公开(公告)号：US07802759B2

公开(公告)日：2010-09-28

申请号：US11298502

申请日：2005-12-12

申请人： Takashi Ishikawa ,  Yutaka Iwahori ,  Tomohiro Yokozeki ,  Shin-ichi Takeda

发明人： Takashi Ishikawa ,  Yutaka Iwahori ,  Tomohiro Yokozeki ,  Shin-ichi Takeda

IPC分类号： B64C3/26

CPC分类号： B64C3/48

摘要： To provide an aircraft wing which has both high bending flexibility in the wing chord direction and high capacity to maintain the wing shape in the wing span direction, and to which morphing aircraft technology can be applied in the high-speed regime where aerodynamic forces are high.The wing is formed by arranging a plurality of CFRP rods having maximum anisotropic stiffness in the axial direction, so as to be parallel to the wing span direction, and filling the gaps between the CFRP rods with an elastic material.

摘要翻译： 为了提供一种在机翼方向上具有高弯曲灵活性并且具有高容量以维持机翼跨度方向上的机翼形状的飞机机翼，并且在气动力高的高速机构中可以应用变形飞行器技术 。 机翼通过在轴向方向上布置具有最大各向异性刚度的多个CFRP杆而形成，以平行于翼展方向，并用弹性材料填充CFRP杆之间的间隙。

公开(公告)号：US07623956B2

公开(公告)日：2009-11-24

申请号：US11365316

申请日：2006-02-28

申请人： Junichiro Kawaguchi

发明人： Junichiro Kawaguchi

IPC分类号： G08G1/01 ,  G06F19/00

CPC分类号： G08G1/22 ,  B60W30/165 ,  G08G1/161

摘要： The present invention provides a method and a device, which is in one hand implemented as a man-machine system in which the operations are shared such that a driver takes in charge of an inter-vehicle distance and speed control, while on the other hand a quantity of controls for stabilizing the inter-vehicle distance sequence is calculated automatically and additionally incorporated by the addition in respective vehicles. The stabilization of the inter-vehicle distance can be realized by employing the distributed control method in which a set of acceleration and deceleration information from a vehicle traveling ahead is appropriately integrated and transmitted in relay to a following vehicle. This enables the stabilization of the inter-vehicle distance sequence without requiring the inter-vehicle distance measurement in itself and the easy installation of equipment, and realizes a method in which safety is ensured by allowing the driver to still take charge of a local control.

摘要翻译： 本发明提供了一种方法和装置，其一方面实现为人机系统，其中共享操作，使得驾驶员负责车辆间距离和速度控制，而另一方面 自动计算用于稳定车辆间距离序列的量的控制，并且通过在相应的车辆中的添加另外地并入。 车辆间距离的稳定化可以通过采用分散控制方法来实现，其中来自前方行驶的车辆的一组加速和减速信息被适当地整合并且以继电器的形式发送给后续的车辆。 这使得能够稳定车辆间距离序列，而不需要本身的车间距离测量和设备的容易安装，并且实现了通过允许驾驶员仍然负责本地控制来确保安全性的方法。

公开(公告)号：US07591586B2

公开(公告)日：2009-09-22

申请号：US11836693

申请日：2007-08-09

申请人： Akira Ohnishi

发明人： Akira Ohnishi

IPC分类号： G01J5/00

CPC分类号： G01J5/0003

摘要： A method of precisely measuring temperature of an object without having to setting the emissivity of the object over a wide temperature range from low to high temperature with a single radiation thermometer. The temperature-measuring device of the present invention includes a reference object having an emissivity of substantially 1 in a prescribed wavelength range; a bandpass filter transmitting radiant energy in the prescribed wavelength range; and a radiation thermometer for observing temperature by taking in the radiant energy transmitted through the bandpass filter. The device has a structure for measuring temperature of an object by bringing the reference object into contact with the object, observing temperature radiated from the reference object after the temperature of the reference object has become substantially in the thermal equilibrium with the object and transmitted through the bandpass filter using the radiation thermometer, and determining the object temperature based on the observed temperature.

