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1.发明申请SYSTEMS AND METHODS FOR USING RADAR-ADAPTIVE BEAM PATTERN FOR WINGTIP PROTECTION 审中-公开使用雷达自适应光束图案进行WITTIP保护的系统和方法
公开(公告)号：WO2014052060A1
公开(公告)日：2014-04-03
申请号：PCT/US2013/059874
申请日：2013-09-16
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： DUSIK, Matej , VASEK, Jiri , KIRK, James C. , VACANTI, David C. , MAGULA, Filip
CPC classification number: G08G5/045 , B64D43/00 , G01S13/93 , G01S13/931 , G01S2013/9335 , G01S2013/9339 , G08G5/065
Abstract: Systems and methods for adaptively steering radar beam patterns for coverage during aircraft turns. The radar sensor system is mechanically or electrically steered to alter the radar sensor's beam pattern in order to adapt the radar sensor's field of view (FOV) to cover the area of anticipated aircraft wingtip trajectory. The anticipated trajectory is derived, for example, from the aircraft groundspeed, acceleration, heading, turn rate, tiller position, attitude, taxi clearance, etc.
Abstract translation: 用于自适应地引导雷达波束模式以在飞机转弯期间覆盖的系统和方法。 雷达传感器系统被机械或电气控制以改变雷达传感器的波束图案，以便使雷达传感器的视场（FOV）适应于预期飞机翼尖轨迹的面积。 例如，从飞机地速，加速度，航向，转弯率，分蘖位置，姿态，出租车清关等导出预期轨迹。
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公开(公告)号：WO2013181334A1
公开(公告)日：2013-12-05
申请号：PCT/US2013/043257
申请日：2013-05-30
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： LAMKIN, Andrew, Fannon , STARR, Jeffrey, W. , BUSTER, Duke
CPC classification number: G01S13/9303 , G01S7/04 , G01S7/22 , G01S13/931 , G01S2013/9335 , G08G5/0021 , G08G5/065
Abstract: A ground obstacle collision-avoidance system includes a plurality of radar sensor modules that each receive at a radar detector radar return signals corresponding to reflections of the emitted signal from a ground obstacle, and transmits radar information associated with the received radar signal reflections reflected from the ground obstacle, wherein each of the plurality of radar sensor modules are uniquely located on a surface of an aircraft that is at risk for collision with a ground obstacle if the aircraft is moving; a gateway unit that receives the radar information transmitted from the radar sensor module and transmits information associated with the received radar information; a processing system configured to determine a distance from the installation aircraft to a detected ground object detected; and a display configured to present a plan view indicating an aircraft icon and a graphical ground obstacle icon that is associated with the detected ground obstacle.
Abstract translation: 地面障碍物碰撞避免系统包括多个雷达传感器模块，每个雷达传感器模块在雷达检测器处接收雷达对应于来自地面障碍物的发射信号的反射的返回信号，并且发射与从雷达信号反射的接收的雷达信号反射相关联的雷达信息 地面障碍物，其中所述多个雷达传感器模块中的每一个唯一地位于飞机的表面上，如果所述飞行器正在移动，则所述飞机的表面处于与地面障碍物碰撞的风险中; 接收从雷达传感器模块发送的雷达信息并发送与所接收的雷达信息相关联的信息的网关单元; 被配置为确定从所述安装飞行器到检测到的检测到的地面物体的距离的处理系统; 以及显示器，被配置为呈现指示飞行器图标的平面图和与所检测的地面障碍物相关联的图形地面障碍物图标。
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3.发明申请PROCÉDÉ ET DISPOSITIF DE DÉTERMINATION DU RISQUE DE COLLISION AU SOL D'UN AVION 审中-公开用于确定飞机地面碰撞风险的方法和装置
公开(公告)号：WO2016045703A1
公开(公告)日：2016-03-31
申请号：PCT/EP2014/070236
申请日：2014-09-23
Applicant: AIRBUS OPERATIONS (S.A.S.)
