮机燃烧器10包括将燃料和空气混合进入燃烧室11的预混合注入管16。 将来自预混合物注入管16的混合物注入存在于火焰19的下游侧的燃烧气体19a，燃烧气体19从从燃烧器15喷射到燃烧室11中，并将该混合物与燃烧气体 19 a。 即使在比易燃性的下限更稀的混合物中，燃烧气体中的自由基a1a也有效地起始反应，从而可以开始混合物的燃烧。 由于燃烧气体的氧浓度低于新鲜混合物，并且由于预混合物分散在空间中，因此可以抑制NOx的产生。
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公开(公告)号：US20050016157A1
公开(公告)日：2005-01-27
申请号：US10623601
申请日：2003-07-22
摘要： A novel combined engine for a single-stage spacecraft is provided that combines a air-breathing engine utilizing oxygen in the atmosphere as oxidizer and rocket engines for obtaining thrust outside the atmosphere and that does not require a portion whose shape is variable in accordance with the flight speed. Rocket engines 15 are provided on struts 12 that form air introduction channels 10 in the air intake section 4. The rocket jets 18 from the rocket engines 15 control the flow of the airflows 16 introduced into the combustion chamber 20 in accordance with the flight speed. When the spacecraft 1 is stationary or in subsonic flight, the rocket jets 18 promote air intake into the combustion chamber 20 by lowering of static pressure due to expansion (ejector effect). In the subsonic flight condition, it performs the role of air compression, mixing with incoming air, fuel injection and ignition and during supersonic/ultra-supersonic flight it performs the role of a variable diffuser.
摘要翻译： 提供了一种用于单级航天器的新型组合发动机，其将在大气中使用氧气的空气呼吸发动机作为氧化剂和用于在大气外部获得推力的火箭发动机相结合，并且不需要其形状根据 飞行速度。 火箭发动机15设置在支柱12上，支柱12在空气吸入部分4中形成空气引入通道10.来自火箭发动机15的火箭喷射器18根据飞行速度控制引入燃烧室20的气流16的流动。 当航天器1是静止或亚音速飞行时，火箭喷射器18通过由于膨胀（喷射器效应）降低静压而促进进入燃烧室20的空气。 在亚音速飞行条件下，它起到空气压缩，与进入的空气混合，燃料喷射和点燃的作用，并且在超音速/超超音速飞行期间，它执行可变扩散器的作用。
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3.发明授权GPS device for measuring wave height and current direction and speed and GPS system for measuring wave height and current direction and speed 失效用于测量波高和电流方向和速度的GPS装置以及用于测量波高和电流方向和速度的GPS系统公开(公告)号：US06847326B2
公开(公告)日：2005-01-25
申请号：US10404088
申请日：2003-04-02
申请人： Masatoshi Harigae , Isao Yamaguchi , Tokio Kasai
发明人： Masatoshi Harigae , Isao Yamaguchi , Tokio Kasai
CPC分类号： G01S19/14 , G01C13/002 , G01S19/35 , G01S19/39
摘要： The present invention provides a GPS device for measuring the wave height and current direction and speed, which is capable of accurately measuring the wave height (height of the waves) and current direction and speed (tidal current) in any point on the sea, ocean, lake, or marsh, and to a system using such a device. The GPS receiver 2 of the GPS device 1 for measuring the wave height and current direction and speed processes the GPS signals received with the GPS antenna 3 and measures the three-dimensional position of antenna 3. The three-dimensional position data are recorded by the data recording unit 4 connected to the GPS receiver 2. When the floating body 5 having those devices 2-4 installed thereon floats on the sea or ocean, it moves together with the waves and tidal current in the present location. The software 7 for conducting high-pass filter processing and smoothing processing is installed in the data processing unit 6, and the data on the wave height and current direction and speed are output, while the errors are being removed from the three-dimensional position data recorded in the data recording unit 4.
