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    Hybrid multicopter and fixed wing aerial vehicle
    1.
    发明授权
    Hybrid multicopter and fixed wing aerial vehicle 有权

    公开(公告)号：US10035591B2

    公开(公告)日：2018-07-31

    申请号：US15837614

    申请日：2017-12-11

    Applicant: Coriolis Games Corporation

    Inventor： Jacob Apkarian

    IPC: B64C29/00 ,  B64C39/02 ,  B64F5/10

    CPC classification number: B64C29/0033 ,  B64C27/20 ,  B64C27/52 ,  B64C39/024 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/146 ,  B64C2201/162 ,  B64C2211/00 ,  B64F5/10

    Abstract: An aerial vehicle is includes a wing, first and second rotors, and a movement sensor. The first and second multicopter rotors are rotatably coupled to the wing, the first multicopter rotor is rotatable relative to the wing about a first lateral axis, and the second multicopter rotor is rotatable relative to the wing about a second lateral axis. Each multicopter rotor is coupled to each other multicopter rotor, wherein the multicopter rotors are restricted to collective synchronous rotation relative to the wing between a multicopter configuration and a fixed-wing configuration. The movement sensor is coupled to the multicopter rotors, wherein the movement sensor is positioned to rotate relative to the wing when the multicopter rotors rotate relative to the wing between the multicopter and fixed-wing configurations.

    Hybrid multicopter and fixed wing aerial vehicle
    2.
    发明授权
    Hybrid multicopter and fixed wing aerial vehicle 有权

    公开(公告)号：US09873508B2

    公开(公告)日：2018-01-23

    申请号：US15585743

    申请日：2017-05-03

    Applicant: Coriolis Games Corporation

    Inventor： Jacob Apkarian

    IPC: B64C29/00 ,  B64C39/02 ,  B64F5/10

    CPC classification number: B64C29/0033 ,  B64C27/20 ,  B64C27/52 ,  B64C39/024 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/146 ,  B64C2201/162 ,  B64C2211/00 ,  B64F5/10

    Abstract: An aerial vehicle is includes a wing, first and second rotors, and a movement sensor. The first and second multicopter rotors are rotatably coupled to the wing, the first multicopter rotor is rotatable relative to the wing about a first lateral axis, and the second multicopter rotor is rotatable relative to the wing about a second lateral axis. Each multicopter rotor is coupled to each other multicopter rotor, wherein the multicopter rotors are restricted to collective synchronous rotation relative to the wing between a multicopter configuration and a fixed-wing configuration. The movement sensor is coupled to the multicopter rotors, wherein the movement sensor is positioned to rotate relative to the wing when the multicopter rotors rotate relative to the wing between the multicopter and fixed-wing configurations.

    SIMULATED FIREARM WITH TARGET ACCURACY DETECTION, AND RELATED METHODS AND SYSTEMS
    3.
    发明申请
    SIMULATED FIREARM WITH TARGET ACCURACY DETECTION, AND RELATED METHODS AND SYSTEMS 审中-公开

    公开(公告)号：US20170321987A1

    公开(公告)日：2017-11-09

    申请号：US15585459

    申请日：2017-05-03

    Applicant: Coriolis Games Corporation

    Inventor： Jacob Apkarian

    IPC: F41A33/02 ,  F41G3/26

    Abstract: A simulated firearm includes a body, a camera, a memory, and a processor. The body has a handle, a trigger, and a barrel portion. The barrel portion defines a shooting axis. The camera is coupled to the body and aligned with the shooting axis. The camera is configured to capture an image in response to actuation of the trigger. The memory is coupled to the body and stores marker data corresponding to at least one target marker. The processor is coupled to the body and configured to determine whether a portion of the image captured by the camera matches any one or more of the at least one target marker.

