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WO/2024/047279A1 |
The invention is an unmanned aircraft (1) that comprises an airframe (2), a propulsion engine with control and operating systems, two coaxial rotors (3a and 3b) that turn in opposite directions, a tail rotor (7), and a fixing arrangement...
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WO/2024/042894A1 |
Provided is a flying mobile body 1 that comprises a body 3 and a plurality of rotor blade units 2 mounted to the body 3. The rotor blade units 2 each have rotor blades 20 and a cylindrical body 10 that covers the rotor blades 20. During ...
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WO/2024/043459A1 |
This autonomous landing method for a drone using object recognition and camera angle control comprises the steps of: learning in advance, by a drone, to identify a landing pad through a preset deep learning algorithm; when the drone dete...
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WO/2024/044289A1 |
Controlling navigation of an autonomous unmanned aerial vehicle (UAV), commonly known as a drone, involves mathematical modeling and the resulting estimations. The autonomous UAV has one or more rotors, a wind sensor, and a controller fo...
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WO/2024/043501A1 |
The present invention relates to a drone delivery system provided with a kiosk and a station for drone control, the drone delivery system being characterized by comprising: a drone control device; a station (200) that provides drone stan...
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WO/2024/040945A1 |
The present invention relates to the technical field of inspection and defect detection, and relates to an automatic inspection and intelligent corrosion defect detection method and device for a spillway tunnel. The method comprises the ...
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WO/2024/041897A1 |
Present invention discloses a method for establishing a secured communication for an Unmanned Aerial Vehicle (UAV) (113). Further, the present disclosure discloses a user terminal (101), a server (111) and the UAV (113) to establish the ...
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WO/2024/038634A1 |
Provided is a flight method that makes it possible to prevent a collision of a drone and entanglement of a power supply cable. This flight control system relating to flight control of an electrically driven drone 3 that is connected to a...
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WO/2024/038362A1 |
Provided is a vertical take-off and landing unmanned aerial vehicle (VTOL UAV) comprising a body, a pair of wings pivotably attached to the body with at least one pair of front rotors mounted on the wings, a rear rotor pivotably attached...
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WO/2024/038582A1 |
An unmanned aerial vehicle according to the present invention comprises: an anchoring member which is capable of anchoring an article; a linear member which is connected to the anchoring member; and a reel on which the linear member is w...
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WO/2024/038811A1 |
A conveyance control method according to one aspect of the present disclosure is a method for lifting and conveying cargo via a plurality of flexible cables by using a plurality of unmanned aerial vehicles, each of which is capable of ge...
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WO/2024/033432A1 |
A method (700) by a user equipment, UE, (112) for communicating in a restricted zone includes determining (702) a location of the UE in relation to the restricted zone. Based on the location of the UE in relation to the restricted zone, ...
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WO/2024/035714A1 |
A compact and lightweight, drone delivery device propelled by an electric ducted air propulsion system. The device is called an ArcSpear Electric Jet Drone System and is relatively di f ficult to track in flight ( stealth), relatively fa...
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WO/2024/034498A1 |
Provided is a robot arm in which a first sensor detects the posture of a flying robot. The robot arm has a control unit that controls a second drive module, on the basis of a detection signal from the first sensor, and that thereby cause...
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WO/2024/035019A1 |
The present invention relates to a low-impact landing system for a rotary wing aircraft for reducing landing impact transmitted to an airframe (11) upon landing of a rotary wing aircraft (10), comprising: a landing platform (110) having ...
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WO/2024/028739A1 |
An unmanned aerial vehicle (UAV) comprising a rotor module comprising a coaxially arranged rotor having a substantially vertical axis of rotation and a laterally extending rotor housing, a battery located below the rotor module, a shaft ...
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WO/2024/024991A1 |
The present invention is to provide a remotely drone-controlled, battery-loaded surfboard, in which a plurality of batteries are loaded inside the surfboard, and a guide tube is suspended from the bottom of a drone in the air and has bui...
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WO/2024/021135A1 |
Provided in the embodiment of the present application is an aircraft, comprising: a center body; two arm assemblies, which are respectively arranged on opposite sides of the center body, and each of which is provided with a proximal end ...
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WO/2024/024815A1 |
This robot arm has a base end connected to a flying robot, and a tip connected to an end effector. At a plurality of locations between the base end and the tip of the robot arm, first joints that rotate about an axis parallel to a pitch ...
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WO/2024/025163A1 |
The present invention relates to a drone station having a function of guiding a drone to a correct position, the drone station comprising: a take-off/landing pad where a drone takes off and lands; and a plurality of landing skid movement...
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WO/2024/023855A1 |
A cleaning system (1) is described comprising: a pumping unit or pump (4) designed to pump out water or other similar fluids; an electric motor (3); a device (5) for regulating the revolutions of the pump (4) so that it delivers water at...
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WO/2024/022368A1 |
A cleaning unmanned aerial vehicle structure and a using method. A propeller unit (2), a telescopic unit (3), and a cleaning unit (1) are sequentially connected, during flight of the propeller unit (2), the cleaning unit (1) relies on it...
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WO/2024/019975A1 |
A method includes receiving a two-dimensional (2D) image captured by a camera on a unmanned aerial vehicle (UAV) and representative of an environment of the UAV. The method further includes applying a trained machine learning model to th...
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WO/2024/016767A1 |
A nest for an unmanned aerial vehicle. The nest is suitable for being arranged on a vehicle, and comprises: a nest body (100), which is used for accommodating an unmanned aerial vehicle; a charging device (200), which is arranged in the ...
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WO/2024/018392A1 |
A rotorcraft type UAV drone comprises a main body (1) which supports at least one rotor (2, 4) with blades (6) and at least one compressor (18, 20), integrated with each other and operated by the same driving force (10, 12), to generate ...