摘要翻译： 本发明提供一种用于测量波高和电流方向和速度的GPS装置，其能够精确地测量海洋，海洋中的任何点的波高（波高）和当前方向和速度（潮汐流） ，湖泊或沼泽地，以及使用这种设备的系统。 用于测量波高和当前方向的GPS装置1的GPS接收机2和速度处理用GPS天线3接收的GPS信号并测量天线3的三维位置。三维位置数据由 数据记录单元4连接到GPS接收机2.当具有安装在其上的那些设备2-4的浮体5漂浮在海洋或海洋上时，它与当前位置的波浪和潮汐流一起移动。 用于进行高通滤波处理和平滑处理的软件7安装在数据处理单元6中，并且输出波高和电流方向和速度的数据，同时从三维位置数据中去除误差 记录在数据记录单元4中。
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公开(公告)号：US20040067364A1
公开(公告)日：2004-04-08
申请号：US10643969
申请日：2003-08-20
发明人： Takashi Ishikawa , Yutaka Iwahori , Shin Ishiwata , Shunji Higaki
IPC分类号： B32B009/04
CPC分类号： B82Y30/00 , B32B5/26 , B32B5/28 , C08J5/005 , C08K7/24 , C08K2201/011 , Y10T428/292 , Y10T428/31504
摘要： The resin in a fiber-reinforced resin material that uses a single fiber reinforcing ply or a number of fiber reinforcing plies for reinforcing the resin material is reinforced by dispersing carbon nanofibers therein, whereby a fiber-reinforced composite resin material having improved strength such as compressive strength is provided. In a carbon nanofiber-dispersed resin fiber-reinforced composite material 1, an uncured resin 4 having carbon nanofibers 5 dispersed therein is impregnated into a number of fiber reinforcing plies 2a laid one upon another. Upon curing the resin 4, the strength of the matrix 3 itself is increased through the carbon nanofibers 5 dispersed in the resin 4. Moreover, the fiber reinforcement 2 and the resin 4 are joined together strongly by the carbon nanofibers 5, and hence the strength of the composite material, for example the compressive strength, which hitherto has been dependent on the strength of the resin 4 only, is improved.
摘要翻译： 使用单纤维增强层或多个纤维增强层增强树脂材料的纤维增强树脂材料中的树脂通过在其中分散碳纳米纤维而得到增强，由此提高强度如纤维增强复合树脂材料 提供力量。 在碳纳米纤维分散树脂纤维增强复合材料1中，将分散有碳纳米纤维5的未固化树脂4浸渍在多个彼此叠置的纤维增强层2a中。 在固化树脂4时，通过分散在树脂4中的碳纳米纤维5增加基质3本身的强度。此外，纤维增强材料2和树脂4通过碳纳米纤维5牢固地结合在一起，因此强度 的复合材料，例如迄今为止仅依赖于树脂4的强度的抗压强度得到改善。
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公开(公告)号：US20030006089A1
公开(公告)日：2003-01-09
申请号：US10167459
申请日：2002-06-13
发明人： Tatsuya Ishii
IPC分类号： B64F001/26 , G10K011/00 , E04H017/00
CPC分类号： B64D29/00 , B64D2033/0206 , G10K11/178 , G10K2210/109 , G10K2210/121 , G10K2210/1281 , G10K2210/32121
摘要： The fine jet control type sound absorption system of this invention, aimed at absorbing low-frequency sound with both discrete frequency and broadband frequency to the same degree as already existing acoustic lining can do, is composed of two parts. One is a barrier wall covering an air space in which the concerning low-frequency sound propagates and having a multiplicity of small holes formed therein. The other is the means for causing a fine jet passing through these small holes into or out from the air space. This sound absorption system realizes a fine jet in the vicinity of the barrier wall for the purpose of canceling the sound inside the air space by means of the interference of the sound with the fine jets. Any of or a combination of shape of small holes, jet ejection angle or suction angle, amount of jet flow, thickness of a barrier wall back layer and air flow angle at which secondary air flows into the barrier wall back layer is selected.
摘要翻译： 本发明的精细喷射控制型吸音系统由两部分组成，其目的是吸收具有离散频率和宽带频率的低频声音至与已有声学衬里相同的程度。 一个是覆盖有关低频声音传播并且形成有多个小孔的空气空间的阻挡壁。 另一种是使细小喷嘴穿过这些小洞进入或离开空气的装置。 这种吸音系统在隔壁附近实现了细小的喷射，以便通过声音与细小射流的干扰来消除空气中的声音。 选择小孔的形状，喷射喷射角度或吸入角度，射流量，阻挡壁背层的厚度和二次空气流入阻挡壁背层中的空气流动角度的任何形式或组合。
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公开(公告)号：US20060110007A1
公开(公告)日：2006-05-25
申请号：US10277881
申请日：2002-10-23
摘要： A method for detecting a linear image in a planar picture is provided whereby the positions of a linear image can be determined by devising suitable processing of image data, even if a linear image traced by a moving object, such as space debris, a meteor, or the like, does not appear clearly on a picture. Image data processing, consisting of division processing (S2) for dividing image data of a planar picture captured by an imaging element into a plurality of mutually parallel columnar image data and representative value selection processing (S3) for taking the median value determined for each of the columnar image data as a representative value for the corresponding columnar image data, is performed in every direction of said planar picture, whereupon analysis processing consisting of significant value detection processing (S6) for detecting whether or not said representative value of each of said columnar image data is a significant value, and linear image position identification processing (S7) for identifying the linear position of columnar image data having a representative value indicating a significant value as the position of a linear image resulting from the passage of the moving object or the like, is performed.
