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61. 发明授权

US09304199B2 Obstacle and terrain warning radar system for a rotorcraft 有权
标题翻译：用于旋翼航空器的障碍物和地形警告雷达系统
公开(公告)号：US09304199B2
公开(公告)日：2016-04-05
申请号：US14100580
申请日：2013-12-09
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GMBH
发明人： Wolfgang Kreitmair-Steck , Richard Scheiblhofer
IPC分类号： G01S13/93 , G01S13/94 , G01S13/00 , G01S13/90
CPC分类号： G01S13/9303 , G01S13/93 , G01S13/94 , G01S2013/9082
摘要： Obstacle and terrain warning radar system (1) for a rotorcraft (2), the system having at least two assemblies (10), each having at least one radar unit, said rotorcraft (2) including at least one main rotor (20) having at least two blades (22) and a rotor head (23). Each radar unit transmits a centrifugal radar beam (17) with angular beam width in azimuth α of at least 5° and beam width in elevation ε of at least 5°. Said assemblies (10) of at least one radar unit are positioned directly on said rotor head (23) between said blades (22), said radar system (1) electronically scanning the surroundings with angular coverage in elevation of at least +/−15° and mechanically scanning the surroundings with angular coverage in azimuth of 360°, and then informing the pilot of said rotorcraft (2).
摘要翻译：用于旋翼航空器（2）的障碍物和地形警告雷达系统（1），所述系统具有至少两个组件（10），每个组件具有至少一个雷达单元，所述旋翼航空器（2）包括至少一个主转子（20）至少两个叶片（22）和转子头（23）。每个雷达单元发射具有至少5°的方位角α的角波束宽度和仰角波束宽度的离心雷达波束（17）至少5°。至少一个雷达单元的所述组件（10）直接位于所述叶片（22）之间的所述转子头（23）上，所述雷达系统（1）以高度角度覆盖至少+/- 15的电子扫描周围环境 °并以360°的方位角度覆盖机械扫描周围环境，然后通知所述旋翼航空器（2）的飞行员。

62. 发明授权

US09251627B2 Removable dashboard instrument system 有权
标题翻译：可拆卸仪表板仪表系统
公开(公告)号：US09251627B2
公开(公告)日：2016-02-02
申请号：US13785337
申请日：2013-03-05
申请人： Ross Carl
发明人： Ross Carl
IPC分类号： G01S13/94 , G07C5/00 , G07C5/08 , H04W4/04 , B60K37/00 , G06Q10/04 , H04L29/08 , B60R11/02
CPC分类号： G07C5/008 , B60K37/00 , B60K37/04 , B60K2350/941 , B60K2350/946 , B60R11/02 , G06Q10/047 , G07C5/0858 , H04L67/12 , H04W4/046
摘要： An instrument system for a vehicle in which information regarding the operation of the vehicle is displayed on the display of a portable communication device. Information regarding the operation of the vehicle may be sensed by at least one sensor. The sensed information may be communicated to a vehicle controller and/or transmitted to the portable communication device. The sensed information may be used by the vehicle controller and/or the portable communication device to derive information regarding the performance or operation of the vehicle and displayed on the display. The portable communication device may also retrieve or derive other information relating to the operation of the vehicle, such as information obtained from a remote server, and display the additional information for the user of the vehicle. The vehicle may be configured to receive the secure placement of the portable communication device in the vehicle, such as on a dashboard.
摘要翻译：一种用于车辆的仪表系统，其中关于车辆的操作的信息被显示在便携式通信设备的显示器上。关于车辆的操作的信息可以由至少一个传感器感测。感测到的信息可以被传送到车辆控制器和/或传送到便携式通信设备。感测到的信息可以由车辆控制器和/或便携式通信设备使用以得到关于车辆的性能或操作并显示在显示器上的信息。便携式通信装置还可以检索或导出与车辆的操作有关的其他信息，例如从远程服务器获得的信息，并显示车辆用户的附加信息。车辆可以被配置为接收便携式通信设备在车辆中的安全放置，诸如在仪表板上。

