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    System and method for aircraft-to-aircraft exchange of radar information over low bandwidth communication channel
    11.
    发明专利
    System and method for aircraft-to-aircraft exchange of radar information over low bandwidth communication channel 审中-公开
    雷达信息在低带宽通信信道上的飞行交换的系统和方法

    公开(公告)号：JP2010279034A

    公开(公告)日：2010-12-09

    申请号：JP2010118355

    申请日：2010-05-24

    Applicant: Honeywell Internatl Inc ,  ハネウェル・インターナショナル・インコーポレーテッド

    Inventor： BUNCH BRIAN P ,  GROVE MICHAEL M ,  TRUE WILLARD R ,  KUTTLER KEN

    IPC: H04M11/00 ,  G01S7/20 ,  G01S13/95

    CPC classification number: H04B7/18506 ,  G01S7/003 ,  G01S7/06 ,  G01S13/953 ,  H04B7/18502 ,  Y02A90/18

    Abstract: PROBLEM TO BE SOLVED: To effectively extend the range of an aircraft's weather radar so that the crew of the aircraft has more time to respond to adverse weather conditions and/or potentially dangerous objects, such as other aircraft. SOLUTION: System and method for communicating weather radar information between aircraft communicate weather information between aircraft using low bandwidth communication transceivers 306. An exemplary embodiment receives weather information from a weather radar system 310 on board a remote aircraft 120, processes the received weather information into weather radar image information that is displayable on at least a display 322, processes the weather radar image information into a reduced size dataset, and communicates the reduced size dataset to an installation aircraft 104 over the low bandwidth communication channel, wherein the low bandwidth communication channel is generated by a low bandwidth communication transceiver 306 on board the remote aircraft. COPYRIGHT: (C)2011,JPO&INPIT

    Abstract translation: 要解决的问题：为了有效地扩展飞机的天气雷达的范围，使飞机的机组人员有更多的时间来应对恶劣的天气条件和/或潜在的危险物体，如其他飞机。 解决方案：用于在飞行器之间传播天气雷达信息的系统和方法在使用低带宽通信收发器306的飞机之间传播飞行器之间的天气信息。示例性实施例从遥控飞机120上的天气雷达系统310接收天气信息，处理接收到的天气 至少可以在显示器322上显示的天气雷达图像信息的信息，将天气雷达图像信息处理成缩小尺寸的数据集，并且通过低带宽通信信道将缩小尺寸的数据集传送到安装飞机104，其中低带宽 通信信道由远程飞行器上的低带宽通信收发器306产生。 版权所有（C）2011，JPO＆INPIT

    Systems and methods for collecting weather information using an airborne aircraft
    12.
    发明专利
    Systems and methods for collecting weather information using an airborne aircraft 审中-公开
    使用AIRBORNE飞机收集天气信息的系统和方法

    公开(公告)号：JP2010243483A

    公开(公告)日：2010-10-28

    申请号：JP2010054747

    申请日：2010-03-11

    Applicant: Honeywell Internatl Inc ,  ハネウェル・インターナショナル・インコーポレーテッド

    Inventor： KAUFFMAN DONALD C

    IPC: G01S13/95 ,  G01W1/08

    CPC classification number: G01S13/953 ,  G01S7/22 ,  G01S7/2927 ,  G01S7/41 ,  Y02A90/18

    Abstract: PROBLEM TO BE SOLVED: To provide a system and a method of storing detected weather information using airbone aircraft by detecting weather. SOLUTION: Weather information recording system and method are operable to record information detected by aircraft 104 under flight. This system generates a trigger event, corresponding to the presence of weather 108, 110 of interest, stores weather information collected by an aviation electronics system 302 in a memory in response to generating the trigger event and downloads the stored weather information to a remote memory. At least one dimension of weather is determined by generation of the trigger event, and by comparing at least one dimension of weather with the threshold value of the corresponding dimension, the weather information may be stored in response to at least one dimension of weather exceeded in weather dimension threshold. The weather information may be stored at the detected turbulence exceeded in turbulence threshold value, in response to the dimension. COPYRIGHT: (C)2011,JPO&INPIT

    Abstract translation: 要解决的问题：提供一种通过检测天气来使用空中飞行器来存储检测到的天气信息的系统和方法。

    解决方案：天气信息记录系统和方法可操作以记录由飞行器104在飞行中检测到的信息。 该系统响应于感兴趣的天气108,110的存在而生成触发事件，将航空电子系统302收集的天气信息存储在响应于生成触发事件的存储器中并将所存储的天气信息下载到远程存储器。 通过产生触发事件来确定天气的至少一个维度，并且通过将天气的至少一个维度与相应维度的阈值进行比较，可以响应于天气超过的至少一个维度来存储天气信息 天气维度阈值。 响应于尺寸，天气信息可以以湍流阈值超出的检测到的湍流存储。 版权所有（C）2011，JPO＆INPIT

    Radar monitoring method of wake turbulence
    13.
    发明专利
    Radar monitoring method of wake turbulence 审中-公开