摘要翻译： 提供了一种用于检测平面图像中的线性图像的方法，通过设计图像数据的适当处理可以确定线性图像的位置，即使由诸如空间碎片，流星等移动物体跟踪的线性图像， 等等，在图片上不会清楚地显示出来。 图像数据处理由将由摄像元件拍摄的平面图像的图像数据分割为多个相互平行的柱状图像数据的分割处理（S 2）和代表值选择处理（S 3）构成， 在所述平面图像的每个方向上执行作为相应柱状图像数据的代表值的每个柱状图像数据，由此分析处理包括用于检测每个图像的所述代表值是否有效值检测处理（S 6） 所述柱状图像数据是有效值，并且线性图像位置识别处理（S 7）用于识别具有表示有效值的代表值的柱状图像数据的线性位置，作为由 移动物体等。
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公开(公告)号：US06976401B2
公开(公告)日：2005-12-20
申请号：US10190538
申请日：2002-07-09
申请人： Osamu Okamoto , Teruomi Nakaya , Isao Yamaguchi , Seizo Suzuki , Jyunichi Ueno , Yasuoki Usui , Hiroaki Nagano , Katsuhiko Renbutsu , Mitsuharu Izaki , Tadashi Kishimoto
发明人： Osamu Okamoto , Teruomi Nakaya , Isao Yamaguchi , Seizo Suzuki , Jyunichi Ueno , Yasuoki Usui , Hiroaki Nagano , Katsuhiko Renbutsu , Mitsuharu Izaki , Tadashi Kishimoto
CPC分类号： B25J17/0291 , Y10T74/20311 , Y10T74/20317 , Y10T74/20329
摘要： An offset rotary joint unit equipped with a rotation correction mechanism, in which a bending motion can be executed in a two-dimensional plane only by virtue of a rotary mechanism and which can support a high-load weight and is applicable for two-arm mechanisms such as nursing assistant robots. One offset rotary joint unit 4 is composed of a first arm 1, a rotation correction arm 2 rotationally driven around the axial line of the first arm, and a second arm 3 rotationally driven around an axial line obliquely intersecting with the rotation correction arm. A rotation correction joint mechanism 5 linking the first arm 1 and the rotation correction arm 2 and an offset rotary joint mechanism 6 linking the rotation correction arm 2 and the second arm 3 are driven by a single motor 12, and the rotation correction joint mechanism 5 rotates synchronously and in the reverse direction, following the rotation of the offset rotary joint mechanism 6, thereby allowing the second arm 3 to execute a bending motion in a two-dimensional plane with respect to the first arm 1 only by virtue of rotary mechanisms.
摘要翻译： 一种具有旋转校正机构的偏移旋转接头单元，其中只能通过旋转机构在二维平面中执行弯曲运动，并且可以支撑高负载重量并且适用于双臂机构 如护理助理机器人。 一个偏移旋转接头单元4由第一臂1，围绕第一臂的轴线旋转驱动的旋转校正臂2和与旋转校正臂倾斜相交的轴线旋转地驱动的第二臂3组成。 连接第一臂1和旋转校正臂2的旋转校正关节机构5和连接旋转校正臂2和第二臂3的偏移旋转关节机构6由单个电动机12驱动，旋转校正关节机构5 在偏移旋转接头机构6的旋转之后，同步且相反方向旋转，从而允许第二臂3仅通过旋转机构相对于第一臂1在二维平面中执行弯曲运动。
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公开(公告)号：US06922610B2
公开(公告)日：2005-07-26
申请号：US10424711
申请日：2003-04-29
申请人： Osamu Okamoto , Teruomi Nakaya , Seizo Suzuki , Isao Yamaguchi , Heihachiro Kamimura , Kotaro Matsumoto , Sachiko Wakabayashi , Shuichi Sasa
发明人： Osamu Okamoto , Teruomi Nakaya , Seizo Suzuki , Isao Yamaguchi , Heihachiro Kamimura , Kotaro Matsumoto , Sachiko Wakabayashi , Shuichi Sasa
CPC分类号： B62D57/028 , B25J9/06 , B25J17/025 , B64G1/16 , B64G1/62
摘要： A robot is obtained having various functions that are demanded for planetary landing vehicles, extreme operations robots or the like, in particular to provide a leg structure for a robot that is capable of getting up itself when overturned, facilitating take-off and landing on uneven ground, and that has a walking function and that has a hand function capable of three-dimensional operation. A robot comprises a main robot body and at least three legs mounted on this main body for enabling three-dimensional movement of the main robot body such as a self-erecting action or walking action; each leg is constituted by a multi-joint arm having a plurality of said offset rotary joints linked together and has a ground-engaging member mounted at the leading end of the arm, so that each leg is capable of independently controlled three-dimensional movement and drive.