摘要翻译： 一种精确测量物体温度的方法，而不必用单个辐射温度计在低温到高温的宽温度范围内设定物体的发射率。 本发明的温度测量装置包括在规定波长范围内具有大致1的发射率的参考对象; 带通滤波器，在规定的波长范围内发射辐射能; 以及辐射温度计，用于通过吸收透过带通滤光器的辐射能观察温度。 该装置具有用于通过使基准对象与物体接触来测量物体的温度的结构，在参考对象的温度变得基本上与物体的热平衡之后，观察从参考物体辐射的温度，并通过 使用辐射温度计的带通滤波器，并且基于观察到的温度来确定对象温度。

公开(公告)号：US20090226297A1

公开(公告)日：2009-09-10

申请号：US12392203

申请日：2009-02-25

申请人： Ryoji Yanagi ,  Hitoshi Fujiwara

发明人： Ryoji Yanagi ,  Hitoshi Fujiwara

IPC分类号： F01D25/24

CPC分类号： F02K3/065 ,  B64C7/02 ,  B64D29/02 ,  F02C7/04 ,  F05D2250/14 ,  Y02T50/671

摘要： To provide a turbofan jet engine which is capable of increasing the bypass ratio without increasing the fan diameter, and of reducing air resistance acting on the engine, a front fan duct that discharges air compressed by a front fan to the atmosphere and an aft fan duct that introduces air into an aft fan are disposed such as to change cross-sectional shapes thereof by rotating around a core engine in a counterclockwise direction, so that the cross-sectional geometric relationship between the front fan duct and the aft fan duct at a position immediately posterior to the front fan and a cross-sectional geometric relationship between the front fan duct and the aft fan duct at a position immediately anterior to the aft fan are inverted.

摘要翻译： 为了提供一种涡轮风扇喷气发动机，其能够在不增加风扇直径的同时增加旁路比，并且降低作用在发动机上的空气阻力，将由前风扇压缩的空气排出到大气的前风扇管道和向后排出的风扇导管 将空气引入后风扇的方式设置成通过围绕核心发动机沿逆时针方向旋转来改变其横截面形状，使得前风扇管道和后风扇管道在位置处的横截面几何关系 紧靠前风扇的后方，在风扇前方的前方风扇管道与后风扇管道之间的截面几何关系被反转。

公开(公告)号：US07576583B2

公开(公告)日：2009-08-18

申请号：US11638189

申请日：2006-12-12

申请人： Satoshi Kuboyama ,  Hiroyuki Shindou ,  Yoshiya Ilde ,  Akiko Makihara

发明人： Satoshi Kuboyama ,  Hiroyuki Shindou ,  Yoshiya Ilde ,  Akiko Makihara

IPC分类号： H03K3/00

CPC分类号： H03K3/0375

摘要： Disclosed are a latch circuit and a flip-flop circuit, which are capable of suppressing occurrence of a single-event effect, and, in the event of a single-event transient (SET), elimination adverse effects thereof on the circuit. The latch circuit comprises a dual-port inverter, and a dual-port clocked inverter including no transmission gate to reduce a region of strong electric field to be formed. A delay time is set up in a clock to eliminate adverse effects of the SET, and a leading-edge delayed clock to be entered into one of two storage nodes is generated in such a manner as to delay a transition of the storage node and the entire storage nodes from a latch mode to a through mode while preventing an increase in hold time due to the delay time.

摘要翻译： 公开了一种锁存电路和触发器电路，其能够抑制单事件效应的发生，并且在单事件瞬变（SET）的情况下，消除对电路的不利影响。 锁存电路包括双端口反相器和双端口时钟反相器，其不包括传输门，以减少要形成的强电场区域。 延迟时间设置在时钟中以消除SET的不利影响，并且以这样的方式生成要输入到两个存储节点之一的前沿延迟时钟，以延迟存储节点和 整个存储节点从锁存模式到直通模式，同时防止由于延迟时间引起的保持时间的增加。

公开(公告)号：US07544245B2

公开(公告)日：2009-06-09

申请号：US11044325

申请日：2005-01-28

申请人： Kentei Yono ,  Paul-Francois Paradis ,  Takehiko Ishikawa ,  Shinichi Yoda

发明人： Kentei Yono ,  Paul-Francois Paradis ,  Takehiko Ishikawa ,  Shinichi Yoda

IPC分类号： C30B30/00 ,  C30B13/00

CPC分类号： C04B35/4682 ,  C04B35/465 ,  C04B35/47 ,  C04B35/472 ,  C04B2235/3208 ,  C04B2235/604 ,  C04B2235/79 ,  C04B2235/94 ,  C04B2235/95 ,  C30B11/00 ,  C30B11/002 ,  C30B29/16 ,  Y10S117/901