63. 发明授权

US09238507B2 Terrain awareness system with obstruction alerts 有权
标题翻译：具有障碍警报的地形意识系统
公开(公告)号：US09238507B2
公开(公告)日：2016-01-19
申请号：US13668995
申请日：2012-11-05
申请人： Sandel Avionics, Inc.
发明人： Gerald J. Block
IPC分类号： B64C13/10 , G01C23/00 , G08G5/00 , G01S13/94 , B64D13/00
CPC分类号： G08G5/0086 , B64D13/00 , G08G5/0013 , G08G5/0021 , G08G5/0026 , G08G5/04 , G08G5/045
摘要： Current TAWS systems generally do not provide alerts based on structures or wire obstacles. Such structures and wire obstacles include transmission and electrical wires, and power lines, bridges, and buildings. The current system allows just such alerting. Such alerts are particularly useful for helicopter aircraft, which commonly fly at heights where such structures and obstacles are present near the normal flying altitude of the aircraft. Certain implementations of the system and method include a method of creating an obstacle for use in a terrain awareness warning system, including: receiving data about a first terminus of an obstacle; receiving data about a second terminus of the obstacle; constructing a virtual volume about the first and second termini and a volume therebetween; and storing the virtual volume, whereby a database may be constructed of virtual volumes for use in addition to terrain information to provide alerting on obstacles for an aircraft.
摘要翻译：目前的TAWS系统通常不提供基于结构或线障碍的警报。这种结构和电线障碍物包括传输和电线，电力线，桥梁和建筑物。目前的系统只允许这样的警报。这种警报对于在飞机正常飞行高度附近存在这种结构和障碍物的高度通常飞行的直升机飞机特别有用。该系统和方法的某些实施方式包括创建在地形识别警告系统中使用的障碍物的方法，包括：接收关于障碍物的第一终端的数据; 接收关于障碍物的第二终点的数据; 构建关于第一和第二终端的虚拟体积和它们之间的体积; 并且存储虚拟卷，由此数据库可以由除了地形信息之外的虚拟卷构成以在飞机的障碍物上提供警报。

64. 发明授权

US09141113B1 Probabilistic surface characterization for safe landing hazard detection and avoidance (HDA) 有权
标题翻译：用于安全着陆危险检测和回避（HDA）的概率表面特征
公开(公告)号：US09141113B1
公开(公告)日：2015-09-22
申请号：US13456451
申请日：2012-04-26
申请人： Tonislav I. Ivanov , Andres Huertas , Andrew E. Johnson
发明人： Tonislav I. Ivanov , Andres Huertas , Andrew E. Johnson
IPC分类号： G05D1/00 , G05D1/06 , G01S13/94
CPC分类号： G05D1/0676 , B64G1/00 , G01S7/4808 , G01S13/94 , G01S17/89 , G01S17/933
摘要： Apparatuses, systems, computer programs and methods for performing hazard detection and avoidance for landing vehicles are provided. Hazard assessment takes into consideration the geometry of the lander. Safety probabilities are computed for a plurality of pixels in a digital elevation map. The safety probabilities are combined for pixels associated with one or more aim points and orientations. A worst case probability value is assigned to each of the one or more aim points and orientations.
摘要翻译：提供了用于执行着陆车辆的危害检测和避免的装置，系统，计算机程序和方法。危险评估考虑了着陆器的几何形状。为数字高程图中的多个像素计算安全概率。对于与一个或多个目标点和取向相关联的像素组合安全概率。最坏情况概率值被分配给一个或多个目标点和取向中的每一个。

65. 发明申请

US20150185317A1 THREE DIMENSIONAL RADAR SYSTEM 有权
标题翻译：三维雷达系统
公开(公告)号：US20150185317A1
公开(公告)日：2015-07-02
申请号：US14658619
申请日：2015-03-16
申请人： ELBIT SYSTEMS LTD.
发明人： Hans Martin BRAUN , Gadi MAYDAN , Holger BAESSLER , Carston JONAS , Ofer KLEIN
IPC分类号： G01S13/89 , G01S7/28 , G01S13/94
CPC分类号： G01S13/89 , G01S7/2806 , G01S7/298 , G01S13/5242 , G01S13/9023 , G01S13/94 , G01S2007/027 , G01S2013/9082
摘要： A system and a method of generating a three-dimensional terrain model using one-dimensional interferometry of a rotating radar unit is provided herein. Height information is evaluated from phase differences between two echoes by applying a Kalman filter in relation to a phase confidence map that is generated from phase forward projections relating to formerly analyzed phase data. The radar system starts from a flat earth model and gathers height information of the actual terrain as the platform approaches it. Height ambiguities are corrected by removing redundant 2π multiples from the unwrapped phase difference between the echoes.
摘要翻译：本文提供了使用旋转雷达单元的一维干涉测量来生成三维地形模型的系统和方法。通过应用卡尔曼滤波器相对于从与以前分析的相位数据相关的相位前进投影产生的相位置信图来评估两个回波之间的相位差的高度信息。雷达系统从平地模型开始，并在平台接近时收集实际地形的高度信息。通过删除冗余的2＆pgr来校正高度模糊度; 来自回波之间的展开相位差的倍数。

