ENGINE DEVICE FOR UNMANNED FLYING APPARATUS
    2.
    发明公开

    公开(公告)号:US20240300680A1

    公开(公告)日:2024-09-12

    申请号:US17997581

    申请日:2022-05-06

    Inventor: Kunio ARASE

    Abstract: An engine device for an unmanned flying apparatus that provides good weight balance for the flying apparatus; cancels the gyroscopic effect; and has auto rotating propellers.
    The engine device includes a first cylinder and a second cylinder arranged horizontally and opposed to each other, and pistons within the cylinders advance and retract in opposite directions to each other; a first crankshaft and a second crankshaft arranged in the vertical direction, driven by the first cylinder and the second cylinder, respectively, and rotate in opposite directions; a first centrifugal clutch and a second centrifugal clutch rotate in opposite directions to each other; a final drive shaft transmitting rotational force to a gear mechanism comprising orthogonal transform gears, to rotate a propeller shaft; a one-way clutch arranged between



    the first crankshaft, the second crankshaft and
    the final drive shaft, and driven by both the first crankshaft and the second crankshaft.

    FLIGHT DEVICE
    4.
    发明公开
    FLIGHT DEVICE 审中-公开

    公开(公告)号:US20240336379A1

    公开(公告)日:2024-10-10

    申请号:US18681620

    申请日:2022-10-06

    Inventor: Mitsuru Ishikawa

    CPC classification number: B64U50/20 B64U10/16 B64U50/11 B64U50/30

    Abstract: A flight device in which a mechanism for transmitting power is simplified is provided. The flight device 10 includes an airframe 19, main rotors 14, an engine 30, and power transmission shafts 25. The main rotors 14 are rotated to generate drive force that causes the airframe 19 to lift. The engine 30 includes crankshafts. The power transmission shafts 25 are connected to the crankshafts. Moreover, the engine 30 rotates the main rotors 14 via the power transmission shafts 25. The power transmission shafts 25 are tilted with respect to a second direction D2.

    Engine device for unmanned flying apparatus

    公开(公告)号:US12097980B1

    公开(公告)日:2024-09-24

    申请号:US17997581

    申请日:2022-05-06

    Inventor: Kunio Arase

    Abstract: An engine device for an unmanned flying apparatus that provides good weight balance for the flying apparatus; cancels the gyroscopic effect; and has auto rotating propellers.
    The engine device includes a first cylinder and a second cylinder arranged horizontally and opposed to each other, and pistons within the cylinders advance and retract in opposite directions to each other; a first crankshaft and a second crankshaft arranged in the vertical direction, driven by the first cylinder and the second cylinder, respectively, and rotate in opposite directions; a first centrifugal clutch and a second centrifugal clutch rotate in opposite directions to each other; a final drive shaft transmitting rotational force to a gear mechanism comprising orthogonal transform gears, to rotate a propeller shaft; a one-way clutch arranged between



    the first crankshaft, the second crankshaft and
    the final drive shaft, and driven by both the first crankshaft and the second crankshaft.

    CONTROL DEVICE, DRONE, CONTROL METHOD, AND RECORDING MEDIUM

    公开(公告)号:US20250037590A1

    公开(公告)日:2025-01-30

    申请号:US18714139

    申请日:2021-12-16

    Abstract: A control device that includes a sensing unit that detects, from an image captured by a camera mounted in a drone, a guide light to be used for forming a corridor used by the drone, and identifies a position of the detected guide light, a calculation unit that calculates, according to positions of the drone and the guide light, a predicted arrival position of the drone and a control target position according to a positional relationship between the drone and the guide light at a control timing subsequent to a timing of capturing the image, a control condition generation unit that generates a control condition for a motor that drives a propeller of the drone according to the predicted arrival position and the control target position, and a control condition setting unit that sets the control condition for the motors of the drone.

    DRONE PROPULSION SYSTEM
    9.
    发明公开

    公开(公告)号:US20240286775A1

    公开(公告)日:2024-08-29

    申请号:US18113436

    申请日:2023-02-23

    Applicant: Colin Ho-Shing

    Inventor: Colin Ho-Shing

    Abstract: A propulsion system includes a motor, the motor disposed at a center portion of the propulsion system, the motor further including a rotor shaft. The system includes a splitter gearbox coupled to the rotor shaft, the splitter gearbox further comprising at least one splitter output shaft. The system includes at least one continuously variable transmission (CVT), the CVT coupled to the splitter output shaft, the CVTs further including a driveshaft. The system includes at least one bevel gearbox, the bevel gearbox comprising a bevel gearbox input shaft and a bevel gearbox output shaft, the bevel gearbox input shaft disposed parallel to the horizontal plane and the bevel gearbox output shaft disposed at an angle to the bevel gearbox input shaft, wherein the bevel gearbox input shaft is coupled to the driveshaft. The system includes at least one propeller coupled to the bevel gearbox output shaft.

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