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WO/2024/019411A1 |
According to the present disclosure, a method by which an electronic device obtains image information about targets comprises the steps of: identifying, on the basis of information about a mission plan, flight time and a first flight pat...
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WO/2024/020096A1 |
The system can include: a vehicle 100 and a stabilizer 200. However, the system can additionally or alternatively include any other suitable set of components. The system functions to facilitate vehicular transport (e.g., via a cabin). A...
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WO/2024/020544A1 |
A photophoretically levitating macroscopic structure includes a photophoretically active structure (PAS), a PAS support framework, and a device superstructure. The photophoretically active structure includes at least one top sheet and at...
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WO/2024/015756A1 |
An unmanned aerial vehicle (UAV) including a fuselage body having a cavity that forms a cargo bay for transporting a payload, and a lower access opening for lowering the payload from the cargo bay, the lower access opening including a ca...
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WO/2024/015402A1 |
A method includes obtaining sensor data indicating a tension experienced by a tether while a payload coupling apparatus connected to the tether is lowered from an aerial vehicle using the tether. The method also includes determining, bas...
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WO/2024/012587A1 |
The present invention provides a device allowing for connecting, combining, and fixing, in particular an apparatus allowing for aerial connecting, combining, and fixing, and a method therefor and an application thereof. The device or app...
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WO/2024/014086A1 |
The present invention provides a payload management apparatus that calculates a weight that can safely be loaded on an aircraft of the rotary wing type, suppresses a decrease in transport efficiency, and increases flight safety of the ai...
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WO/2024/014459A1 |
Provided are a flying mobile body, a flight position estimation method, a computer program, and a flight position estimation system that make it possible to estimate a flight position of the flying mobile body with higher accuracy. The f...
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WO/2024/015732A1 |
An unmanned aerial vehicle (UAV) including a fuselage body having a cavity that forms a cargo bay for transporting a payload; an access opening positioned in the cargo bay adapted to receive the payload; a. winch system positioned in an ...
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WO/2024/015961A1 |
A unmanned aerial vehicle (UAV) includes a fuselage body including a cavity that forms a cargo bay for transporting a payload, an upper access opening for receiving the payload into the cargo bay from a first direction, and a lower acces...
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WO/2024/014613A1 |
An unmanned aerial vehicle control duplex system and method using a mobile communication network and RF communication are provided. An unmanned mobility system according to an embodiment of the present invention comprises: a ground contr...
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WO/2024/014644A1 |
Provided are a steering system and a method for simultaneous control of an unmanned aerial vehicle and a gimbal device. An unmanned moving system according to an embodiment of the present invention comprises: a ground control system that...
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WO/2024/014614A1 |
An image acquisition/pre-processing/transmission system and method based on an unmanned aerial vehicle are provided. An unmanned mobility system according to an embodiment of the present invention comprises: a ground control system for t...
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WO/2024/013413A1 |
The present invention relates to an unmanned aerial system for autonomously delivering and collecting products that is intended to optimise last-mile deliveries of goods and products to the final recipients and, furthermore, to drastical...
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WO/2024/011267A1 |
The invention relates to an aircraft (1) and to a method for controlling the aircraft (1), wherein: the aircraft (1) comprises a wing assembly (2); the wing assembly (2) is designed such that the wing assembly (2) generates lift (4) of t...
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WO/2024/013496A1 |
The present invention is concerned with an aircraft comprising an elongate fuselage for containing cargo or passengers. The fuselage comprises a lower floor and an upper ceiling and opposing fuselage sides extending between the ceiling a...
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WO/2024/015401A1 |
A method includes causing an aerial vehicle to deploy a tethered component to a particular distance beneath the aerial vehicle by releasing a tether connecting the tethered component to the aerial vehicle. The method also includes obtain...
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WO/2024/014615A1 |
An image file/transmission validity verification system and method based on an unmanned aerial vehicle are provided. An unmanned mobility system according to an embodiment of the present invention comprises: a ground control system for t...
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WO/2024/014645A1 |
Provided are a mobile communication network-based system and method for radio controlling an unmanned aerial vehicle. An unmanned mobile system according to an embodiment of the present invention comprises: a ground control system that t...
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WO/2024/010967A1 |
The disclosure provides an example charging nest for wireless power transfer to drones is disclosed. The charging nest includes (a) a housing having an opening at a first end, (b) a plurality of antennas arranged around a periphery of th...
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WO/2024/010856A1 |
A system for exploring unidentified aerial phenomena (UAP) includes a processor and a memory. The memory includes instructions stored thereon, which, when executed by the processor, cause the system to: access a UAP dataset comprising re...
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WO/2024/009443A1 |
A takeoff and landing site monitoring device (30) is configured to comprise: an image data acquisition unit (41) which acquires, from an imaging device (21) for imaging a takeoff and landing site (1), image data that represents an image ...
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WO/2024/009062A1 |
A drone (10) operable for flight. The drone has a fuselage (100) having a length (L) extending along an x-axis, the fuselage (100) comprising a port side fuselage section (102) spaced apart from a starboard side fuselage section (104) to...
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WO/2024/004158A1 |
Provided is an unmanned aircraft that has horizontal wings and that is compact overall. An unmanned aircraft 100 comprises: an unmanned aircraft body 101; a plurality of rotors 104A, 104B and 104C which each have a rotary shaft extendi...
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WO/2024/003620A1 |
A drone is disclosed having a low acoustic signature. The drone includes a fuselage, a main inboard wing attached to the fuselage, a pylon located towards an aft end of the fuselage and having an end that is higher than the main inboard ...
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