摘要翻译： 获得具有对于行星式着陆车辆，极限作战机器人等要求的各种功能的机器人，特别是提供一种用于机器人的腿部结构，其能够在翻倒时自身起床，便于起飞和着陆在不均匀 地面，具有行走功能，具有能够进行三维操作的手功能。 机器人包括主机器人体和安装在该主体上的至少三个腿，用于使主机器人体的三维运动，例如自立行动或行走动作; 每个腿由具有连接在一起的多个所述偏移旋转接头的多关节臂构成，并且具有安装在臂的前端的接地构件，使得每个腿能够独立控制三维运动， 驾驶。
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9.发明申请GPS device for Measuring wave height and current direction and speed and GPS system for measuring wave height and current direction and speed 失效用于测量波高和电流方向和速度的GPS装置以及用于测量波高和电流方向和速度的GPS系统公开(公告)号：US20030189513A1
公开(公告)日：2003-10-09
申请号：US10404088
申请日：2003-04-02
发明人： Masatoshi Harigae , Isao Yamaguchi , Tokio Kasai
IPC分类号： G01S005/14
CPC分类号： G01S19/14 , G01C13/002 , G01S19/35 , G01S19/39
摘要： The present invention provides a GPS device for measuring the wave height and current direction and speed, which is capable of accurately measuring the wave height (height of the waves) and current direction and speed (tidal current) in any point on the sea, ocean, lake, or marsh, and to a system using such a device. The GPS receiver 2 of the GPS device 1 for measuring the wave height and current direction and speed processes the GPS signals received with the GPS antenna 3 and measures the three-dimensional position of antenna 3. The three-dimensional position data are recorded by the data recording unit 4 connected to the GPS receiver 2. When the floating body 5 having those devices 2-4 installed thereon floats on the sea or ocean, it moves together with the waves and tidal current in the present location. The software 7 for conducting high-pass filter processing and smoothing processing is installed in the data processing unit 6, and the data on the wave height and current direction and speed are output, while the errors are being removed from the three-dimensional position data recorded in the data recording unit 4.
摘要翻译： 本发明提供一种用于测量波高和电流方向和速度的GPS装置，其能够精确地测量海洋，海洋中的任何点的波高（波高）和当前方向和速度（潮汐流） ，湖泊或沼泽地，以及使用这种设备的系统。 用于测量波高和当前方向的GPS装置1的GPS接收机2和速度处理用GPS天线3接收的GPS信号并测量天线3的三维位置。三维位置数据由 数据记录单元4连接到GPS接收机2.当具有安装在其上的那些设备2-4的浮体5漂浮在海洋或海洋上时，它与当前位置的波浪和潮汐流一起移动。 用于进行高通滤波处理和平滑处理的软件7安装在数据处理单元6中，并且输出波高和电流方向和速度的数据，同时从三维位置数据中去除误差 记录在数据记录单元4中。
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公开(公告)号：US20030146344A1
公开(公告)日：2003-08-07
申请号：US10341386
申请日：2003-01-14
IPC分类号： B64D027/00
摘要： This invention provides a multi-fan system separated core engine type turbofan engine in which high pressure air is used as the working fluid for a turbine which drives a fan, thereby reducing the manufacturing costs of the turbofan engine and simplifying the constitution thereof. A turbine for driving a fan 11 which is provided in a propulsion device 3 of the multi-fan system separated core engine type turbofan engine 1 is an air turbine 13 which is driven by the supply through a duct 9 of a part of high pressure air compressed in a compressor 5 of a core engine 2. Since the working fluid of the air turbine 13 for driving the fan 11 is not high temperature combustion gas, there is no need to use expensive heat-resistant material for the turbine, and thus the propulsion device 3 can be manufactured at low cost, the constitution thereof can be simplified, and operational control can be ameliorated.
摘要翻译： 本发明提供了一种多风扇系统分离式核心发动机型涡扇发动机，其中使用高压空气作为驱动风扇的涡轮机的工作流体，从而降低涡轮风扇发动机的制造成本并简化其结构。 用于驱动设置在多风扇系统分离的核心发动机型涡扇发动机1的推进装置3中的风扇11的涡轮机是由供应通过高压空气的一部分的管道9驱动的空气涡轮机13 在核心发动机2的压缩机5中被压缩。由于用于驱动风扇11的空气涡轮13的工作流体不是高温燃烧气体，因此不需要使用昂贵的用于涡轮机的耐热材料，因此， 推进装置3能够以低成本制造，其结构可以简化，并且可以改善操作控制。
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