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公开(公告)号：US11054220B2
公开(公告)日：2021-07-06
申请号：US16472757
申请日：2017-12-24
Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.
Inventor： Michael Maidanik , Oded M. Golan , Miki Livne , Jacob Rovinsky
Abstract: The presently disclosed subject matter includes a computerized method and system for determining miss-distance between platforms. The proposed method and system make use of an electro optic sensor (e.g. camera) mounted on one of the platforms for obtaining additional data which is used for improving the accuracy of positioning data obtained from conventional positioning devices. A navigation error is calculated where the relative position of the two platforms is converted to the camera reference frame. Once the navigation error is available, it can be used to correct a measured miss-distance.
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公开(公告)号：US09995559B2
公开(公告)日：2018-06-12
申请号：US14935831
申请日：2015-11-09
Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.
Inventor： Jacob Rovinsky
CPC classification number: F41H11/02 , F41G7/30 , F41G7/303 , F42B15/01 , G01S7/003 , G01S13/003 , G01S13/878
Abstract: A counter-flying object system comprising a sensor array including at least one active sensor configured to detect and track the flying object, and a missile launcher configured to launch an interceptor to intercept the flying object, wherein upon launching of the interceptor, the sensor array is configured to determine the location of the interceptor and send said object and interceptor locations to a control system, the control system being configured to provide mission data to the interceptor based on said object and interceptor locations for guiding the interceptor toward the flying object and activating a fragmentation warhead on or in the vicinity of said flying object when a lethality criteria is met.
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公开(公告)号：US11187507B2
公开(公告)日：2021-11-30
申请号：US16820238
申请日：2020-03-16
Applicant: Israel Aerospace Industries Ltd.
Inventor： Jacob Rovinsky
Abstract: A fragmentation warhead is provided, capable of being mounted in a carrier vehicle, the warhead having a longitudinal axis. In at least one example the warhead includes a shell that extends along the longitudinal axis. The shell includes a fixed shell portion and a fragmentation portion, and defines therebetween a cavity for accommodating therein an explosive charge. The fragmentation portion includes at least one set of serially adjacent fragments in correspondingly serially contiguous relationship in the fragmentation portion and in generally helical relationship with respect to the longitudinal axis. A corresponding carrier vehicle and a corresponding missile are also provided.
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公开(公告)号：US10012481B2
公开(公告)日：2018-07-03
申请号：US14861328
申请日：2015-09-22
Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.
Inventor： Jacob Rovinsky , Yoav Tourgeman
CPC classification number: F41J2/00 , F41G7/003 , F41G7/004 , F41G7/006 , F41J2/02 , F41J9/08 , F42B8/12 , F42B8/24
Abstract: An inflatable dummy target fittable into a carrier missile capable of being released from the carrier missile during exo-atmospheric flight; upon release, the dummy target or portion thereof is capable of being inflated and manifest characteristics that resemble GTG missile characteristics, wherein the GTG missile characteristics include IR signature, RF signature and GTG missile.
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公开(公告)号：US11946727B2
公开(公告)日：2024-04-02
申请号：US17765148
申请日：2020-10-08
Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.
Inventor： Jacob Rovinsky
CPC classification number: F42B10/668 , F41F3/04 , F41G7/36 , F42B10/26
Abstract: The presently disclosed subject matter includes a system and a method for launching a projectile towards a target, wherein the system comprises a control circuitry, a booster engine, and one or more thrusters adapted to be connected to the projectile and capable of being spun during launch around a longitudinal axis of the projectile, the control circuitry being operatively connected to the one or more thrusters; wherein responsive to ignition of propellant stowed in a combustion chamber of the booster engine, the booster engine causes the projectile to launch from its cell; following launch of the projectile, cause the projectile to turn at a certain rate and a certain azimuth.
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Patent Agency Ranking
公开(公告)号：US10260844B2
公开(公告)日：2019-04-16
申请号：US15130526
申请日：2016-04-15
Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.
Inventor： Jacob Rovinsky , Yoav Tourgeman
IPC: F41J2/00 , F42B10/60 , F42B10/62 , F41J2/02 , F41G7/00 , F41J9/08 , F42B8/12 , F42B8/24 , F41J9/00
Abstract: There is provided an inflatable dummy target comprising a chassis wrapped with a sheet. The chassis can be formed by individual inflatable ducts and can comprise at least two ring-shaped ducts interconnected by one or more elongate ducts. The inflatable dummy target can further comprise rigidizing ducts. The inflatable dummy target geometry can be conical, cylindrical, etc. Optionally, the inflatable dummy target can comprise several attached axi-symmetrical sections, wherein each section has a chassis wrapped with a sheet, the chassis formed by individual inflatable ducts. Optionally, the shape of each section can be selected from the group consisting of conical, frustoconical and cylindrical forms.
