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1.发明公开A LOCKING APPARATUS AND A SECURING MECHANISM THEREIN 审中-公开SPERRVORRICHTUNG UND SICHERUNGSMECHANISMUS DARIN
公开(公告)号：EP3097040A4
公开(公告)日：2017-10-04
申请号：EP15737779
申请日：2015-01-18
发明人： LEPEK HANAN , HERZIG YOAV , EINAV OMER , SHABANOV DORON
CPC分类号： B65D90/0006 , B65G1/0471 , B65G63/004 , F16B2/04 , F16B2/14 , F16B2/18
摘要： A securing mechanism for securing thereto a load. The securing mechanism comprises a locking member having at least one planner with a peripheral shape, a cam follower mechanism having a follower with a load facing end and being configured to translate a linear displacement along an axis being perpendicular to said load facing end to a rotational movement thereof about said axis, and being so disposed relative to said locking member such that said rotational movement thereof sequentially shifts said locking member between a released position in which at least one dimension of said peripheral shape has a first size and a secured position in which said dimension has a second size, said second size being larger than said first size.
摘要翻译： 用于固定其上的固定机构。 该固定机构包括锁定构件，该锁定构件具有至少一个具有周边形状的平面设计器，凸轮从动件机构，该凸轮从动件机构具有从动件，该从动件具有面向负载端并且构造成将线性位移沿垂直于所述面向载荷端的轴线平移至旋转 其围绕所述轴线的运动，并且相对于所述锁定构件如此布置，使得其所述旋转运动顺序地将所述锁定构件在释放位置和释放位置之间移动，在释放位置中，所述外围形状的至少一个尺寸具有第一尺寸， 所述尺寸具有第二尺寸，所述第二尺寸大于所述第一尺寸。
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2.发明公开COMPUTERIZED SYSTEM FOR MONITORING AND CONTROLLING PHYSICAL DATA-PRODUCING APPARATUS 审中-公开计算机检测系统ZURÜBERWACHUNGUND STEUERUNG EINESGERÄTSZUR ERZEUGUNG VON PHYSIKALISCHEN DATEN
公开(公告)号：EP2659409A4
公开(公告)日：2017-08-23
申请号：EP11852387
申请日：2011-12-19
发明人： RETTER ALON
CPC分类号： G06N5/02 , G05B23/0254 , G06K9/0053
摘要： A computerized system for monitoring physical data for anomalies, which physical data are predictable given predetermined information, the system comprising a predetermined information data point generator operative to compute a sequence of model data points which the physical data, given predetermined information, can be expected to duplicate at each of a corresponding sequence of temporal sampling points; a wayward point monitor including a processor operative for monitoring the physical data including identifying wayward points within said physical data that are incongruous with the predetermined information; and an anomalous episode-prompted alarm generator operative for identifying anomalous episodes, each including a cluster of wayward points satisfying predefined anomalous episode-defining criteria and generating an alarm for each anomalous episode identified.
摘要翻译： 一种计算机化的系统，用于监视异常的物理数据，该物理数据在给定预定信息的情况下是可预测的，该系统包括预定的信息数据点生成器，该预定的信息数据点生成器可操作以计算给定预定信息的物理数据可预期的 在时间采样点的相应序列中的每一个处复制; 包括处理器的任意点监视器，所述处理器操作用于监视所述物理数据，所述处理器包括识别与所述预定信息不协调的所述物理数据内的任意点; 以及异常情节提示警报发生器，用于识别异常情节，每个异常情节包括满足预定义的异常情节定义标准的任意点的群集，并且针对每个识别的异常情节产生警报。
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公开(公告)号：EP3140826A4
公开(公告)日：2017-05-10
申请号：EP15789428
申请日：2015-05-07
发明人： SHENFELD URI , ROSENFELD SAMUEL
CPC分类号： G08G5/0008 , G08G5/0021 , G08G5/0078 , G08G5/045
摘要： The presently disclosed subject matter includes a collision warning and avoidance system and method for detecting a collision risk between an interrogating aircraft and at least one interrogated aircraft. Signals received from the at least one interrogated aircraft or by the at least one interrogated aircraft and at least one other interrogating aircraft are used for determining various situation awareness data which is used for determining whether the interrogating aircraft is in a risk of collision. If indeed a collision risk exists a collision warning is generated, the collision warning including data indicative of at least an estimated location of the at least one interrogated aircraft.
