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71. 发明申请

US20170159937A1 FUEL INJECTION DEVICE 审中-公开
公开(公告)号：US20170159937A1
公开(公告)日：2017-06-08
申请号：US15435680
申请日：2017-02-17
申请人： KAWASAKI JUKOGYO KABUSHIKI KAISHA , JAPAN AEROSPACE EXPLORATION AGENCY
发明人： Masayoshi KOBAYASHI , Ryusuke MATSUYAMA , Kenta YAMAGUCHI , Hitoshi FUJIWARA
IPC分类号： F23R3/16 , F02C7/24 , F02C7/22 , F23R3/28
CPC分类号： F23R3/16 , F02C7/22 , F02C7/232 , F02C7/24 , F05D2220/32 , F05D2240/35 , F05D2260/231 , F23R3/28
摘要： A fuel injection device for a gas turbine combustor includes: a pilot fuel injector; a main fuel injector; a plurality of main fuel injection holes arranged in the main fuel injector to inject the fuel rearward; a main fuel injection nozzle to guide the fuel to a main air passage, protruding rearward from a circumference of the main fuel injection hole into the opening formed in a passage wall that forms the main air passage; a heat-shielding casing covering the main fuel injector; and a ring member interposed in an axial gap between the passage wall and the heat-shielding casing. The ring member covers a through-hole gap between the main fuel injection nozzle and a through-hole in the heat-shielding casing, and has a purge passage communicated with the opening to introduce air into the main air passage.

72. 发明授权

US09664391B2 Gas turbine combustor 有权
公开(公告)号：US09664391B2
公开(公告)日：2017-05-30
申请号：US14091619
申请日：2013-11-27
申请人： KAWASAKI JUKOGYO KABUSHIKI KAISHA , JAPAN AEROSPACE EXPLORATION AGENCY
发明人： Masayoshi Kobayashi , Takeo Oda , Ryusuke Matsuyama , Atsushi Horikawa , Hitoshi Fujiwara
IPC分类号： F23R3/28 , F23R3/16 , F23R3/18 , F23R3/34 , F23R3/50 , F23R3/14
CPC分类号： F23R3/28 , F23R3/14 , F23R3/16 , F23R3/18 , F23R3/286 , F23R3/343 , F23R3/50
摘要： An annular type gas turbine combustor having a plurality of fuel nozzle assemblies (10) on a circumference includes a pilot nozzle unit (12) for spraying a fuel for diffusive combustion from a pilot outer peripheral nozzle (34) into a combustion chamber (8), a main nozzle unit (14) provided so as to surround the pilot nozzle unit (12) for spraying a fuel for premix combustion, and a flow guide (27) disposed on a downstream side of each of the fuel nozzle assemblies (10) and having a sectional area of a passage for air and air-fuel mixture from each of the fuel nozzle assemblies (10), which gradually increase in a downstream direction.

73. 发明申请

US20170129280A1 RIGID WHEEL AND GROUSER DESIGNS FOR OFF-ROAD MOBILITY 审中-公开
公开(公告)号：US20170129280A1
公开(公告)日：2017-05-11
申请号：US15348913
申请日：2016-11-10
申请人： CALIFORNIA INSTITUTE OF TECHNOLOGY , JAPAN AEROSPACE EXPLORATION AGENCY
发明人： Issa A. NESNAS , Masatsugu OTSUKI
IPC分类号： B60B15/18 , B60B11/02
CPC分类号： B60B15/18 , B60B11/02 , B60B15/02 , B60B2900/551 , B60B2900/721
摘要： A wheel includes a circular wheel main body and at least one grouser. The at least one grouser is provided along an outer circumference of the wheel main body and has a contact surface capable of drawing a first tangent line. The first tangent line is inclined opposite to a rotational direction of the wheel main body from the center line of the wheel main body.

74. 发明申请

US20160376032A1 TORQUE GENERATION SYSTEM, ATTITUDE CONTROL SYSTEM FOR SPACECRAFT, AND RELATIVE POSITION AND VELOCITY CONTROL SYSTEM FOR SPACECRAFT 审中-公开
标题翻译：扭矩发生系统，空间姿态控制系统及相关位置及速度控制系统
公开(公告)号：US20160376032A1
公开(公告)日：2016-12-29
申请号：US15150994
申请日：2016-05-10
申请人： Japan Aerospace Exploration Agency
发明人： Osamu MORI , Junichiro KAWAGUCHI , Yoji SHIRASAWA , Toshihiro CHUJO , Kosuke AKATSUKA
IPC分类号： B64G1/24 , B64G1/44 , B64G1/36 , H02S40/30
CPC分类号： B64G1/407 , B64G1/10 , B64G1/24 , B64G1/34 , B64G1/36 , B64G1/361 , B64G1/365 , B64G1/44 , B64G1/443 , H02S40/30
摘要： A torque generation system includes: a plurality of solar array panels and/or solar array panel divisions; and a torque controller configured to control an electricity generation ratio of each of the plurality of solar array panels and/or solar array panel divisions to generate torque.
摘要翻译：扭矩产生系统包括：多个太阳能阵列面板和/或太阳能阵列面板部分; 以及转矩控制器，其被配置为控制所述多个太阳能电池阵列面板和/或太阳能电池阵列面板部分中的每一个的发电率以产生转矩。

