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1. 发明专利

TW200930621A 用於輸送飛機的系統及方法 SYSTEM AND METHOD FOR TRANSFERRING AIRPLANES 审中-公开
简体标题：用于输送飞机的系统及方法 SYSTEM AND METHOD FOR TRANSFERRING AIRPLANES
公开(公告)号：TW200930621A
公开(公告)日：2009-07-16
申请号：TW097100697
申请日：2008-01-08
申请人：以色列航太工業有限公司 ISRAEL AEROSPACE INDUSTRIES LTD.
发明人：柏瑞爾 BRAIER, RAN , 裴艾伊 PERRY, ARIE
IPC分类号： B64F , G05D
CPC分类号： B64F1/22 , B64F1/227 , B64F1/228 , Y02T50/826
摘要：本發明係無人操作式飛機輸送系統以及輸送飛機的方法。無人操作式飛機輸送系統包含:接收一輸送訊號,該輸送訊號回應於飛機控制組件的移動;及因應該輸送訊號,利用無人操作式飛機輸送系統輸送飛機。
简体摘要：本发明系无人操作式飞机输送系统以及输送飞机的方法。无人操作式飞机输送系统包含:接收一输送信号,该输送信号回应于飞机控制组件的移动;及因应该输送信号,利用无人操作式飞机输送系统输送飞机。

2. 发明专利

TWI398382B 用於輸送飛機的系統及方法有权
简体标题：用于输送飞机的系统及方法
公开(公告)号：TWI398382B
公开(公告)日：2013-06-11
申请号：TW097100697
申请日：2008-01-08
申请人：以色列航太工業有限公司 , ISRAEL AEROSPACE INDUSTRIES LTD.
发明人：柏瑞爾 , BRAIER, RAN , 裴艾伊 , PERRY, ARIE
IPC分类号： B64F1/22 , G05D1/00
CPC分类号： B64F1/22 , B64F1/227 , B64F1/228 , Y02T50/826

3. 发明申请

WO2022058997A1 EVENT PREDICTION BASED ON MACHINE LEARNING AND ENGINEERING ANALYSIS TOOLS 审中-公开
公开(公告)号：WO2022058997A1
公开(公告)日：2022-03-24
申请号：PCT/IL2021/051000
申请日：2021-08-17
申请人： ISRAEL AEROSPACE INDUSTRIES LTD.
发明人： BOUAZIZ, Laura , ASSARAF, Sarit
IPC分类号： G05B23/02 , G06N20/00 , G06N3/08 , G06N3/02
摘要： A computerized system performs training of machine learning models to enable prediction of occurrence of event(s), which are associated with a system to be analyzed. The system performs the following: (a) provide trained Anomaly Detection Model(s). (b) provide Analysis Tool(s), configured to provide quantitative indications of the event(s). The quantitative indications of the event(s) are based on input events(s). (c) receive first unlabeled data associated with the system, where this data comprise sensor data, (d) input the first unlabeled data to the Anomaly Detection Model(s). (d) generate, using the Anomaly Detection Models, indications of occurrence of the input event(s), based on the first unlabeled data, (e) input the indications of the occurrence into the Tool(s). (f) generate, using the Tools, quantitative indications of the events, based the indications of the occurrence, (g) generate, using the quantitative indications, labels for the first unlabeled data.

4. 发明申请

WO2021240509A1 DATABASE UPDATES INDUCED COMMUNICATION IN A COMMUNICATION NETWORK 审中-公开
公开(公告)号：WO2021240509A1
公开(公告)日：2021-12-02
申请号：PCT/IL2021/050603
申请日：2021-05-24
申请人： ISRAEL AEROSPACE INDUSTRIES LTD.
发明人： SHIMON, Yitzhak , INDIK, Yaakov
IPC分类号： G06F8/658 , H04L29/08 , H04W28/06
摘要： According to the subject matter disclosed herein, an application running on a network communication subsystem is assigned with at least one respective database, where data inputs received by the application induce a database update in the respective database. A database update automatically induces packaging of the updated data in a network message followed by transmission of the message to one or more other network communication subsystems connected to the same network. Likewise, in the other direction, an incoming network data-update message, received by the network communication subsystem, initiates a chain of events that cause a database update, which may ultimately affect the data provided to an application running at the application layer.

5. 发明申请

WO2021240506A1 AIR VEHICLE AND METHOD FOR OPERATING THE AIR VEHICLE 审中-公开
公开(公告)号：WO2021240506A1
公开(公告)日：2021-12-02
申请号：PCT/IL2021/050597
申请日：2021-05-23
申请人： ISRAEL AEROSPACE INDUSTRIES LTD.
发明人： HOFI, Nissim , RYNSKI, Shuki
IPC分类号： B64C27/08 , B64C29/00 , B64C27/82 , G05D1/08
摘要： An air vehicle is provided including a body, a primary propulsion unit mounted to the body, and a set of secondary propulsion units mounted to the body. The primary propulsion unit includes at least one primary rotor and is configured for providing at least a majority of a total vertical thrust required for enabling vectored thrust flight to the air vehicle. The set includes at least three said secondary propulsion units. The set is configured for providing variable vectored thrust at least sufficient for generating control moments for stability and control of the air vehicle. The set of secondary propulsion units includes at least one secondary propulsion unit pivotably mounted with respect to the body about a respective pivot axis and configured for pivoting about the pivot axis between at least a vertical mode and a horizontal mode, to respectively provide a thrust vector at least in a range between a vertical thrust vector and a horizontal thrust vector. The pivotable secondary propulsion units are further configured for providing at least horizontal propulsion to the air vehicle at least when not in vertical mode.