摘要翻译： 目前公开的主题包括用于检测询问飞机和至少一个询问飞机之间的碰撞风险的碰撞警告和回避系统和方法。 从至少一个询问飞机或由至少一个询问飞机和至少一个其他询问飞机接收到的信号用于确定各种情况感知数据，该数据用于确定询问飞机是否处于碰撞危险中。 如果确实存在碰撞风险，则生成碰撞警告，碰撞警告包括表示至少一个询问飞机的至少估计位置的数据。
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公开(公告)号：EP3017269A4
公开(公告)日：2017-03-01
申请号：EP14819424
申请日：2014-07-01
发明人： LEVY BENJAMIN , GOLDBERG SHMUEL
摘要： The presently disclosed subject matter includes a method, apparatus and computer storage device for reducing dispersion of a rocket caused by jet-stream misalignment, the rocket comprising a rocket engine. Information indicative of a division of total operation time of the rocket engine into a first time period and a second time period is obtained; wherein an impulse which is generated during the first time period is at least approximately the same as an impulse generated during the second time period; a period of time which equals to the first time period starting from time of activation of the rocket engine is measured; upon termination of the period of time, the rocket is rotated around the rocket's longitudinal axis; and the angle of rotation measured; and the rotation is stopped once a 180° rotation is completed.
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5.发明公开DELAY COMPENSATION WHILE CONTROLLING A REMOTE SENSOR 审中-公开VERZÖGERUNGSKOMPENSTINGBEI DER REGELUNG EINES FERNSENSORS
公开(公告)号：EP2946283A4
公开(公告)日：2016-10-12
申请号：EP14740815
申请日：2014-01-14
发明人： BAR DAVID SAGIV , COHEN YOSSI
CPC分类号： G01S3/7864 , G06K9/32 , H04N5/232 , H04N5/23203 , H04N5/23216
摘要： The presently disclosed subject matter includes a method, a system and a delay compensation unit configured for compensating a delay in communication between a sensing unit and a control unit. A succession of two or more captured images are received from the sensing unit; information indicative of command dynamics parameters are obtained from the control unit; based on the information and a respective transfer function which models the dynamics of the sensor module, the expected reaction of the sensor module to the command is determined; and information indicative of the reaction before the command is executed in the sensing unit can be provided.
摘要翻译： 目前公开的主题包括被配置为补偿感测单元和控制单元之间的通信延迟的方法，系统和延迟补偿单元。 从感测单元接收一连串的两个或更多个拍摄图像; 从控制单元获得表示指令动力学参数的信息; 基于对传感器模块的动力学建模的信息和相应的传递函数，确定感测模块对命令的预期反应; 并且可以提供表示在感测单元中执行命令之前的反应的信息。
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公开(公告)号：EP2946361A4
公开(公告)日：2016-09-21
申请号：EP14740456
申请日：2014-01-14
发明人： SABATO MOSHE
IPC分类号： G06T7/20
CPC分类号： H04N7/183 , G06T7/20 , G06T2207/10016 , G06T2207/10032 , G06T2207/20104 , G06T2207/30232 , H04N5/23216
摘要： The presently disclosed subject matter includes tracking method and system wherein a succession images is generated at a sensing unit; one or more moving object in the succession of images is identified; an object tag is assigned to at least one of the moving objects to yield in a respective tagged object; responsive to a command received from a control unit indicative of a selected object, identifying a location of the selected object in a latest available captured image, wherein: if the selected object is a moving object, the selected object is identified in the latest available captured image based on a respective object tag; and if the selected object is a stationary object, the selected object is identified using an image or piece thereof comprising the at least one selected object.