75. 发明授权

US09347810B2 Method and apparatus for measuring a pulsatingly fluctuating flow rate 有权
标题翻译：用于测量脉动波动流量的方法和装置
公开(公告)号：US09347810B2
公开(公告)日：2016-05-24
申请号：US14323836
申请日：2014-07-03
申请人： Japan Aerospace Exploration Agency
发明人： Hiroki Kannan , Shusuke Hori , Hideaki Nanri , Masaharu Uchiumi , Yoshiki Yoshida
IPC分类号： G01F1/66 , G01F1/72
CPC分类号： G01F1/72 , G01F1/66
摘要： A method and apparatus for measuring a pulsatingly fluctuating flow rate under a general condition, without needing electrical conductivity for a fluid, and without allowing a phase lag corresponding to a calculation time or attenuation, or resulting from a relation between pressure difference and flow rate, to occur. Ultrasonic waves are repeatedly transmitted with respect to a pulsatingly fluctuating fluid, while the ultrasonic wave is being received, and a signal indicative of the transmission and receipt, and a signal indicative of a timing of the transmission and receipt are recorded. Alternatively, the ultrasonic wave is transmitted and received based on a preliminarily set timing signal, and the signal indicative of the transmission and receipt is recorded. These signals are used to determine flow rates and transmission and receipt timings to plot a pulsating fluctuation. In one or more implementations, the timing signal may be phase-synchronized with a pulsation reference signal.
摘要翻译：一种用于在一般情况下测量脉动波动流量的方法和装置，不需要流体的导电性，并且不允许对应于计算时间或衰减的相位滞后，或由压力差和流量之间的关系产生的相位差，发生。超声波相对于脉动波动的液体被重复传输，同时正在接收超声波，并且记录表示发送和接收的信号以及指示发送和接收的定时的信号。或者，基于预先设定的定时信号来发送接收超声波，记录表示发送和接收的信号。这些信号用于确定流量和传输和接收时间以绘制脉动波动。在一个或多个实现中，定时信号可以与脉动参考信号相位同步。

76. 发明申请

US20140240147A1 APPARATUS AND METHOD FOR SUPPORTING DISTRIBUTION FROM AIRCRAFT 有权
标题翻译：用于支持飞机分配的装置和方法
公开(公告)号：US20140240147A1
公开(公告)日：2014-08-28
申请号：US14259400
申请日：2014-04-23
申请人： ShinMaywa Industries, Ltd. , Japan Aerospace Exploration Agency
发明人： Yushi GODA , Tsubasa YAMADA , Masatoshi ARIMOTO , Shinji TAGAWA , Taiki NAKAIE , Jun ADACHI , Takeshi ITO , Koji MURAOKA , Kohei FUNABIKI , Yuichi MATSUO
IPC分类号： B64D45/00
CPC分类号： A62C3/0242 , A62C3/0228 , A62C3/0292 , B64D1/16 , B64D43/00 , B64D45/00 , F41G9/002 , G01C23/00
摘要： When distribution material is distributed over a target site on a ground surface from an aircraft, a distribution supporting apparatus offers support information to a pilot dropping the distribution material to efficiently distribute the distribution material. The distribution supporting apparatus includes: an input section to which information items on at least an aircraft velocity, an aircraft altitude, and a wind velocity are input; a computation section configured to compute a location at which the distribution material dropped from the aircraft arrives on the ground surface and a density distribution of the distribution material on the ground surface based on the information items input to the input section; and a display control section configured to display, on a display, the support information relating to the location and density distribution computed by the computation section.
摘要翻译：当分配材料从飞机上分布在地面上的目标地点上时，分配支持装置向飞行员提供支持信息，降低分配材料以有效地分配分配材料。分配支持装置包括：至少输入飞行器速度，飞行器高度和风速的信息项的输入部分; 计算部，被配置为基于输入到所述输入部的信息项，计算从所述飞机落下的分布材料到达所述地面的位置以及所述分布材料在所述地面上的密度分布; 以及显示控制部，被配置为在显示器上显示与由计算部计算出的位置和密度分布有关的支持信息。