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公开(公告)号：US09170076B2
公开(公告)日：2015-10-27
申请号：US14063645
申请日：2013-10-25
Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.
Inventor： Jacob Rovinsky , Yoav Tourgeman
CPC classification number: F41J2/00 , F41G7/003 , F41G7/004 , F41G7/006 , F41J2/02 , F41J9/08 , F42B8/12 , F42B8/24
Abstract: An inflatable dummy target fittable into a carrier missile capable of being released from the carrier missile during exo-atmospheric flight; upon release, the dummy target or portion thereof is capable of being inflated and manifest characteristics that resemble GTG missile characteristics, wherein the GTG missile characteristics include IR signature, RF signature and GTG missile.
Abstract translation: 一个可充气的虚拟目标，可以安装在能够在外部大气飞行期间从载体导弹释放的载体导弹; 在释放时，虚拟目标或其部分能够被充气并显现出类似GTG导弹特性的特征，其中GTG导弹特征包括IR签名，RF签名和GTG导弹。
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公开(公告)号：US20220325993A1
公开(公告)日：2022-10-13
申请号：US17765148
申请日：2020-10-10
Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.
Inventor： Jacob Rovinsky
Abstract: The presently disclosed subject matter includes a system and a method for launching a projectile towards a target, wherein the system comprises a control circuitry, a booster engine, and one or more thrusters adapted to be connected to the projectile and capable of being spun during launch around a longitudinal axis of the projectile, the control circuitry being operatively connected to the one or more thrusters; wherein responsive to ignition of propellant stowed in a combustion chamber of the booster engine, the booster engine causes the projectile to launch from its cell; following launch of the projectile, the control circuitry is configured to activate one or more thrusters that cause the projectile to turn at a certain rate and a certain azimuth.
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公开(公告)号：US20160320165A1
公开(公告)日：2016-11-03
申请号：US15108656
申请日：2015-01-01
Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.
Inventor： Jacob Rovinsky
CPC classification number: F42B12/22 , B64C39/024 , B64C2201/121 , F41G7/001 , F41G7/20 , F42B10/26 , F42B12/202 , F42B12/32 , F42C19/095
Abstract: A fragmentation warhead is provided, capable of being mounted in a carrier vehicle, the warhead having a longitudinal axis. In at least one example the warhead includes a shell that extends along the longitudinal axis. The shell includes a fixed shell portion and a fragmentation portion, and defines therebetween a cavity for accommodating therein an explosive charge. The fragmentation portion includes at least one set of serially adjacent fragments in correspondingly serially contiguous relationship in the fragmentation portion and in generally helical relationship with respect to the longitudinal axis. A corresponding carrier vehicle and a corresponding missile are also provided.
Abstract translation: 提供了能够安装在载体车辆中的分裂弹头，该弹头具有纵向轴线。 在至少一个示例中，弹头包括沿着纵向轴线延伸的壳体。 壳体包括固定壳体部分和碎裂部分，并且在其间限定用于在其中容纳炸药的空腔。 碎裂部分包括在碎裂部分中以相应的串联连续关系的至少一组串联相邻碎片，并且相对于纵向轴线呈大致螺旋关系。 还提供了相应的载体车辆和相应的导弹。
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公开(公告)号：US09207049B2
公开(公告)日：2015-12-08
申请号：US14371480
申请日：2013-01-10
Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.
Inventor： Jacob Rovinsky
CPC classification number: F41H11/02 , F41G7/30 , F41G7/303 , F42B15/01 , G01S7/003 , G01S13/003 , G01S13/878
Abstract: A counter-flying object system that includes a sensor array including an active sensor for detecting and tracking the flying object. An interceptor missile launcher for launching an interceptor to intercept the flying object, wherein upon launching of the interceptor, the sensor array determines the location of the interceptor and sends the object's and interceptor's locations to a control system. The control system provides mission data to the interceptor based on the object's and interceptor's locations for guiding the interceptor toward the flying object and activating a fragmentation warhead on or in the vicinity of the flying object when a lethality criteria is met.
Abstract translation: 一种反飞行物体系统，其包括传感器阵列，其包括用于检测和跟踪飞行物体的主动传感器。 用于发射拦截器以拦截飞行物体的拦截弹导弹发射器，其中在拦截器发射时，传感器阵列确定拦截器的位置，并将物体和拦截器的位置发送到控制系统。 控制系统基于对象和拦截器的位置向拦截器提供任务数据，以在遇到致命性标准时将拦截器引向飞行物体并激活飞行物体上或附近的分裂弹头。
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