    公开(公告)号：JP2010526716A

    公开(公告)日：2010-08-05

    申请号：JP2010507906

    申请日：2008-05-13

    Applicant: テールズ

    Inventor： バルバレスコ、フレデリック

    IPC: B64D45/00

    CPC classification number: G01S13/951 ,  G01S13/64 ,  G01S13/953 ,  Y02A90/18

    Abstract: 【課題】本発明は、航空機に起因する後方乱気流の状態及び発達を、距離及び方位に関して所与の寸法の解析セルを通して解析される、この乱気流によって反射されたレーダ信号に基づいて検出し評価する方法に関連する。
    【解決手段】この方法は、主に、セル内の乱気流を検出し位置特定するのに適した第１の事前主要検出ステップと、前記検出された乱気流の強度を決定する第２のステップと、前記検出された乱気流の発生からの経過時間及び前記検出された乱気流を特徴付けるジオメトリックパラメータを決定する第３のステップとを含む。
    本発明による方法は、有利なことに、後方乱気流の検出を可能にすると共に、後方乱気流の位置及び強度並びにその発達段階の同時決定を可能にする。
    本発明は、特に、航空交通制御及び航空安全の分野全般に適用される。
    【選択図】図５

    Enhanced alerting of characteristic weather hazards
    14.
    发明专利
    Enhanced alerting of characteristic weather hazards 审中-公开
    加强特征天气危害的报警

    公开(公告)号：JP2010107511A

    公开(公告)日：2010-05-13

    申请号：JP2009247873

    申请日：2009-10-28

    Applicant: Honeywell Internatl Inc ,  ハネウェル・インターナショナル・インコーポレーテッド

    Inventor： KHATWA RATAN ,  MATHAN SANTOSH

    IPC: G01W1/00 ,  G01S13/95 ,  G01W1/10

    CPC classification number: G01S7/22 ,  G01S7/41 ,  G01S13/953 ,  Y02A90/18

    Abstract: PROBLEM TO BE SOLVED: To provide a method of providing weather radar images to the flight crew of an aircraft for enhancing the awareness of weather threats so as to alert the flight crew as to whether the aircraft is most likely to be placed in an unsafe position. SOLUTION: An aircraft weather-radar system 40 includes a display device 44, and a processor 42 coupled to the display device. The processor 42 is configured so as to obtain volumetric radar data, corresponding to at least one signal reflected off of a weather system, based on the radar data, computationally classify the weather system as being one of a first type among a plurality of weather-system types; and after classifying the weather system, the radar data are image-processed. The image processing is configured so as to yield an image representing the weather system and corresponding to the first weather-system type, and to display the image on the display device 44. The volumetric radar data is stored inside a three-dimensional buffer. COPYRIGHT: (C)2010,JPO&INPIT

    Abstract translation: 要解决的问题：提供一种向飞机机组人员提供气象雷达图像的方法，以增强对天气威胁的认识，以便向飞行机组警告飞机是否最有可能被放置在 一个不安全的位置。 解决方案：飞机气象雷达系统40包括显示设备44和耦合到显示设备的处理器42。 处理器42被配置为基于雷达数据获得对应于从天气系统反射的至少一个信号的体积雷达数据，将天气系统计算分类为多个天气系统中的第一类型之一， 系统类型; 在对天气系统进行分类后，对雷达数据进行图像处理。 图像处理被配置为产生表示天气系统并且对应于第一气象系统类型的图像，并且将图像显示在显示装置44上。体积雷达数据被存储在三维缓冲器内。 版权所有（C）2010，JPO＆INPIT

    Self-stabilizing antenna base
    18.
    发明专利
    Self-stabilizing antenna base 审中-公开
    自稳定天线基

    公开(公告)号：JP2010259069A

    公开(公告)日：2010-11-11

    申请号：JP2010094989

    申请日：2010-04-16

    Applicant: Honeywell Internatl Inc ,  ハネウェル・インターナショナル・インコーポレーテッド

    Inventor： GIBSON TIMOTHY ,  TYNER GENE MONTE ,  CRAWFORD TOM ALAN

    IPC: H01Q3/02 ,  G01S7/02 ,  G01S13/60 ,  G01S13/95

    CPC classification number: H01Q3/02 ,  G01C21/16 ,  G01S7/4026 ,  G01S13/953 ,  G01S2007/403 ,  G01S2007/4034 ,  G01S2007/4091 ,  Y02A90/18

    Abstract: PROBLEM TO BE SOLVED: To provide an antenna device (18) having a system for automatic stabilization and positioning control. SOLUTION: The antenna device incorporates micro-electromechanical (MEMS)-based accelerometer and gyroscope integrated circuit (IC) sensors (26) directly into the antenna base (20) in a vehicle-mounted antenna application. The sensors enable the antenna device to automatically stabilize the antenna (22) to achieve a desired beam sweep region, independent of vehicle movement, without requiring external sensor input. The invention eliminates the need for a communication interface to externally mounted orientation sensors, reduces cable I/O, and eases the installation procedure. COPYRIGHT: (C)2011,JPO&INPIT