Inventor： BOUSQUET, Fabrice , LE BERRE, Guillaume
CPC classification number: G08G5/0021 , G01S13/931 , G01S15/931 , G01S17/933 , G01S2013/9335 , G01S2013/9364 , G01S2013/9367 , G08G5/0078 , G08G5/0086 , G08G5/045 , G08G5/065
Abstract: Ce procédé de détermination des risques de collision d'un avion (1) lors de sa circulation au sol comprend les étapes de : - détermination de la trajectoire de l'avion (1), - détermination, en fonction de ladite trajectoire, d'au moins un volume de protection (V R , V P ) associé à au moins une partie de l'avion, - détection d'un objet entrant dans ledit volume de protection (V R , V P ), - génération d'une alerte en réponse à la détection dudit obstacle.
Abstract translation: 本发明涉及一种用于确定滑行飞机（1）的碰撞风险的方法，包括以下步骤：确定飞行器（1）的轨迹; 根据所述轨迹，确定与所述飞行器的至少一部分相关联的至少一个保护体积（VR，VP）; 检测保护体内（VR，VP）内的物体; 并响应于障碍物的检测而产生报警。
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4.发明申请SYSTEMS AND METHODS FOR ENHANCED AWARENESS OF OBSTACLE PROXIMITY DURING TAXI OPERATIONS 审中-公开加强对税收执行过程中不良后果的认识的系统与方法
公开(公告)号：WO2013181351A1
公开(公告)日：2013-12-05
申请号：PCT/US2013/043287
申请日：2013-05-30
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： KHATWA, Ratan , MANNON, Pamela
CPC classification number: G01S13/66 , B60Q9/008 , B64C25/42 , B64D43/00 , B64D45/00 , G01C23/00 , G01S7/04 , G01S13/765 , G01S13/93 , G01S13/931 , G01S2013/9335 , G01S2013/9339 , G08G5/04 , G08G5/045 , G08G5/065
Abstract: Systems and methods for predicting and displaying targets based on height in relation to the wing, wingtip or other elements of the aircraft, such as engine nacelles. The location of ground obstacles is based on radar returns (from sensors deployed on the ownship), aircraft surveillance data, and/or an airport moving map database.
Abstract translation: 基于与机翼，翼尖或飞机的其他元件（如发动机舱）相关的高度来预测和显示目标的系统和方法。 地面障碍物的位置是基于雷达回报（来自自身部署的传感器），飞机监视数据和/或机场移动地图数据库。
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公开(公告)号：WO2006137871A3
公开(公告)日：2007-05-03
申请号：PCT/US2005033321
申请日：2005-09-16
Applicant: BOEING CO , ANDERSON DAVID M , AKDENIZ AYDIN , BANKS DAVID L , RENTON WILLIAM J , AVERY ROBERT L
Inventor： ANDERSON DAVID M , AKDENIZ AYDIN , BANKS DAVID L , RENTON WILLIAM J , AVERY ROBERT L
IPC: G01S13/93
CPC classification number: G08G5/045 , B60Q1/48 , B60Q1/525 , B60Q5/006 , B64F1/3055 , G01S13/931 , G01S2013/9335 , G01S2013/9367 , G08G5/0082 , G08G5/065 , Y10S367/909
Abstract: The present invention comprises systems and methods for preventing collisions between aircraft and ground vehicles. In one embodiment, a system includes a proximity detection unit and a transducer proximate to a selected structural portion of an aircraft, the proximity detection unit being operable to emit ranging signals through the transducer and to receive reflected signals through the transducer to determine the position of an object within a ranging area adjacent to the structural portion. The system further includes an alarm device coupled to the proximity detection unit that is responsive to a signal generated by the proximity detection unit. In another embodiment, a method includes determining a distance between the ground service vehicle and a selected structural portion of the aircraft when the vehicle is positioned in a ranging area about the aircraft. The method further includes generating a proximity alarm based upon the distance.
Abstract translation: 本发明包括用于防止飞机和地面车辆之间碰撞的系统和方法。 在一个实施例中，系统包括接近检测单元和靠近飞行器的选定结构部分的换能器，该接近检测单元可操作以通过换能器发射测距信号并且通过换能器接收反射信号以确定 与结构部分相邻的测距区域内的对象。 该系统还包括耦合到接近检测单元的报警装置，其响应于由接近检测单元产生的信号。 在另一个实施例中，一种方法包括当车辆位于围绕飞机的测距区域中时，确定地面服务车辆与飞行器的选定结构部分之间的距离。 该方法还包括基于距离产生接近警报。
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Patent Agency Ranking
公开(公告)号：WO2006137871A2
公开(公告)日：2006-12-28
申请号：PCT/US2005/033321
申请日：2005-09-16
Applicant: THE BOEING COMPANY , ANDERSON, David, M. , AKDENIZ, Aydin , BANKS, David, L. , RENTON, William, J. , AVERY, Robert, L.