摘要： Disclosed is a method for producing a barium titanium oxide single crystal piece with a given structure using a containerless solidification process, which comprises the steps of preparing a material made of a barium titanium oxide, controlling the material to be in a levitated state within a levitation furnace, melting the levitated material using a laser, and solidifying the molten material while maintaining the levitated state. In a specific embodiment, a spherical sample having a composition of BaTiO3 and a weight of about 20 mg is subjected to a rapid solidification and melting process (temperature gradient: about 700 K/sec) 3 times while levitating the sample in 4.5 atm of air atmosphere using an electrostatic levitation furnace. Then, the re-molten sample is maintained at a temperature just below the melting point of the sample for a given time, and then rapidly cooled at a cooling rate of 300 K/sec to obtain a transparent blue barium titanium oxide single crystal. The single crystal exhibits innovative dielectric characteristics having a large relative permittivity (100,000 or more at room temperature) and a low dielectric loss. In addition, the single crystal has excellent temperature stability allowing the relative permittivity to be gently reduced in the range of room temperature to 70 K.

摘要翻译： 公开了一种使用无容器凝固方法制造具有给定结构的钡钛氧化物单晶片的方法，其包括以下步骤：制备由氧化钛钡制成的材料，将材料控制在悬浮状态下处于悬浮状态 使用激光对悬浮物进行熔融，同时固化熔融材料，同时保持悬浮状态。 在具体实施方案中，将具有BaTiO 3组成和重量约20mg的球形样品在快速凝固和熔化过程（温度梯度：约700K /秒）下进行3次，同时使样品在4.5atm空气中悬浮 使用静电悬浮炉。 然后，将再熔融样品保持在正好低于样品熔点的温度一定时间，然后以300K /秒的冷却速度快速冷却，得到透明的蓝色钡钛氧化物单晶。 单晶具有相对介电常数（室温下为100,000或更高）和低介电损耗的创新介电特性。 此外，单晶具有优异的温度稳定性，允许相对介电常数在室温至70K的范围内轻轻降低。

公开(公告)号：US20090115661A1

公开(公告)日：2009-05-07

申请号：US12296013

申请日：2007-04-02

申请人： Hideyuki Torimoto ,  Makoto Ishii ,  Masahiro Asako ,  Satoshi Kogure

发明人： Hideyuki Torimoto ,  Makoto Ishii ,  Masahiro Asako ,  Satoshi Kogure

IPC分类号： G01S5/14

CPC分类号： G01C21/12 ,  G01C21/206 ,  G01S19/11 ,  G01S19/46 ,  G01S19/48

摘要： Positional information is provided at a place out of reach of radio wave. The process executed by a positional information providing apparatus includes the steps of: obtaining a received positioning signal (S610); specifying an emission source of the positioning signal (S612); obtaining, when the emission source of the positioning signal is outdoors, a navigation message included in the positioning signal (S622); executing a process for calculating the position based on the signal (S624); obtaining, when the emission source of the positioning signal is indoors, message data from the positioning signal (S630); obtaining coordinate values from the data (S632); and displaying positional information based on the coordinate values (S650).

摘要翻译： 无线电波的地方提供了位置信息。 由位置信息提供装置执行的处理包括以下步骤：获得接收到的定位信号（S610）; 指定定位信号的发射源（S612）; 当定位信号的发射源在室外时，获取包括在定位信号中的导航消息（S622）; 执行基于该信号计算位置的处理（S624）; 当定位信号的发射源在室内时，从定位信号得到消息数据（S630）; 从数据获得坐标值（S632）; 并基于坐标值显示位置信息（S650）。

公开(公告)号：US20080223017A1

公开(公告)日：2008-09-18

申请号：US12048478

申请日：2008-03-14

申请人： Takeshi FURUKAWA

发明人： Takeshi FURUKAWA

IPC分类号： F03H1/00 ,  H05H1/46 ,  H05H1/54

CPC分类号： H05H1/54 ,  F03H1/0031 ,  F03H1/0075

摘要： The present invention provides a hall-type electric propulsion that exhibits both overheating protection and operational stability, thereby simultaneously solving the problem of waste heat, which worsens with micronization, and the problem of discharge current oscillation. First, the magnetic flux distribution in ionization/acceleration channel is formed to optimize ion velocity vector, whereupon a propellant flow passage (propellant conduit) is disposed in a magnetic pole of the propulsion, or more specifically in the vicinity of the acceleration channel, and then propellant is passed through the flow passage. Thus, the magnetic pole, which is overheated by the generated plasma, can be cooled, and at the same time the propellant can be heated. Furthermore, the heated propellant is choked immediately before being introduced into the ionization/acceleration channel by a throat region provided immediately before the ionization/acceleration channel, and as a result the sonic speed of neutral species (propellant) is increased.