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公开(公告)号：EP1913557A4
公开(公告)日：2010-01-06
申请号：EP06745176
申请日：2006-06-22
发明人： KARAZI URI
IPC分类号： H04N7/18
CPC分类号： G06K9/00771 , G01S5/16 , G06K9/3233 , G06K9/3241 , G06T7/20 , G06T2207/10016 , G06T2207/10032 , G06T2207/20104 , G06T2207/30212
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公开(公告)号：EP3178154A4
公开(公告)日：2018-05-02
申请号：EP15829823
申请日：2015-07-29
发明人： REGEV EYAL
CPC分类号： B64D35/02 , B60L11/12 , B64C15/00 , B64C27/14 , B64C2201/042 , B64C2201/165 , B64D27/24 , H02K7/10 , H02K7/108 , H02K16/00 , H02K21/24 , H02K2213/12 , Y02T50/44 , Y02T50/62
摘要： A propulsion system assembly is provided including a driveshaft and a plurality of electric motor modules. The driveshaft is rotatably mounted to a casing about a drive axis, the driveshaft including a first shaft end and an opposite facing second shaft end. The plurality of electric motor modules are in axially stacked relationship with one another with respect to the drive axis to define an electric motor module stack, each electric motor module being configured for transmitting a torque to the driveshaft when coupled thereto independently of at least one other electric motor module. Each electric motor module includes a controllable clutch arrangement for selectively coupling and decoupling the respective electric motor module with respect to the driveshaft to respectively enable and disable transmission of torque between the respective electric motor module and the driveshaft.
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公开(公告)号：EP3122636A4
公开(公告)日：2017-11-29
申请号：EP15769159
申请日：2015-03-25
CPC分类号： B64D13/08 , B64C39/024 , B64D13/06 , B64D2013/0614 , B64D2013/0618 , B64D2013/0688 , Y02T50/56
摘要： Systems and methods are disclosed for providing a controlled temperature in a control volume. Such systems include a main chamber (defining the control volume), a mixing chamber and a gasflow source. The mixing chamber is in selective fluid communication with the main chamber, and has at least one mixing chamber inlet, and a ram air inlet for allowing ram airflow at a first temperature to be channeled into the mixing chamber. The gasflow source provides a source gasflow at a greater, second temperature to the mixing chamber. The mixing chamber provides the mixing chamber outflow at a third temperature by selectively allowing the ram airflow and the source gasflow in the mixing chamber to mix therein, or, by selectively allowing the ram airflow in the mixing chamber to flow to the main chamber (in absence of source gasflow). A controller is operative to provide a desired level for the third temperature.
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公开(公告)号：EP3111157A4
公开(公告)日：2017-09-27
申请号：EP15755305
申请日：2015-02-24
发明人： OSDON TAL
IPC分类号： F42B10/16
CPC分类号： F42B10/16
摘要： A fin deployment system for a projectile is provided, the fin deployment system defining a longitudinal axis and including: an actuator plate, a first mechanical stop arrangement, an actuation assembly, a plurality of fin assemblies, and a second mechanical stop arrangement. The actuator plate is pivotable from a first pivot position to a second pivot position about the longitudinal axis. The first mechanical stop arrangement is configured for initially locking the actuator plate at the first pivot position, and for selectively unlocking the actuator plate from the first pivot position responsive to an actuating force, to thereby allow the actuator plate to pivot to the second pivot position. The actuation assembly is for selectively applying the actuating force to the first mechanical stop arrangement, to thereby unlock the actuator plate from the first pivot position. Each fin assembly includes a fin pivotable from a stowed position to a deployed position about a respective fin hinge defining a respective deployment axis, each fin assembly forming a kinematic pair with the actuator plate such that the pivoting of the actuator plate between the first pivot position and the second pivot position, and the pivoting of each fin from the respective the stowed position to the respective the deployed position, are concurrent. The second mechanical stop arrangement is for locking the fin assemblies in the respective deployed positions responsive to the actuator plate pivoting from the first pivot position to the second pivot position.
摘要翻译： 提供了用于抛射体的鳍状物展开系统，鳍状部署系统限定纵向轴线并且包括：致动器板，第一机械止动装置，致动组件，多个鳍状物组件和第二机械止动装置。 致动器板能够围绕纵向轴线从第一枢转位置枢转到第二枢转位置。 第一机械止动装置构造成用于首先将致动器板锁定在第一枢转位置处并且用于响应于致动力从第一枢转位置选择性地解锁致动器板从而允许致动器板枢转到第二枢转位置 。 致动组件用于选择性地将致动力施加到第一机械止动装置，从而将致动板从第一枢转位置解锁。 每个翅片组件包括翅片，所述翅片从收起位置枢转到围绕限定相应展开轴线的相应翅片铰链的展开位置，每个翅片组件与致动器板形成运动副，使得致动器板在第一枢转位置 和第二枢转位置以及每个鳍状件从相应的收起位置枢转到相应的展开位置是同时发生的。 第二机械止动装置用于响应于致动器板从第一枢转位置枢转到第二枢转位置而将翅片组件锁定在相应展开位置中。
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