    Hybrid multicopter and fixed wing aerial vehicle
    4.
    发明授权
    Hybrid multicopter and fixed wing aerial vehicle 有权

    公开(公告)号：US10239611B2

    公开(公告)日：2019-03-26

    申请号：US16021800

    申请日：2018-06-28

    Applicant: Coriolis Games Corporation

    Inventor： Jacob Apkarian

    IPC: B64C29/00 ,  B64C27/20 ,  B64F5/10 ,  B64C39/02 ,  B64C27/52

    Abstract: An aerial vehicle is includes a wing, first and second rotors, and a movement sensor. The first and second multicopter rotors are rotatably coupled to the wing, the first multicopter rotor is rotatable relative to the wing about a first lateral axis, and the second multicopter rotor is rotatable relative to the wing about a second lateral axis. Each multicopter rotor is coupled to each other multicopter rotor, wherein the multicopter rotors are restricted to collective synchronous rotation relative to the wing between a multicopter configuration and a fixed-wing configuration. The movement sensor is coupled to the multicopter rotors, wherein the movement sensor is positioned to rotate relative to the wing when the multicopter rotors rotate relative to the wing between the multicopter and fixed-wing configurations.

    HYBRID MULTICOPTER AND FIXED WING AERIAL VEHICLE
    6.
    发明申请
    HYBRID MULTICOPTER AND FIXED WING AERIAL VEHICLE 有权

    公开(公告)号：US20170233069A1

    公开(公告)日：2017-08-17

    申请号：US15585743

    申请日：2017-05-03

    Applicant: Coriolis Games Corporation

    Inventor： Jacob Apkarian

    IPC: B64C29/00 ,  B64F5/10 ,  B64C39/02

    CPC classification number: B64C29/0033 ,  B64C27/20 ,  B64C27/52 ,  B64C39/024 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/146 ,  B64C2201/162 ,  B64C2211/00 ,  B64F5/10

    Abstract: An aerial vehicle is includes a wing, first and second rotors, and a movement sensor. The first and second multicopter rotors are rotatably coupled to the wing, the first multicopter rotor is rotatable relative to the wing about a first lateral axis, and the second multicopter rotor is rotatable relative to the wing about a second lateral axis. Each multicopter rotor is coupled to each other multicopter rotor, wherein the multicopter rotors are restricted to collective synchronous rotation relative to the wing between a multicopter configuration and a fixed-wing configuration. The movement sensor is coupled to the multicopter rotors, wherein the movement sensor is positioned to rotate relative to the wing when the multicopter rotors rotate relative to the wing between the multicopter and fixed-wing configurations.

    HYBRID MULTICOPTER AND FIXED WING AERIAL VEHICLE
    8.
    发明申请
    HYBRID MULTICOPTER AND FIXED WING AERIAL VEHICLE 审中-公开

    公开(公告)号：US20180099742A1

    公开(公告)日：2018-04-12

    申请号：US15837614

    申请日：2017-12-11

    Applicant: Coriolis Games Corporation

    Inventor： Jacob Apkarian

    IPC: B64C29/00 ,  B64F5/10 ,  B64C39/02

    CPC classification number: B64C29/0033 ,  B64C27/20 ,  B64C27/52 ,  B64C39/024 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/146 ,  B64C2201/162 ,  B64C2211/00 ,  B64F5/10

    Abstract: An aerial vehicle is includes a wing, first and second rotors, and a movement sensor. The first and second multicopter rotors are rotatably coupled to the wing, the first multicopter rotor is rotatable relative to the wing about a first lateral axis, and the second multicopter rotor is rotatable relative to the wing about a second lateral axis. Each multicopter rotor is coupled to each other multicopter rotor, wherein the multicopter rotors are restricted to collective synchronous rotation relative to the wing between a multicopter configuration and a fixed-wing configuration. The movement sensor is coupled to the multicopter rotors, wherein the movement sensor is positioned to rotate relative to the wing when the multicopter rotors rotate relative to the wing between the multicopter and fixed-wing configurations.

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