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Matches 101 - 150 out of 62,256

Document Document Title
WO/2024/046052A1
The present invention relates to the technical field of unmanned aerial vehicles. Disclosed are an environmental control system based on an unmanned aerial vehicle and an unmanned aerial vehicle. The system comprises a light and device c...  
WO/2024/049387A1
The present invention relates to a body (2); at least one engine (3) on the body (2), which generates the necessary force for the flight of the air vehicle (1); at least one rotor (4) capable of rotating around itself, connected with the...  
WO/2024/049376A1
This invention is related to the artificial intelligence-based drone fish detection system and algorithm, which provides detailed detection of fish herds, etc. marine creatures by means of drones and its feature is; the propellers positi...  
WO/2024/050201A1
Methods and systems for providing automated asset management are provided. In embodiments, an asset data collector is configured to automatically collect asset data associated with assets in an intermodal facility according to a mission ...  
WO/2024/047221A1
The invention relates to an aircraft-seat device comprising: a mount unit (12a; 12b; 12c; 12d; 12e; 12f; 12g; 12h), which is provided for mounting on a cabin floor and has at least one cross member (22a, 24a; 22b, 24b; 22c, 24c; 22d, 24d...  
WO/2024/047413A1
A human powered aircraft comprising: -A fuselage (a) in which a nacelle (3) is defined; -at least one wing fastened to the fuselage (2); -at least a first propeller (5) adapted to be moved to rotate about a first propeller axis (e_l); -a...  
WO/2024/047222A1
The invention relates to a passenger seat device with a stand unit (12a; 12b; 12c; 12d; 12e; 12f), which is intended for mounting on a cabin floor, having a backrest (34a, 34b; 34c; 34d; 34e; 34f), and having a mounting device (42a; 42b;...  
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...  
WO/2024/046550A1
Disclosed is a passenger drone (1) for transporting winter sportspeople (45) with winter sports gear (46) strapped to their feet, the passenger drone (1) comprising a load drone (2) to which a suspension structure (3) can be preferably d...  
WO/2024/050065A1
An apparatus for frangibly supporting an object to a base includes a lower part comprising a base coupling portion and a lower engagement portion and an upper part comprising an object coupling portion and an upper engagement portion. Th...  
WO/2024/048341A1
An EPU (50) has a motor device (60), an inverter device (80), a unit housing (101), and a cooling device (800). The motor device (60) has a motor (61) and a motor housing (70). The inverter device (80) has an inverter (81) and an inverte...  
WO/2024/045360A1
A seat (100) and an aircraft (200). The seat (100) comprises a body (10) and a first honeycomb core (31). The first honeycomb core (31) has a first side (311) and a second side (312) facing away from each other, the first honeycomb core ...  
WO/2024/049386A1
The present invention relates to a body (2); at least one wing (3) located on the body (2); at least one icebreaker (4) on the wing (3), which enables the ice formed on the wing (3) surface to be removed from the wing (3) surface; an act...  
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 ...  
WO/2024/043092A1
A malfunction indicator diagnosing device (20) diagnoses a malfunction indicator of a battery (106) provided to an eVTOL (100). The malfunction indicator diagnosis device (20) comprises: a malfunction indicator determination unit (23); a...  
WO/2024/044199A1
A measuring device, method of measuring, and transport vessel including the measuring device measuring the ground effect region for the vessel in real time and controlling the transport vessel, e.g., a Wing In Ground Effect (WIG) vessel,...  
WO/2024/042029A1
The present invention provides a system for laying up a first plurality of pre-manufactured elements in a mold for a fibre-reinforced wind turbine blade part. The system comprises: a mold for forming the fibre-reinforced wind turbine bla...  
WO/2024/008207A9
The present invention specifically relates to the technical field of plant-protection unmanned aerial vehicles. Disclosed is an agricultural plant-protection unmanned aerial vehicle, comprising an unmanned aerial vehicle housing. Six sup...  
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...  
WO/2024/043848A1
The invention relates to a weapon integration apparatus (3) that can be rotated in a horizontal/vertical plane to direct the weapon (2) to the target by being connected to the transportation area opening (1) of military aircraft such as ...  
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...  
WO/2024/043164A1
Provided are a device and method for cleaning an aircraft, the device comprising a movable running trolley, a cleaning member that can rotate around an axis following a horizontal direction on the running trolley, a raising/lowering devi...  
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...  
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 ...  
WO/2024/042323A1
There is described an aircraft landing gear including an impact shield for protecting a first element of the landing gear from debris impact, the shield being pivotably connected to a second element of the landing gear different from the...  
WO/2024/040407A1
A ducted aircraft (100) and a duct (10) thereof. The ducted aircraft (100) comprises a duct (10), a fuselage (20), and power assemblies (30). The duct (10) comprises at least two duct units (11). The duct units (11) are each provided wit...  