    Abstract translation: 要解决的问题：提供一种具有用于自动稳定和定位控制的系统的天线装置（18）。 解决方案：天线装置在车载天线应用中将基于微机电（MEMS）的加速度计和陀螺仪集成电路（IC）传感器（26）直接并入天线基座（20）中。 传感器使得天线装置能够自动地稳定天线（22）以实现与车辆移动无关的期望的波束扫掠区域，而不需要外部传感器输入。 本发明消除了对外部安装的定向传感器的通信接口的需要，减少了电缆I / O，并且简化了安装过程。 版权所有（C）2011，JPO＆INPIT

    System and method for assessing weather in proximity to airborne aircraft
    19.
    发明专利
    System and method for assessing weather in proximity to airborne aircraft 有权
    用于评估空中飞机天气的系统和方法

    公开(公告)号：JP2010241412A

    公开(公告)日：2010-10-28

    申请号：JP2010054743

    申请日：2010-03-11

    Applicant: Honeywell Internatl Inc ,  ハネウェル・インターナショナル・インコーポレーテッド

    Inventor： KAUFFMAN DONALD C ,  BUNCH BRIAN P

    IPC: B64D45/00 ,  G01W1/00

    CPC classification number: G01S13/953 ,  G01S7/062 ,  Y02A90/18

    Abstract: PROBLEM TO BE SOLVED: To provide a system and a method for assessing weather in proximity to an airborne aircraft. SOLUTION: The dynamic weather model system and method are operable to assess weather 108, 110 in proximity to the airborne aircraft 104. An exemplary embodiment receives a radar echo signal from the weather, determines reflectivity information from the received radar echo signal, retrieves a weather model from a weather model data base 228, compares the weather with the retrieved weather model and the determined reflectivity information, predicts a characteristic of the weather based upon the comparison of the weather and the weather model, and determines if the predicted characteristic is potentially hazardous to the airborne aircraft or not. The weather model is defined by at least one weather modeling algorithm, and is defined by at least one of a parameter and a variable parameter range residing in a weather characteristic database 338. COPYRIGHT: (C)2011,JPO&INPIT

    Abstract translation: 要解决的问题：提供一种用于评估靠近机载飞机的天气的系统和方法。 解决方案：动态气象模型系统和方法可操作以评估靠近机载飞机104的天气108,110。示例性实施例从天气接收雷达回波信号，从接收到的雷达回波信号确定反射率信息， 从天气模型数据库228检索天气模型，将天气与检索到的天气模型和确定的反射率信息进行比较，基于天气和天气模型的比较来预测天气的特征，并且确定预测特性 对机载飞机有潜在的危害。 天气模型由至少一种天气造型算法定义，并且由驻留在天气特征数据库338中的参数和可变参数范围中的至少一个来定义。版权所有（C）2011，JPO和INPIT

    Ground collision instrument for aircraft and marine vehicle
    20.
    发明专利
    Ground collision instrument for aircraft and marine vehicle 有权
    飞机和海上车辆接地碰撞仪

    公开(公告)号：JP2009282959A

    公开(公告)日：2009-12-03

    申请号：JP2009014269

    申请日：2009-01-26

    Applicant: Honeywell Internatl Inc ,  ハネウェル・インターナショナル・インコーポレーテッド

    Inventor： BATEMAN C DON ,  POE JOHN J ,  GLOVER HOWARD

    IPC: G08G5/04 ,  G01S13/93 ,  G08G3/02

    CPC classification number: G01S13/9307 ,  G01S7/06 ,  G01S7/412 ,  G01S13/931 ,  G01S13/953 ,  G01S2013/9335 ,  Y02A90/18

    Abstract: PROBLEM TO BE SOLVED: To provide a radar return processing system and a method.
    SOLUTION: A radar return processing system and a method are operable to process radar information when an installation vehicle 122 operates in proximity to a surface area of interest. An exemplary embodiment reduces the energy of an output pulse emitted from a radar system 410, receives a plurality of radar echoes from a plurality of objects that reflect the reduced energy output pulses emitted from the radar system 410, determines a surface area of interest based upon at least a current location of the installation vehicle 122, and filters the radar echoes generated by objects to remove them that are located outside the surface area of interest. Optionally, some of the systems and methods may reduce a sweep range of an antenna on which the reduced energy output pulses are emitted.
    COPYRIGHT: (C)2010,JPO&INPIT

    Abstract translation: 要解决的问题：提供雷达返回处理系统和方法。 解决方案：当安装车辆122在感兴趣的表面区域附近操作时，雷达返回处理系统和方法可操作用于处理雷达信息。 示例性实施例减少从雷达系统410发射的输出脉冲的能量，从反映从雷达系统410发射的减少的能量输出脉冲的多个物体接收多个雷达回波，基于雷达系统410确定感兴趣的表面区域 至少安装车辆122的当前位置，并且对由物体产生的雷达回波进行过滤，以移除位于感兴趣的表面区域之外的它们。 可选地，一些系统和方法可以减少在其上发射减少的能量输出脉冲的天线的扫描范围。 版权所有（C）2010，JPO＆INPIT

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