6. 发明申请

WO2021205429A1 DISTRIBUTED RADAR SYSTEM AND METHOD OF OPERATION THEREOF 审中-公开
公开(公告)号：WO2021205429A1
公开(公告)日：2021-10-14
申请号：PCT/IL2021/050313
申请日：2021-03-21
申请人： ISRAEL AEROSPACE INDUSTRIES LTD.
发明人： HASSON, Joseph , GOLDNER, Galya
IPC分类号： G01S13/44 , G01S13/58 , G01S13/00 , H01Q21/29
摘要： An antenna system, corresponding control system, and method for operation of the antenna are described. The antenna system comprises: a plurality of antenna units arranged in a predetermined spaced apart arrangement in a selected region and configured to collectively transmit output radiation signal having known beam structure and a control system, the control system is connected to the plurality of antenna units and configured for: transmitting operational instructions to said plurality of antenna units for transmitting radiation signals; receiving data indicative of collected radiation signals, collected in response to reflection of the transmitted signal, and processing the data indicative of the collected radiation signals and determining at least data on angular location of one or more objects associated with said collected radiation signals. The processing comprises, for at least one axis: applying a first mono-pulse beam processing characterized by a first angular shift, determining relative location of said one or more objects with respect to internal features in received beam, and applying a second mono-pulse beam processing characterized by a second angular shift for determining location of said one or more objects with respect to said arrangement of plurality of antenna units.An antenna system, corresponding control system, and method for operation of the antenna are described. The antenna system comprises: a plurality of antenna units arranged in a predetermined spaced apart arrangement in a selected region and configured to collectively transmit output radiation signal having known beam structure and a control system (500). the control system is connected to the plurality of antenna units and configured for: transmitting operational instructions to said plurality of antenna units for transmitting radiation signals; receiving data indicative of collected radiation signals, collected in response to reflection of the transmitted signal, and processing the data indicative of the collected radiation signals and determining at least data on angular location of one or more objects associated with said collected radiation signals. The processing comprises, for at least one axis: applying a first mono-pulse beam processing characterized by a first angular shift, determining relative location of said one or more objects with respect to internal features in received beam, and applying a second monopulse beam processing characterized by a second angular shift for determining location of said one or more objects with respect to said arrangement of plurality of antenna units.

7. 发明申请

WO2021090312A2 LINE OF SIGHT MAINTENANCE DURING OBJECT TRACKING 审中-公开
公开(公告)号：WO2021090312A2
公开(公告)日：2021-05-14
申请号：PCT/IL2020/051141
申请日：2020-11-04
申请人： ISRAEL AEROSPACE INDUSTRIES LTD.
发明人： ROZENBERG, Ohad
IPC分类号： G01S3/786 , G05D1/00 , G01S13/72 , G01S17/66
摘要： The presently disclosed subject matter includes a system and method that provides autonomous flight monitoring and control over an aircraft that assists in maintaining continuous object tracking by a sensing device (e.g. imaging payload such as a camera) mounted on the aircraft (e.g. UAV) and reduce the likelihood of line of sight obstruction or interception while tracking an object.

8. 发明申请

WO2021070185A1 TRAJECTORY SHAPING 审中-公开
公开(公告)号：WO2021070185A1
公开(公告)日：2021-04-15
申请号：PCT/IL2020/051087
申请日：2020-10-08
申请人： ISRAEL AEROSPACE INDUSTRIES LTD.
发明人： ROVINSKY, Jacob
IPC分类号： F42B10/66 , F41F3/04
摘要： 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.

9. 发明申请

WO2020026220A1 CONFORMAL ANTENNA 审中-公开
公开(公告)号：WO2020026220A1
公开(公告)日：2020-02-06
申请号：PCT/IL2018/050855
申请日：2018-08-01
申请人： ISRAEL AEROSPACE INDUSTRIES LTD.
发明人： ROJANSKI, Vladimir
IPC分类号： H01Q1/28 , H01Q13/08 , H01Q21/06 , H01Q21/20
摘要： An antenna device is presented comprising: a conformal antenna body which has a desired geometry corresponding to a front portion of a platform on which the antenna device is to be mounted, and an antenna unit carried by the antenna body. The antenna unit comprises at least one phased array of antenna elements, the antenna elements of each of the at least one array being arranged in a spaced-apart relationship in a closed loop path along a circumference of the antenna body having a desired geometry corresponding to the front portion of the platform on which the antenna unit is to be mounted. Each of the antenna elements is configured as an end-fire antenna element capable of emitting linearly polarized radiation. The array of the antenna elements is operable as a forward looking end-fire antenna array, enabling electronic steering of an antenna beam by controllably modifying phases of the antenna elements of each array.

10. 发明申请

WO2019244150A1 REMOVABLE FLOOR SYSTEM WITH AUXILIARY FUEL TANKS FOR AN AIRCRAFT 审中-公开
公开(公告)号：WO2019244150A1
公开(公告)日：2019-12-26
申请号：PCT/IL2019/050678
申请日：2019-06-18
申请人： ISRAEL AEROSPACE INDUSTRIES LTD.
发明人： ZADAKA, Iftach , GUETTA, Yossi , PINHASI, Uri
IPC分类号： B64D37/08 , B64C1/18 , B64D37/02
摘要： A floor system designed for use with an aircraft is provided. The aircraft comprises a cabin characterized by a first capacity defined by the number of personnel in a predetermined position which may be accommodated therein, and comprises an auxiliary fuel port. The floor system is configured to be detachably installed within the cabin and comprises one or more top panels constituting, when the floor system is installed in the aircraft, a floor of the cabin, and one or more fuel tanks disposed below the top panels and defining an internal space for containing liquid fuel there within. At least one of the fuel tanks is configured for connection to the auxiliary fuel port for supplying the fuel to the aircraft. The cabin with the floor system installed therein is characterized by a second capacity being equal to the first capacity.

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