WO/2024/041838A1
The invention relates to an assembly (1) of an electric motor (2) for propelling an aircraft and a control device (5), the electric motor (2) comprising a stator (21) and a rotor (22) and at least one cooling channel (CR) configured to b...  
WO/2024/042287A1
The invention relates to a device for separating a second part (14) from a first part (12), comprising a first interface (16) intended to be attached to the first part and a second interface (18) intended to be attached to the second par...  
WO/2024/041584A1
A rotary aircraft launching apparatus and system, comprising a support body (1), at least one rotary body (2) rotating about the axis of the support body (1), and a driving apparatus (4) for supplying power for the rotation of the rotary...  
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 ...  
WO/2024/043207A1
Provided are an aircraft coating removal device and method. The device comprises: a travel cart that can move; a blast head that is mounted on the travel cart and that can spray a blast material; a raising/lowering device that can move t...  
WO/2024/040482A1
A gimbal, a gimbal camera (400) and an unmanned aerial vehicle. The gimbal specifically comprises: a first driving mechanism (10), which is used for driving a photographing device (20) to rotate about a first rotary shaft; a base (11), w...  
WO/2024/041370A1
The present invention relates to the technical field of aircrafts. Disclosed are an aircraft state indication method, an aircraft, and a storage medium. The aircraft state indication method comprises: when a preset condition is satisfied...  
WO/2024/042293A1
The present application relates to a blade (3) of a static vane assembly (2) of a turbine engine (1) comprising: - a blade root (8) comprising a fibrous reinforcer (13) comprising a first skin (12) and a second skin (12) separated by a c...  
WO/2024/044220A1
Embodiments are directed, to low-profile, low-weight cargo loader, including a pair of cargo loaders including a first cargo loader arranged in tandem with a second cargo loader in a first orientation..According to an embodiment, each of...  
WO/2024/043093A1
This prediction device (20) predicts the required performance and/or state of a battery, which is a driving apparatus installed in an eVTOL. The prediction device (20) comprises: an acquisition unit (21) that acquires information includi...  
WO/2024/041934A1
The invention relates to a device (1) for cleaning fuel in a tank (92) of an aircraft (90), and use thereof. The device has a predetermined flow direction (2) for the fuel and comprises units arranged in a fluid-connected manner to forwa...  
WO/2024/042309A1
Air data estimation involves determining values of air data parameters such as airspeed, altitude, angle of attack and angle of sideslip. Accurate determination of air data parameter values is crucial to enable accurate control of an air...  
WO/2024/040466A1
A flight control method, an apparatus, an unmanned aerial vehicle, and a storage medium. The method comprises: in a flight state, determining whether a collision of an unmanned aerial vehicle occurs (31); and, when it is determined that ...  
WO/2024/039824A1
Systems and methods for flight control on an electric aircraft. The system includes a propulsor configured to generate lift to propel an electric aircraft, a pilot input mechanically coupled to the electric aircraft, a sensor communicati...  
WO/2024/037831A1
The invention relates to an air data indicating and calibrating arrangement (1) and method for a vertical take-off and landing aircraft, in particular a helicopter (50), for providing information on an air speed of the vertical take-off ...  
WO/2024/038247A1
A fuel delivery device for air-to-air refuelling, the device comprising: a fuel outlet; and an optical transceiver, wherein the optical transceiver is configured to: illuminate the fuel delivery device to provide visual indication to an ...  
WO/2024/038249A1
A flow body unit (600) for a fluid flow rig (10) for simulating fluid flow patterns; the flow body unit (600) comprising: a flow body support frame (700); a core member (800) extending from the flow body support frame (700) along a flow ...  
WO/2024/039423A1
A linear actuation system includes a pin pivotably coupled to an output rod of a linear motion actuator and a rotatable output shaft that includes a bushing therein. The pin can be configured to slide in and out of the bushing in respons...  
WO/2024/038189A1
The present invention relates to a system (40) for redistributing power in an aircraft with at least two electrical powertrain units (10), each powertrain unit (10) comprises a propulsion unit (15) powered by an energy storage unit (13);...  
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...  
WO/2024/038756A1
In a passive radar satellite 1, one or a plurality of radar openings 18 are attached to a satellite bus unit 14 by way of a radar opening drive device 17 having a variable attachment angle, wherein: in the radar openings 18, one or a plu...  
WO/2024/037875A1
The invention relates to a pivoting wing (1) for an aircraft (13), characterised in that the pivoting wing (1) is designed as a partial profile pivoting wing, wherein the partial profile pivoting wing is assembled from individual partial...  
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...  
WO/2024/038489A1
[Problem] The ability to acquire information useful for the flight of an aircraft is demanded. [Solution] In the present invention, terminal devices 600 provided in the cabin space of a target aircraft 810 each comprises a sensor unit 68...  

Matches 101 - 150 out of 62,256