摘要翻译： 本发明提供一种展示过热保护和操作稳定性的霍尔型电动推进器，从而同时解决了随着微粉化而恶化的废热问题和放电电流振荡的问题。 首先，形成电离/加速通道中的磁通量分布，以优化离子速度矢量，由此将推进剂流动通道（推进剂导管）设置在推进的磁极中，或者更具体地在加速通道附近，以及 然后推进剂通过流道。 因此，可以冷却由所产生的等离子体过热的磁极，同时可以加热推进剂。 此外，加热的推进剂在被离子化/加速通道之前提供的喉部区域引入离子化/加速通道之前立即窒息，结果中性物质（推进剂）的声速增加。

公开(公告)号：US07383104B2

公开(公告)日：2008-06-03

申请号：US11196397

申请日：2005-08-04

申请人： Hirokazu Ishii ,  Kohei Funabiki ,  Yoshinori Okuno ,  Hiromi Gomi

发明人： Hirokazu Ishii ,  Kohei Funabiki ,  Yoshinori Okuno ,  Hiromi Gomi

IPC分类号： G06F7/00 ,  G06F17/00

CPC分类号： G01C21/32 ,  G01C23/00

摘要： It is an object of the present invention to provide a system that is used to provide support so that a pilot can perform flight operations that reduce noise pollution, by devising this system so that noise conditions on the ground are calculated and displayed on the basis of map information for the flight area in which facilities and the like are described, environmental conditions in the flight area such as the wind direction and wind velocity, or the temperature and density of the atmosphere, and noise generation data for the aircraft itself. The apparatus for supporting low-noise flight according to the present invention comprises means for estimating the noise generated by an aircraft using flight data such as the flight speed, the climb and descent rates, the engine power and the like of the aircraft, means for calculating the level at which the noise generated by the aircraft is propagated in the respective regions on the ground, and means for displaying the calculation results on a map in quantitative terms.

摘要翻译： 本发明的目的是提供一种用于提供支撑的系统，使得飞行员可以通过设计该系统来执行降低噪声污染的飞行操作，从而基于地面上的噪声条件被计算和显示 描述设施等的飞行区域的地图信息，飞行区域中的风向和风速的环境条件，大气的温度和密度，以及飞机本身的噪声产生数据。 根据本发明的用于支持低噪声飞行的装置包括用于使用诸如飞行速度，爬升和下降速率，飞机功率等飞行数据来估计飞行器产生的噪声的装置， 计算飞机产生的噪声在地面上相应区域中传播的水平，以及用于在地图上以数量显示计算结果的装置。

公开(公告)号：US20080038618A1

公开(公告)日：2008-02-14

申请号：US11838144

申请日：2007-08-13

申请人： Hitoshi NAITO ,  Yoshitsugu SONE ,  Mitsushi UENO

发明人： Hitoshi NAITO ,  Yoshitsugu SONE ,  Mitsushi UENO

IPC分类号： H01M8/06

CPC分类号： H01M8/04164 ,  F04D29/701

摘要： There is provided a fuel cell system having a moisture mixture separating mechanism capable of separating produced water in high purity. While a sheet member closes an outlet port of a drain port and an inlet port of a drain passage by closely adhering to an outlet-side opening end of the drain port and an inlet-side opening end of the drain passage in a state when hydraulic pressure within a Pitot tube is low, it elastically deforms and separates from the opening ends of the drain port and drain passage when the hydraulic pressure within the Pitot tube increases, thus communicating the outlet-side opening end of the drain port with the inlet-side opening end of the drain passage and discharging water in the drain port to the drain passage.

摘要翻译： 提供一种具有能够分离高纯度的生成水的水分混合分离机构的燃料电池系统。 当片材通过在液压的状态下紧密地粘附到排水口的出口侧开口端和排水通道的入口侧开口端而封闭排水口的出口和排水通道的入口 皮托管内的压力较低，当皮托管内的液压增加时，弹性变形并与排水口和排水通道的开口端分离，从而将排水口的出口侧开口端与入口 - 排水通道的侧面开口端，并将排水口内的水排出到排水通道。