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    SYSTEM AND METHOD FOR DETECTING FAILURES IN A SAFETY COUPLING
    2.
    发明申请
    SYSTEM AND METHOD FOR DETECTING FAILURES IN A SAFETY COUPLING 有权

    公开(公告)号：US20240420300A1

    公开(公告)日：2024-12-19

    申请号：US18742076

    申请日：2024-06-13

    Applicant: ODYSIGHT.AI LTD. ,  ISRAEL AEROSPACE INDUSTRIES LTD.

    Inventor： Amir GOVRIN ,  Yekaterina DLUGACH ,  Shoham BEN SHOSHAN

    IPC: G06T7/00 ,  G06T7/73

    Abstract: A system for monitoring a safety coupling, the safety coupling including a visual failure indicator provided by a manufacturer thereof, the system includes: a processing circuitry configured for: receiving image data from the at least one optical sensor, the image data including data of a region of interest of the safety coupling and devoid of the visual failure indicator of the safety coupling; analyzing the image data to detect a change in a relative position between a first and a second part of the safety coupling; evaluating health of the safety coupling by determining whether the detected change is a fault associated with a failure mode of the safety coupling; and outputting an indicator of said health of said safety coupling based on said evaluating.

    Propulsion system
    3.
    发明授权
    Propulsion system 有权

    公开(公告)号：US12097948B2

    公开(公告)日：2024-09-24

    申请号：US18596947

    申请日：2024-03-06

    Applicant: Israel Aerospace Industries Ltd.

    Inventor： Danny Abramov ,  Shai Alexandroni ,  Ben Keshales

    IPC: B64C11/28 ,  B64C7/02 ,  F01D7/00

    CPC classification number: B64C11/28 ,  B64C7/02 ,  F01D7/00

    Abstract: A propulsion system, including a rotor arrangement rotatably mounted with respect to a nacelle about a rotor axis. The rotor arrangement includes rotor blades, each being pivotably mounted to a hub element about a respective blade pivot axis, the rotor blades being deployable between an undeployed configuration and a deployed configuration. The nacelle includes a nacelle body having a nacelle outer surface including facet elements and transition elements, each facet element extending aft from the hub element, each adjacent pair of facet elements being circumferentially spaced from one another by a corresponding transition element, each facet element having a first curvature with respect to the rotor axis, each transition element having a second curvature with respect to the rotor axis. The first curvature is different from the second curvature. In the undeployed configuration, each rotor blade is in overlying and fully external relationship with respect to a corresponding facet element.

    SYSTEM AND METHOD FOR TRACKING AND CLASSIFYING MOVING OBJECTS
    4.
    发明公开
    SYSTEM AND METHOD FOR TRACKING AND CLASSIFYING MOVING OBJECTS 审中-公开

    公开(公告)号：US20240221180A1

    公开(公告)日：2024-07-04

    申请号：US18558218

    申请日：2022-04-05

    Applicant: Israel Aerospace Industries Ltd.

    Inventor： Tal SIAK ,  Anna GULITSKI ,  Yaacov TAVGER

    IPC: G06T7/20 ,  G01S17/89 ,  G06T5/20 ,  G06V10/25 ,  G06V10/762 ,  G06V10/764

    CPC classification number: G06T7/20 ,  G01S17/89 ,  G06T5/20 ,  G06V10/25 ,  G06V10/762 ,  G06V10/764 ,  G06V2201/07

    Abstract: A system and method for tracking moving objects located within an area of interest are described. A sequence of periodic frames of the area is generated from LiDAR measurements. The sequence includes preliminary periodic and periodic operational frames. Each periodic frame includes point cloud data including static object data and dynamic object data. The static data are filtered out by applying a pattern mask generated by using the predetermined number of the preliminary periodic frames. For each periodic operational frame, clusters of points related to the dynamic object data are generated. Tracks of the moving objects are constructed from clusters related to the same object. The clusters are obtained for a predetermined number of the periodic operational frames. Each cluster is defined by a characteristics vector associated with a moving object in a corresponding periodic operational frame. Each characteristics vector includes cluster parameters associated with the corresponding moving object.