Inventor： ANDERSON, David, M. , AKDENIZ, Aydin , BANKS, David, L. , RENTON, William, J. , AVERY, Robert, L.
IPC: G01S13/93
CPC classification number: G08G5/045 , B60Q1/48 , B60Q1/525 , B60Q5/006 , B64F1/3055 , G01S13/931 , G01S2013/9335 , G01S2013/9367 , G08G5/0082 , G08G5/065 , Y10S367/909
Abstract: The present invention comprises systems and methods for preventing collisions between aircraft and ground vehicles. In one embodiment, a system includes a proximity detection unit and a transducer proximate to a selected structural portion of an aircraft, the proximity detection unit being operable to emit ranging signals through the transducer and to receive reflected signals through the transducer to determine the position of an object within a ranging area adjacent to the structural portion. The system further includes an alarm device coupled to the proximity detection unit that is responsive to a signal generated by the proximity detection unit. In another embodiment, a method includes determining a distance between the ground service vehicle and a selected structural portion of the aircraft when the vehicle is positioned in a ranging area about the aircraft. The method further includes generating a proximity alarm based upon the distance.
Abstract translation: 本发明包括用于防止飞机和地面车辆之间碰撞的系统和方法。 在一个实施例中，系统包括接近检测单元和靠近飞行器的选定结构部分的换能器，该接近检测单元可操作以通过换能器发射测距信号并且通过换能器接收反射信号以确定 与结构部分相邻的测距区域内的对象。 该系统还包括耦合到接近检测单元的报警装置，其响应于由接近检测单元产生的信号。 在另一个实施例中，一种方法包括当车辆位于围绕飞机的测距区域中时，确定地面服务车辆与飞行器的选定结构部分之间的距离。 该方法还包括基于距离产生接近警报。
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7.发明申请SYSTEMS AND METHODS FOR ENHANCING SITUATIONAL AWARENESS OF AN AIRCRAFT ON THE GROUND 审中-公开提高飞机在地面上的应用意识的系统和方法
公开(公告)号：WO2006135923A2
公开(公告)日：2006-12-21
申请号：PCT/US2006/023113
申请日：2006-06-12
Applicant: AVIATION COMMUNICATION & SURVEILLANCE SYSTEMS LLC , STONE, Cyro , STAYTON, Gregory , MANBERG, Chuck
Inventor： STONE, Cyro , STAYTON, Gregory , MANBERG, Chuck
CPC classification number: G08G5/0078 , G01S7/04 , G01S13/74 , G01S13/931 , G01S2013/9335 , G01S2013/9339 , G01S2013/9353 , G08G5/0008 , G08G5/0021 , G08G5/0065
Abstract: A delineated collision avoidance system may comprise a processor for executing one or more instructions that implement one or more functions of the collision avoidance system, a transceiver for transmitting information from and receiving information for the host aircraft, and memory for storing the one or more instructions for execution by the processor to implement the one or more functions of the collision avoidance system to: receive from the transceiver information from another aircraft, generate from the received information a track for the other aircraft, and determine whether the track will intersect within a predefined period of time a region of interest around the host aircraft. In a variation, the system may include a display and the memory may include instructions to: determine whether a predefined condition is satisfied and change an appearance of a symbol shown on the display to indicate that the predefined condition is satisfied.
Abstract translation: 描绘的防撞系统可以包括用于执行实现冲突避免系统的一个或多个功能的一个或多个指令的处理器，用于从主机飞行器发送信息并且接收主机的信息的收发器，以及用于存储一个或多个指令的存储器 用于由处理器执行以实现冲突避免系统的一个或多个功能：从来自另一飞行器的收发器信息接收从所接收的信息生成另一飞行器的轨道，并且确定轨道是否将在预定义的范围内相交 时间段是主机周围的一个感兴趣的区域。 在一个变型中，系统可以包括显示器，并且存储器可以包括以下指令：确定是否满足预定义条件，并且改变显示器上所示的符号的外观以指示满足预定条件。
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公开(公告)号：WO2014154860A1
公开(公告)日：2014-10-02
申请号：PCT/EP2014/056271
申请日：2014-03-28
Applicant: MALLAGHAN ENGINEERING LIMITED
Inventor： RONAN, Mallaghan
CPC classification number: G01S13/931 , G01S2013/9335 , G01S2013/9353 , G01S2013/936 , G08G1/16 , G08G1/163 , G08G1/166 , G08G5/04 , G08G5/06 , G08G5/065
Abstract: A collision prevention system for ground support equipment, said system comprising means for identifying an aircraft in the vicinity of the ground support equipment and for determining a virtual model of the aircraft based upon stored data and said identification of the aircraft, the system further comprising means for determining parameters relating to the location, speed and orientation of the ground support equipment relative to the aircraft and comparing said parameters to said virtual model to prevent collisions between the ground support equipment and the aircraft.
