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    • 1. 发明授权
    • Storage apparatus and method of cooling storage apparatus
    • 冷藏存储装置的储存装置及方法
    • US08572430B2
    • 2013-10-29
    • US13381041
    • 2011-11-24
    • Toshikatsu NakamuraMitsuhide SatoNobuhiro Yokoyama
    • Toshikatsu NakamuraMitsuhide SatoNobuhiro Yokoyama
    • G06F11/00
    • G11B33/142G06F3/0614G06F3/0658G06F3/0689H05K7/20727
    • Provided is a storage apparatus for providing a logical storage area as a data storage area to an external apparatus, comprising: a physical storage medium for creating the logical storage area; first and second storage control modules each of which is communicatively coupled to the physical storage medium to control data input/output processing between the external apparatus and the logical storage area; and first and second power supply modules each of which supplies power to the physical storage medium and the first and second storage control modules and includes a blower for generating a cooling airflow to cool down the physical storage medium and the first and second storage control modules, wherein the blower of the first power supply module generates a first cooling airflow which flows through the physical storage medium, the first storage control module, and the first power supply module, the blower of the second power supply module generates a second cooling airflow which flows through the physical storage medium, the second storage control module, and the second power supply module, and in a case where the first power supply module is removed from the storage apparatus, the blower of the second power supply module generates a third cooling airflow which flows through the physical storage medium, the first storage control module, and the second power supply module as a replacement for the first cooling airflow.
    • 提供一种用于向外部装置提供作为数据存储区域的逻辑存储区域的存储装置,包括:用于创建逻辑存储区域的物理存储介质; 第一和第二存储控制模块,每个存储控制模块通信地耦合到物理存储介质以控制外部设备和逻辑存储区域之间的数据输入/输出处理; 以及第一和第二电源模块,每个电源模块向物理存储介质和第一和第二存储控制模块供电,并且包括用于产生冷却气流以冷却物理存储介质和第一和第二存储控制模块的鼓风机, 其中所述第一电源模块的鼓风机产生流过所述物理存储介质,所述第一存储控制模块和所述第一电源模块的第一冷却气流,所述第二电源模块的鼓风机产生流动的第二冷却气流 通过物理存储介质,第二存储控制模块和第二电源模块,并且在第一电源模块从存储装置移除的情况下,第二电源模块的鼓风机产生第三冷却气流, 流过物理存储介质,第一存储控制模块和第二电源模块作为替代 为第一个冷却气流。
    • 5. 发明申请
    • Storage Apparatus and Method of Cooling Storage Apparatus
    • 储存装置及储存装置的冷却方法
    • US20130139000A1
    • 2013-05-30
    • US13381041
    • 2011-11-24
    • Toshikatsu NakamuraMitsuhide SatoNobuhiro Yokoyama
    • Toshikatsu NakamuraMitsuhide SatoNobuhiro Yokoyama
    • G06F1/20G06F1/16G06F11/20
    • G11B33/142G06F3/0614G06F3/0658G06F3/0689H05K7/20727
    • Provided is a storage apparatus for providing a logical storage area as a data storage area to an external apparatus, comprising: a physical storage medium for creating the logical storage area; first and second storage control modules each of which is communicatively coupled to the physical storage medium to control data input/output processing between the external apparatus and the logical storage area; and first and second power supply modules each of which supplies power to the physical storage medium and the first and second storage control modules and includes a blower for generating a cooling airflow to cool down the physical storage medium and the first and second storage control modules, wherein the blower of the first power supply module generates a first cooling airflow which flows through the physical storage medium, the first storage control module, and the first power supply module, the blower of the second power supply module generates a second cooling airflow which flows through the physical storage medium, the second storage control module, and the second power supply module, and in a case where the first power supply module is removed from the storage apparatus, the blower of the second power supply module generates a third cooling airflow which flows through the physical storage medium, the first storage control module, and the second power supply module as a replacement for the first cooling airflow.
    • 提供一种用于向外部装置提供作为数据存储区域的逻辑存储区域的存储装置,包括:用于创建逻辑存储区域的物理存储介质; 第一和第二存储控制模块,每个存储控制模块通信地耦合到物理存储介质以控制外部设备和逻辑存储区域之间的数据输入/输出处理; 以及第一和第二电源模块,每个电源模块向物理存储介质和第一和第二存储控制模块供电,并且包括用于产生冷却气流以冷却物理存储介质和第一和第二存储控制模块的鼓风机, 其中所述第一电源模块的鼓风机产生流过所述物理存储介质,所述第一存储控制模块和所述第一电源模块的第一冷却气流,所述第二电源模块的鼓风机产生流动的第二冷却气流 通过物理存储介质,第二存储控制模块和第二电源模块,并且在第一电源模块从存储装置移除的情况下,第二电源模块的鼓风机产生第三冷却气流, 流过物理存储介质,第一存储控制模块和第二电源模块作为替代 为第一个冷却气流。
    • 6. 发明申请
    • TURBULENCE AVOIDANCE OPERATION ASSIST DEVICE
    • 湍流避免操作辅助装置
    • US20110172919A1
    • 2011-07-14
    • US12909810
    • 2010-10-21
    • Hamaki InokuchiNobuhiro Yokoyama
    • Hamaki InokuchiNobuhiro Yokoyama
    • G06G7/78G06F17/16
    • G08G5/0039G01S17/95
    • An object of the present invention is to provide a turbulence avoidance operation assist device that automatically generates an optimal trajectory of emergency avoidance and reports this trajectory to a pilot when distant turbulence is detected during an aircraft flight. The turbulence avoidance operation assist device in accordance with the present invention includes: means for detecting the presence of a danger region such as a turbulence region ahead of aircraft in a flight direction; means for representing the danger region as an assembly of rectangular solids when the detection means recognizes the danger region, and generating a flight trajectory by a local optimum solution of an avoidance trajectory using a convex quadratic programming method in which deviation from a reference trajectory is the smallest on the basis of an initial estimation solution obtained by a semidefinite programming method; and means for reporting the flight trajectory to a pilot.