66. 发明授权

US08970423B2 Helicopter collision-avoidance system using light fixture mounted radar sensors 有权
标题翻译：直升机避雷系统采用灯具安装的雷达传感器
公开(公告)号：US08970423B2
公开(公告)日：2015-03-03
申请号：US13706858
申请日：2012-12-06
申请人： Honeywell International Inc.
发明人： Tomas Kabrt , George Papageorgiou , Jean-Luc Derouineau , Michal Orlita
IPC分类号： G01S13/93 , G01S7/00 , G01S13/87 , G01S13/94
CPC分类号： G01S13/9303 , G01S7/003 , G01S13/87 , G01S13/94
摘要： A helicopter collision-avoidance system is disclosed. An exemplary system includes at least one lamp, such as a light emitting diode (LED) lamp, an incandescent lamp, a halogen lamp, an infrared lamp, or the like; a radar emitter configured to emit a radar signal; a radar detector configured to receive a radar return signal associated with reflections of the emitted radar signal that are reflected from an object; and a radio frequency (RF) system configured to wirelessly transmit radar information associated with the received radar return signal to a radar information receiver configured to receive the wirelessly transmitted radar information. The light module is located at one of a plurality of light positions on an external surface of a helicopter.
摘要翻译：公开了一种直升机防撞系统。示例性系统包括至少一个灯，例如发光二极管（LED）灯，白炽灯，卤素灯，红外灯等; 被配置为发射雷达信号的雷达发射器; 雷达检测器，被配置为接收与从物体反射的所发射的雷达信号的反射相关联的雷达返回信号; 以及射频（RF）系统，被配置为将与所接收的雷达返回信号相关联的雷达信息无线地发射到被配置为接收无线发射的雷达信息的雷达信息接收机。光模块位于直升机的外表面上的多个光位置之一处。

67. 发明授权

US08773301B1 System for and method of sequential lobing using less than full aperture antenna techniques 有权
标题翻译：使用小于全孔径天线技术的顺序波纹的系统和方法
公开(公告)号：US08773301B1
公开(公告)日：2014-07-08
申请号：US13474559
申请日：2012-05-17
申请人： Daniel L. Woodell
发明人： Daniel L. Woodell
IPC分类号： G01S13/94 , G01S13/00
CPC分类号： G01S13/94 , G01S3/32 , G01S3/48 , G01S13/953 , Y02A90/18
摘要： A method of determining an angle within the beam to a target using an airborne radar includes receiving first data associated with first returns associated with a first portion of an antenna. The method further includes receiving second data associated with second returns associated with a second portion of an antenna, wherein the first portion is not identical to the second portion. The method further includes determining the angle within the beam to the target using the first and second data.
摘要翻译：使用机载雷达确定射束内的角度到目标的方法包括接收与天线的第一部分相关联的与第一返回相关联的第一数据。该方法还包括接收与天线的第二部分相关联的第二返回相关联的第二数据，其中第一部分与第二部分不同。该方法还包括使用第一和第二数据确定射束内的与目标的角度。

68. 发明授权

US08558731B1 System for and method of sequential lobing using less than full aperture antenna techniques 有权
标题翻译：使用小于全孔径天线技术的顺序波纹的系统和方法
公开(公告)号：US08558731B1
公开(公告)日：2013-10-15
申请号：US12167203
申请日：2008-07-02
申请人： Daniel L. Woodell
发明人： Daniel L. Woodell
IPC分类号： G01S13/94 , G01S13/00
CPC分类号： G01S13/94 , G01S3/32 , G01S3/48 , G01S13/953 , Y02A90/18
摘要： A method of determining an angle within the beam to a target using an airborne radar includes receiving first data associated with first returns associated with a first portion of an antenna. The method further includes receiving second data associated with second returns associated with a second portion of an antenna, wherein the first portion is not identical to the second portion. The method further includes determining the angle within the beam to the target using the first and second data.
摘要翻译：使用机载雷达确定射束内的角度到目标的方法包括接收与天线的第一部分相关联的与第一返回相关联的第一数据。该方法还包括接收与天线的第二部分相关联的第二返回相关联的第二数据，其中第一部分与第二部分不同。该方法还包括使用第一和第二数据确定射束内的与目标的角度。