Abstract translation: 一种用于地面支撑设备的防碰撞系统，所述系统包括用于识别地面支撑设备附近的飞行器的装置，并且用于基于所存储的数据和所述飞行器的识别来确定飞行器的虚拟模型，所述系统还包括装置 用于确定与地面支撑设备相对于飞行器的位置，速度和方向有关的参数，并将所述参数与所述虚拟模型进行比较，以防止地面支撑设备与飞机之间的碰撞。
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公开(公告)号：WO2010141043A1
公开(公告)日：2010-12-09
申请号：PCT/US2010/000621
申请日：2010-03-02
Applicant: GRIFFITH, Gregory, M.
Inventor： GRIFFITH, Gregory, M.
CPC classification number: G08G5/045 , B64F1/228 , G01S13/86 , G01S13/931 , G01S2013/9335 , G01S2013/936 , G08B3/10 , G08G5/04 , G08G5/065
Abstract: An aircraft collision avoidance system comprising (a) at least one separation monitoring device connectable to at least a portion of an aircraft, the separation monitoring device comprising (1) at least one transmitter and (2) at least one receiver and (b) a master unit.
Abstract translation: 1.一种飞机防撞系统，包括：（a）至少一个可连接到飞行器的至少一部分的分离监测装置，所述分离监测装置包括：（1）至少一个发射器和（2）至少一个接收器，以及（b） 主单位
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10.发明申请SYSTEM AND METHOD FOR ENHANCING SITUATIONAL AWARENESS OF AN AIRCRAFT ON THE GROUND 审中-公开用于提高地面上飞机状态意识的系统和方法
公开(公告)号：WO2006135923A3
公开(公告)日：2007-03-01
申请号：PCT/US2006023113
申请日：2006-06-12
Applicant: AVIAT COMM & SURVEILLANCE SYS , STONE CYRO , STAYTON GREGORY , MANBERG CHUCK
Inventor： STONE CYRO , STAYTON GREGORY , MANBERG CHUCK
CPC classification number: G08G5/0078 , G01S7/04 , G01S13/74 , G01S13/931 , G01S2013/9335 , G01S2013/9339 , G01S2013/9353 , G08G5/0008 , G08G5/0021 , G08G5/0065
Abstract: A delineated collision avoidance system may comprise a processor for executing one or more instructions that implement one or more functions of the collision avoidance system, a transceiver for transmitting information from and receiving information for the host aircraft, and memory for storing the one or more instructions for execution by the processor to implement the one or more functions of the collision avoidance system to: receive from the transceiver information from another aircraft, generate from the received information a track for the other aircraft, and determine whether the track will intersect within a predefined period of time a region of interest around the host aircraft. In a variation, the system may include a display and the memory may include instructions to: determine whether a predefined condition is satisfied and change an appearance of a symbol shown on the display to indicate that the predefined condition is satisfied.
Abstract translation: 描绘的防撞系统可以包括用于执行实现冲突避免系统的一个或多个功能的一个或多个指令的处理器，用于从主机飞行器发送信息并且接收主机的信息的收发器，以及用于存储一个或多个指令的存储器 用于由处理器执行以实现冲突避免系统的一个或多个功能：从来自另一飞行器的收发器信息接收从所接收的信息生成另一飞行器的轨道，并且确定轨道是否将在预定义的范围内相交 时间段是主机周围的一个感兴趣的区域。 在一个变型中，系统可以包括显示器，并且存储器可以包括以下指令：确定是否满足预定义条件，并且改变显示器上所示的符号的外观以指示满足预定条件。
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