公开(公告)号：US20240350879A1

公开(公告)日：2024-10-24

申请号：US18136691

申请日：2023-04-19

Applicant: Matthew Zdunich

Inventor： Matthew Zdunich

IPC: A63B55/60 ,  A63B24/00 ,  A63B71/06 ,  B62B3/10 ,  B62B5/00 ,  B64U10/14 ,  B64U50/20 ,  B64U50/30 ,  G05D1/02 ,  G05D1/10 ,  G06T7/70 ,  G06V20/17 ,  G06V20/40 ,  G06V40/20 ,  G10L15/22 ,  H04N5/91 ,  H04N23/57 ,  H04R1/02

CPC classification number: A63B55/61 ,  A63B24/0006 ,  A63B24/0021 ,  A63B71/0622 ,  B62B3/102 ,  B62B5/00 ,  B62B5/004 ,  B62B5/0043 ,  B62B5/0069 ,  B64U10/14 ,  B64U50/20 ,  B64U50/30 ,  G06T7/70 ,  G06V20/17 ,  G06V20/42 ,  G06V40/23 ,  G10L15/22 ,  H04N5/91 ,  H04N23/57 ,  H04R1/028 ,  A63B2024/0028 ,  A63B2071/0625 ,  A63B2220/05 ,  A63B2220/806 ,  A63B2225/50 ,  B62B2202/406 ,  B64U2101/30 ,  G06T2207/10016 ,  G06T2207/10032 ,  G06T2207/30224 ,  G10L2015/223

Abstract: A golf caddy system for autonomously carrying a golf bag across a golf course, recording video of golf swings, and providing golfing advice to a user includes an autonomous motorized cart. The cart includes a processor with map data of the golf course in a memory of the processor and a global positioning system receiver for determining a current location of the cart. The cart also includes a camera which is configured to capture video of a golf swing.

公开(公告)号：US20240034490A1

公开(公告)日：2024-02-01

申请号：US18161760

申请日：2023-01-30

Applicant: KABUSHIKI KAISHA TOSHIBA

Inventor： Yutaka ASANUMA

IPC: B64U20/20 ,  B64U20/83 ,  B64U50/20 ,  B64U10/16 ,  B64C27/32

CPC classification number: B64U20/20 ,  B64U20/83 ,  B64U50/20 ,  B64U10/16 ,  B64C27/325 ,  B64U2201/10 ,  B64C2220/00

Abstract: According to one embodiment, a flying body includes a radar, a supporter, a plurality of rotors supported by the supporter, and a controller. The rotors include a first rotor. The radar is configured to perform a detection operation and a non-detection operation. The controller is configured to perform a first control operation in a first transition from the non-detection operation to the detection operation. The controller is configured to perform a first change in the first control operation to change a rotational speed of the first rotor from a rotational speed of the first rotor in the non-detection operation. The detection operation is performed after the first control operation.

公开(公告)号：US20240300680A1

公开(公告)日：2024-09-12

申请号：US17997581

申请日：2022-05-06

Applicant: ARASE AIZAWA AEROSPATIALE LLC

Inventor： Kunio ARASE

IPC: B64U50/20 ,  B64D27/04 ,  B64U50/10 ,  F01L1/02 ,  F01N13/10 ,  F02B75/24

CPC classification number: B64U50/20 ,  B64D27/04 ,  B64U50/11 ,  F01L1/026 ,  F01N13/10 ,  F02B75/24 ,  F01L1/047 ,  F01N2340/04 ,  F01N2590/00

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.

公开(公告)号：US20240166384A1

公开(公告)日：2024-05-23

申请号：US18388171

申请日：2023-11-08

Applicant: THALES

Inventor： Marc RIEDINGER ,  Eric GUILLOUET ,  Antoine BONNET ,  Patrick GOUHIER

IPC: B64U20/87 ,  B64U20/70 ,  B64U50/20 ,  G01S13/933

CPC classification number: B64U20/87 ,  B64U20/70 ,  B64U50/20 ,  G01S13/933

Abstract: An unmanned aircraft includes three parallel beams extending in at least one longitudinal direction X from a rear side to a front side of the aircraft, the central beam forming a main fuselage containing a powertrain, with a propeller of diameter D configured to be driven by the powertrain being attached to a front end of the central beam, each side beam being at a distance L/2 from the central beam and each side beam supporting a radar at a front end of the beam.

公开(公告)号：US20240336379A1

公开(公告)日：2024-10-10

申请号：US18681620

申请日：2022-10-06

Applicant: ISHIKAWA ENERGY RESEARCH CO., LTD.

Inventor： Mitsuru Ishikawa

IPC: B64U50/20 ,  B64U10/16 ,  B64U50/11 ,  B64U50/30

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.

公开(公告)号：US12097980B1

公开(公告)日：2024-09-24

申请号：US17997581

申请日：2022-05-06

Applicant: ARASE AIZAWA AEROSPATIALE LLC

Inventor： Kunio Arase

IPC: B64U50/20 ,  B64D27/04 ,  B64U50/11 ,  F01L1/02 ,  F01N13/10 ,  F02B75/24 ,  F01L1/047

CPC classification number: B64U50/20 ,  B64D27/04 ,  B64U50/11 ,  F01L1/026 ,  F01N13/10 ,  F02B75/24 ,  F01L1/047 ,  F01N2340/04 ,  F01N2590/00

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.

公开(公告)号：US11885769B2

公开(公告)日：2024-01-30

申请号：US17445367

申请日：2021-08-18

Applicant: Saudi Arabian Oil Company ,  KING ABDULLAH UNIVERSITY OF SCIENCE AND TECHNOLOGY

Inventor： Fadl Abdellatif ,  Jeff S. Shamma ,  Sultan Shaqaq ,  Abdullah Arab ,  Abdullah A. Alkhder ,  Sahejad Patel

IPC: G01N29/22 ,  B60F5/02 ,  G05D1/10 ,  G01N29/04 ,  G01N29/265 ,  B64U10/70 ,  B64U50/20 ,  F16D48/00 ,  B64U10/13 ,  B64U101/26

CPC classification number: G01N29/225 ,  B60F5/02 ,  B64U10/70 ,  B64U50/20 ,  G01N29/04 ,  G01N29/265 ,  G05D1/101 ,  B64U10/13 ,  B64U2101/26 ,  F16D48/00 ,  G01N2291/023

Abstract: An unmanned aerial vehicle (UAV) has a flight-only mode with a motor only rotating propellers and not rotating on-board wheels to configure the UAV to fly away from a surface of a structure, and a crawling-only mode in which the UAV is configured to crawl on the surface due to the motor only rotating the wheels while not rotating the propellers. In the flight-only mode, a clutch disengages a motor from the wheels so that the motor only engages the propellers to fly to lift from the surface. In the crawling-only mode, the clutch disengages the motor from the propellers so that the motor only engages the wheels to move the UAV on the surface.