    • 本发明的目的是提供一种湍流避免操作辅助装置,其在飞行器飞行期间检测到远距离的湍流时,自动产生紧急避免的最佳轨迹,并将该轨迹报告给飞行员。 根据本发明的湍流避免操作辅助装置包括:用于在飞行方向上检测飞机前方的湍流区域的危险区域的存在的装置; 用于将所述危险区域表示为所述检测装置识别所述危险区域时的矩形固体的组合的装置,以及使用凸二次规划方法通过所述回避轨迹的局部最优解产生飞行轨迹,其中,所述凸二次规划方法与参考轨迹的偏差为 基于通过半定规划方法获得的初始估计解决方案; 以及向飞行员报告飞行轨迹的方法。
    • 7. 发明申请
    • ELECTRONIC DEVICE HAVING BLOWER
    • 具有鼓风机的电子设备
    • US20090129936A1
    • 2009-05-21
    • US12026822
    • 2008-02-06
    • Nobuhiro YOKOYAMATakashi ChikusaMasao Iwakura
    • Nobuhiro YOKOYAMATakashi ChikusaMasao Iwakura
    • F04B49/06F04B17/03H02P5/00
    • F04D29/005F04D25/0633F04D25/064F04D25/0646F04D29/661F04D29/663F04D29/665F04D33/00H02P6/00
    • An electronic device having a first motor which rotates a rotating body (for example, blades) about a rotation axis and a second motor which vibrates a vibrator including the rotating body in the axial direction is provided. A control IC unit has a first circuit which subjects the rotation to control drive by a first waveform, and a second circuit which subjects the vibration to control drive by a second waveform. Rotation and vibration of a rotating and vibrating unit driven by the first and second motors generates an airflow and output sound by a synthesized output of a first output corresponding to the rotation and a second output corresponding to the vibration. The control IC unit generates a second waveform by using a reversed-phase waveform with respect to the first waveform or the like and suppresses the output sound by control of the first and second waveforms.
    • 提供一种电子设备,其具有围绕旋转轴旋转旋转体(例如,叶片)的第一电动机和使包括旋转体的振动器沿轴向振动的第二电动机。 控制IC单元具有使旋转控制第一波形的第一电路和使振动控制第二波形的第二电路。 由第一和第二电动机驱动的旋转和振动单元的旋转和振动通过对应于旋转的第一输出的合成输出和对应于振动的第二输出产生气流和输出声音。 控制IC单元通过使用相对于第一波形等的反相波形来生成第二波形,并且通过控制第一和第二波形来抑制输出声音。
    • 9. 发明授权
    • Turbulence avoidance operation assist device
    • 湍流回避操作辅助装置
    • US09070284B2
    • 2015-06-30
    • US12909810
    • 2010-10-21
    • Hamaki InokuchiNobuhiro Yokoyama
    • Hamaki InokuchiNobuhiro Yokoyama
    • G08G5/00G01S17/95
    • G08G5/0039G01S17/95
    • An object of the present invention is to provide a turbulence avoidance operation assist device that automatically generates an optimal trajectory of emergency avoidance and reports this trajectory to a pilot when distant turbulence is detected during an aircraft flight. The turbulence avoidance operation assist device in accordance with the present invention includes: means for detecting the presence of a danger region such as a turbulence region ahead of aircraft in a flight direction; means for representing the danger region as an assembly of rectangular solids when the detection means recognizes the danger region, and generating a flight trajectory by a local optimum solution of an avoidance trajectory using a convex quadratic programming method in which deviation from a reference trajectory is the smallest on the basis of an initial estimation solution obtained by a semidefinite programming method; and means for reporting the flight trajectory to a pilot.
    • 本发明的目的是提供一种湍流避免操作辅助装置,其在飞行器飞行期间检测到远距离的湍流时,自动产生紧急避免的最佳轨迹,并将该轨迹报告给飞行员。 根据本发明的湍流避免操作辅助装置包括:用于在飞行方向上检测飞机前方的湍流区域的危险区域的存在的装置; 用于将所述危险区域表示为所述检测装置识别所述危险区域时的矩形固体的组合的装置,以及使用凸二次规划方法通过所述回避轨迹的局部最优解产生飞行轨迹,其中,所述凸二次规划方法与参考轨迹的偏差为 基于通过半定规划方法获得的初始估计解决方案; 以及向飞行员报告飞行轨迹的方法。