    LAUNCH SYSTEM AND METHOD
    5.
    发明公开
    LAUNCH SYSTEM AND METHOD 审中-公开

    公开(公告)号：US20240199237A1

    公开(公告)日：2024-06-20

    申请号：US17909824

    申请日：2021-04-05

    Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.

    Inventor： Aharon Yifrach

    IPC: B64G1/00 ,  B64C30/00 ,  B64D5/00 ,  B64G1/64 ,  F02K7/14 ,  F02K7/18

    CPC classification number: B64G1/005 ,  B64C30/00 ,  B64D5/00 ,  B64G1/641 ,  B64G1/645 ,  F02K7/14 ,  F02K7/18

    Abstract: A launch system is provided, including a composite vehicle and a carrier vehicle. The composite vehicle includes a payload vehicle, a booster vehicle and a first coupling system. The payload vehicle is configured for powered spaceflight at least in a space medium, and includes a rocket driven propulsion system. The booster vehicle is configured for powered supersonic/hypersonic aerodynamic flight, includes a ramjet propulsion system, and is configured for transporting the composite vehicle between a first altitude and a second altitude under propulsive power provided by the ramjet propulsion system. The first coupling system is configured for selectively coupling and decoupling the payload vehicle with respect to the booster vehicle. The carrier vehicle is configured at least for powered subsonic/transonic/supersonic aerodynamic flight, and for transporting the composite vehicle to at least the first altitude from a ground location. The launch system also includes a second coupling system for selectively coupling and decoupling the composite vehicle with respect to the carrier aircraft.

    Removable floor system with auxiliary fuel tanks for an aircraft
    7.
    发明授权
    Removable floor system with auxiliary fuel tanks for an aircraft 有权

    公开(公告)号：US11866190B2

    公开(公告)日：2024-01-09

    申请号：US17252898

    申请日：2019-06-18

    Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.

    Inventor： Iftach Zadaka ,  Yossi Guetta ,  Uri Pinhasi

    IPC: B64D37/04 ,  B64C1/18 ,  B64D37/08 ,  B64D37/32 ,  B64C27/04

    CPC classification number: B64D37/04 ,  B64C1/18 ,  B64C27/04 ,  B64D37/08 ,  B64D37/32

    Abstract: 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.

    Aerial vehicle securing system and method
    9.
    发明授权
    Aerial vehicle securing system and method 有权

    公开(公告)号：US11548657B2

    公开(公告)日：2023-01-10

    申请号：US16980541

    申请日：2019-03-11

    Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.

    Inventor： Gil Gelman ,  David Elnekave ,  Yoav Herzig

    IPC: B64F1/12 ,  B64F1/22 ,  B64C39/02

    Abstract: An aerial vehicle securing system for use with a base portion of an aerial vehicle, comprising: at least one substantially flat platform for supporting said base portion upon landing of the vehicle thereon; at least one magnetizable element configured to be integrated in one of said platform or base portion; at least one electropermanent magnet configured to be integrated in another one of said platform or base portion, said electropermanent magnet configured for generating a magnetic field, so that upon a distance between said base portion and said platform reaching a pre-determined value during the landing of the vehicle on the platform, said magnetic field is configured to cause magnetizable element to be attracted to at least said one electropermanent magnet; and a power supply module configured for generating an electric current to said at least one electropermanent magnet for selectively generating and cancelling said magnetic field.

    SYSTEMS AND METHODS OF IMAGE ACQUISITION
    10.
    发明申请
    SYSTEMS AND METHODS OF IMAGE ACQUISITION 有权

    公开(公告)号：US20220385824A1

    公开(公告)日：2022-12-01

    申请号：US17775450

    申请日：2020-09-30

    Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.

    Inventor： Erez YACOBY

    IPC: H04N5/232

    Abstract: An imaging method which comprises, while a line of sight of a camera is maintained fixedly oriented towards a target, controlling the camera to acquire an image by a sensor located at a current position relative to the camera, sending a command to an actuator of the sensor, for inducing a motion of the sensor relative to the camera along at least one direction, from the current position to a new position, controlling the camera to acquire an image by each of the pixel bands of the sensor, wherein motion of the sensor is performed during a first period of time, and the sensor is retained stationary at the new position during a second period of time, wherein acquisition of the image is performed during a third period of time, wherein a majority of the third period of time is within the second period of time.

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