77. 发明申请

US20040138850A1 Method and apparatus for measuring heat flux distribution on object surface using temperature-sensitive paint 失效
标题翻译：使用温度敏感涂料测量物体表面热流分布的方法和装置
公开(公告)号：US20040138850A1
公开(公告)日：2004-07-15
申请号：US10743786
申请日：2003-12-24
申请人： JAPAN AEROSPACE EXPLORATION AGENCY
发明人： Kazuyuki Nakakita , Keisuke Asai
IPC分类号： G01K003/00
CPC分类号： G01K17/20 , G01K11/12
摘要： An object of the present invention is to provide a method that allows the heat flux distribution on an object surface to be measured even when the heat flux is an unsteady or short-duration phenomenon, and that does not depend on the material of the object; and to provide a system for measuring the heat flux distribution on an object surface with the aid of this method. In the method for measuring the heat flux on an object surface in accordance with the present invention, the emission intensity of a temperature-sensitive paint that varies with the temperature of the object surface is chronologically captured and sensed as video information at a high frame rate, an image of the temperature distribution on the object surface is obtained based on characteristics between the emission intensity and temperature calibration, and the heat flux in each domain is calculated by the Cook and Feldermann method.
摘要翻译：本发明的目的是提供即使当热通量是不稳定或短时间现象而且不依赖于物体的材料时，也能够测量物体表面上的热通量分布的方法。并提供一种借助于该方法测量物体表面上的热通量分布的系统。在根据本发明的用于测量物体表面上的热通量的方法中，随着物体表面的温度而变化的温度敏感性涂料的发射强度按时间顺序捕获并被感测为高帧率的视频信息根据发光强度和温度校准之间的特性，获得物体表面温度分布的图像，并通过Cook和Feldermann方法计算每个域中的热通量。

78. 发明申请

US20230130658A1 METHOD OF DESIGNING AN AIRCRAFT SHAPE OF A SUPERSONIC AIRCRAFT, METHOD OF PRODUCING A SUPERSONIC AIRCRAFT, AND SUPERSONIC AIRCRAFT 有权
公开(公告)号：US20230130658A1
公开(公告)日：2023-04-27
申请号：US17905311
申请日：2021-02-05
申请人： JAPAN AEROSPACE EXPLORATION AGENCY
发明人： Atsushi UENO
IPC分类号： B64F5/00 , B64C30/00 , B64C23/04
摘要： A method of designing an aircraft shape of a supersonic aircraft according to an embodiment of the present invention includes: obtaining an equivalent cross-sectional area distribution of an initial shape at an off-track position of an aircraft; setting a target equivalent cross-sectional area distribution at the off-track position of the aircraft for reducing sonic booms on the basis of the obtained equivalent cross-sectional area distribution; and converting, on the basis of a required additional cross-sectional area distribution that is a difference between the equivalent cross-sectional area distribution and the target equivalent cross-sectional area distribution, a required additional cross-sectional area of a cross-section of the aircraft on an off-track Mach plane that extends through an arbitrary position in an airflow direction into a required additional cross-sectional area of a cross-section of the aircraft on an on-track Mach plane of the aircraft that is located near the off-track Mach plane and adding the required additional cross-sectional area of the cross-section of the aircraft on the on-track Mach plane.

79. 发明授权

US11635373B2 Information processing apparatus, information processing method, program, and monitoring system 有权
公开(公告)号：US11635373B2
公开(公告)日：2023-04-25
申请号：US16757900
申请日：2018-08-29
申请人： JAPAN AEROSPACE EXPLORATION AGENCY
发明人： Atsushi Kanda , Kazuki Hashimoto
IPC分类号： G01N21/47 , G01B11/06 , G01N21/84 , G01N21/94 , G01W1/14 , G08B19/02 , B60W40/06 , G01N21/3554 , G01N21/21 , B60T8/171 , B60T8/172
摘要： It is desirable to provide an information processing apparatus, an information processing method, a program, and a monitoring system capable of monitoring a condition of a measured surface highly accurately and using the monitoring result effectively.
To attain the aforementioned object, according to a mode of the present invention, an information processing apparatus includes an obtaining module and a generating module. The obtaining module obtains measuring data about a measured surface. The generating module generates covering material information about a covering material that covers the measured surface based on a feature of the obtained measuring data.

80. 发明申请

US20230124256A1 METHOD FOR CONTROLLING FUEL CELL DEVICE 有权
公开(公告)号：US20230124256A1
公开(公告)日：2023-04-20
申请号：US17795911
申请日：2020-12-22
申请人： Japan Aerospace Exploration Agency
发明人： Yoshitsugu SONE , Motohiko SATO
IPC分类号： H01M8/04223 , H01M8/04089 , H01M8/04082
摘要： A method of controlling a fuel cell device includes: a step of purging a hydrogen supply unit of a fuel electrode and purging a gas supply unit of an oxidant electrode when an operation of the fuel cell device ends; a step of measuring a voltage between the fuel electrode and the oxidant electrode and determining whether the voltage is greater than a predetermined threshold; a step of continuing power generation in the fuel cell device when the voltage is greater than the predetermined threshold; and a step of depressurizing the hydrogen supply unit and the gas supply unit when the voltage is equal to or less than the predetermined threshold.

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