69. 发明申请

US20120127014A1 Method for Producing Sensor-Supported, Synthetic Vision for Landing Support of Helicopters Under Brown-Out or White-Out Conditions 有权
标题翻译：生产传感器支持的合成视觉方法，用于在褐色或白色条件下直升机的着陆支持
公开(公告)号：US20120127014A1
公开(公告)日：2012-05-24
申请号：US13386738
申请日：2010-06-29
申请人： Thomas Muensterer , Matthias Wegner , Peter Kielhorn
发明人： Thomas Muensterer , Matthias Wegner , Peter Kielhorn
IPC分类号： G01S13/94
CPC分类号： G01S13/94 , G01S17/93
摘要： A method for producing a sensor-supported, synthetic view for landing support of helicopters under brown-out or white-out conditions is provided. A virtual 3-D representation of the landing zone is continuously created from 3-D data of the intended landing zone recorded during the landing approach and a monitoring routine is available to ensure that no 3-D data that was produced under brown-out or white-out conditions is considered in the representation. As soon as the monitoring routine detects that 3-D data has been recorded under brown-out or white-out conditions, an additional radar sensor is activated to continuously produce distance and/or Doppler data of potential objects entering the landing zone, the objects being displayed to a pilot of the landing helicopter in the synthetic view.
摘要翻译：提供一种用于在褐色或白色条件下制造用于直升机着陆支持的传感器支撑的合成视图的方法。着陆区域的虚拟3-D表示由着陆方法记录的预期着陆区域的3-D数据连续创建，并且监视程序可用于确保在欠压或不产生的3-D数据下产生在表示中考虑了白色条件。一旦监控程序检测到在褐色或白色条件下记录了3-D数据，则激活附加的雷达传感器以连续地产生进入着陆区域的潜在物体的距离和/或多普勒数据，物体在合成视图中向着陆直升机的飞行员展示。

70. 再颁专利

USRE42708E1 System for avoidance of collision between an aircraft and an obstacle 有权
标题翻译：避免飞机和障碍物碰撞的系统
公开(公告)号：USRE42708E1
公开(公告)日：2011-09-20
申请号：US12685117
申请日：2010-01-11
申请人： Morten Mark , Rolf Bakken
发明人： Morten Mark , Rolf Bakken
IPC分类号： G01S13/93 , G01S13/94 , G08G5/04 , B64D47/00 , G01S13/00
CPC分类号： G08G5/0013 , G01S7/003 , G01S13/91 , G01S13/94 , G01S2013/0254 , G08G5/0026 , H01Q1/06 , H01Q1/1242 , H01Q1/42 , H01Q21/065 , H01Q21/20 , H01Q21/205 , H01Q21/28
摘要： A field unit for warning of a danger of collision between an aircraft and an obstacle, in particular a topographical ground obstacle or an obstacle formed by a mast, building or aerial cable structure, comprises a multi-part tubular mast having devices for fixing a solar panel and a radar antenna; an elongate radar antenna in an environment-protective casing, which, with an electronics unit, forms a radar system for synthesized radar detection of an aircraft in a radar coverage area; a central processing unit for identifying on the basis of information from the radar system an aircraft which is in a zone of the radar coverage area and which on the basis of radar information such as direction, distance and/or speed computes a collision danger area; and a high-intensity light system and radio transmitter system that can be activated by the central processing unit upon detection of an aircraft in a collision danger area. The radio transmitter system may be a VHF or UHF radio transmitter system for providing a radio signal modulated by an audible warning signal, preferably a voice warning signal, whilst the light system preferably comprises a stroboscope light system. The field unit is arranged for communication with other similar field units for remote activation of light or audio warnings in a neighbouring field unit.
摘要翻译：用于警告飞机和障碍物之间的碰撞危险的现场单元，特别是地形地面障碍物或由桅杆，建筑物或航空缆索结构形成的障碍物，包括多部分管状桅杆，其具有用于固定太阳能面板和雷达天线; 在环境保护壳体中的细长雷达天线，其中电子单元形成用于在雷达覆盖区域中的飞行器的合成雷达检测的雷达系统; 基于来自雷达系统的来自雷达覆盖区域的飞机的信息，其基于诸如方向，距离和/或速度的雷达信息来计算碰撞危险区域的中央处理单元; 以及在碰撞危险区域中检测到飞行器时可被中央处理单元激活的高强度光系统和无线电发射机系统。无线电发射机系统可以是VHF或UHF无线电发射机系统，用于提供由可听见的警告信号调制的无线电信号，优选地是语音警告信号，而光系统优选地包括频闪镜系统。该场单元布置成与其他类似的现场单元进行通信，用于远程激活相邻现场单元中的光或音频警告。

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