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WO/2024/054195A1 |
A closed-wing vertical take-off and landing aircraft comprising: a fuselage (1); a tail unit comprising two angularly inclined stabilizers (12); and a closed wing, comprising a front wing formed by two planes (2) mounted to the fuselage ...
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WO/2024/050552A1 |
Devices, systems and methods that are configured to use image processing to detect structural changes in infrastructure assets are described. An example method for identifying damage in an infrastructure asset includes receiving multitem...
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WO/2024/050178A2 |
A unmanned aerial vehicle (UAV) includes a fuselage including a top, a. bottom, a cavity that forms a cargo bay between the top and the bottom, and a lower access opening in the bottom for lowering a payload from the cargo bay. A movable...
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WO/2024/046666A1 |
The invention relates to a seat unit (10) for a transport vehicle comprising - a seat comprising a seat-base and a backrest (12.2), - an induction charging housing (30) for a portable electronic device (31) having a vertical orientation,...
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WO/2024/048342A1 |
This 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 inver...
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WO/2024/048196A1 |
This flying body includes a parachute and a sensor device that detects the flight state of the flying body, and the flying body is provided with: an ejection device capable of ejecting the parachute; and a controller that determines whet...
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WO/2024/046667A1 |
The invention relates to a seat unit (10) for a transport vehicle, comprising: - a seat comprising a seat-base and a backrest (12.2), and - an induction charging housing (30) for a portable electronic device (31) having a vertical orient...
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WO/2024/048101A1 |
An aircraft automatic control system according to an embodiment of the present invention comprises: a measuring unit which measures, as forecast information, a difference between a wind speed actually being experienced by the aircraft, a...
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WO/2024/050200A1 |
Methods and systems for providing mechanisms for automated inventory control are provided. In embodiments, an operational workflow for providing automated inventory control includes automated data collection and automated image data anal...
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WO/2024/045778A1 |
Provided is a space debris collision avoidance method taking an orbit altitude adjustment task into consideration. The method comprises: when a spacecraft has a requirement for consecutive orbital transfer, acquiring a collision risk val...
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WO/2024/047632A1 |
A package unloading and conveying system including a landing platform and one or more container aligning linear rails. The container aligning linear rails for aligning, on or above the landing platform and a hold of an aerial vehicle pla...
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WO/2024/049385A1 |
The present invention comprises a source (S) generating heat and/or radiation; a body (2) located on a space vehicle; at least one avionics chamber (A) on the body (2), in which the avionics equipment is provided; at least one panel (P) ...
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WO/2024/045724A1 |
An anti-crash rotor wing guide rail device for a tandem dual-rotor wing unmanned aerial vehicle, comprising a main beam (1), a rotor wing structure, a rotor wing guide rail device, a self-locking device (2), and a sensing device. The rot...
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WO/2024/045510A1 |
An invisible wing plate-shaped aircraft, comprising an outer balance bin (1), an invisible wing plate-shaped disc (2), a power bin (3) and a cockpit (4), wherein an electric motor (12) is arranged in an upper part of the cockpit; the inv...
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WO/2024/047324A1 |
The present invention provides an alignment device for aligning a corner-casting during installation. The alignment device comprises a body adapted to fit within a corner-casting aperture and to engage with the edges of the aperture with...
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WO/2024/049374A1 |
This invention concerns the autonomous flying rescue cabin, which can be used to quickly reach hard-to-reach places and bring the injured to the hospital after the intervention and its feature is; a chassis (1) containing batteries and t...
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WO/2024/046050A1 |
Disclosed in the present invention are a device power source system of an aircraft, and an aircraft. The system comprises: a first power manage unit (PMU), a second PMU, a third PMU and a power control unit (PCU), which are connected to ...
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WO/2024/049372A1 |
An air traffic control system for providing air traffic control of a group of balloons having at least two hot air balloons (500), each having at least one position sensing unit (141), including at least one hot air balloon (500) navigat...
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WO/2024/047312A1 |
The invention relates to a method for producing a moulded part and to the three-dimensionally moulded part itself, comprising a composite material including a fibrous preform and a resin, the part having a cavity (230') filled with a cel...
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WO/2024/049384A1 |
The present invention relates to a source (S) generating heat and/or radiation; a body (2) located on a space vehicle; at least one avionics chamber (A) on the body (2), in which the avionics equipment is provided; at least one panel (P)...
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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...
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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...
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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...
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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 ...
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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...
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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...
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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;...
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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/2024/046550A1 |
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...
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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...
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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...
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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 ...
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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...
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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/2024/043092A1 |
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...
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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,...
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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...
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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...
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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/2024/043848A1 |
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 ...
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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/2024/043164A1 |
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...
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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/2024/042323A1 |
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...
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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...
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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...
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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...
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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...
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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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