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WO/2024/057935A1 |
Provided is a rotary wing that is unlikely to be deformed by fluid. A rotary wing 1 comprises: a hub 10; a first blade 20, a second blade 30, and a third blade 40, being a plurality of blades which each have one end connected to the hub ...
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WO/2024/059113A1 |
A method of imparting anti-icing characteristics to an article includes combining a part A composition with a part B composition and a part C composition to form a ready-to-use composition; applying the ready -to-use composition on at le...
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WO/2024/059777A1 |
Conventional proprotor systems have a large region in the middle of the proprotor disk area that is occupied by the hub mounted systems including blade pitch control systems and blade retention systems. The hub-mounted systems use rotor ...
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WO/2024/055900A1 |
The present invention relates to the technical field of unmanned aerial vehicles, and provides a battery management system having a plurality of backup communication main units, and an aircraft. In the battery management system provided ...
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WO/2024/055381A1 |
A perching robot and a perching method of the perching robot. The perching robot relates to the technical field of robots, and comprises: a body (101), a control unit, a perching module (102) and a data acquisition unit (103); the contro...
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WO/2024/056549A1 |
The present invention relates to a system (10; 20; 30) for reconfiguring power distribution in an aircraft, the system comprises at least two propulsion units (3), at least two energy storage units (13) and an interconnecting network (15...
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WO/2024/056258A1 |
The invention relates to an item of furniture (30), in particular for an aircraft seat, comprising: -a frame (31), - a movable element (26), - a pivot connection (34) for rotating the movable element (26) relative to the frame (31) betwe...
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WO/2024/056929A1 |
The present invention relates to a smart device (100) for supplying ammonia and hydrogen for mixed combustion in aircraft, as shown in Figure 1, for propulsion. The smart device comprises a subassembly (120) that stores ammonia and suppl...
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WO/2024/052616A1 |
The invention relates to an actuator (20) designed to be connected to a mechanical flight control chain (13) of a vehicle, comprising a motor (22), a first output shaft (23) driven in rotation by the motor (22) about an axis of rotation ...
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WO/2024/054818A1 |
An unmanned vehicle includes at least one navigation sensor configured to measure navigation data indicative of an environment, at least one status sensor configured to measure status data indicative of operating parameters of a hardware...
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WO/2024/050585A1 |
The invention relates to a luggage compartment (1) for an aircraft, comprising: a luggage-compartment housing (2); a chute (6) for receiving an item of luggage (13); a joint (10) between the luggage-compartment housing (2) and the chute ...
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WO/2024/052286A1 |
The invention relates to a protective device (6) for protecting a protruding aerial part (3) of an anemobarometric sensor (1) comprising a sleeve (7) configured to protect said protruding part (3), a grab handle (8) comprising a bar that...
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WO/2024/054833A1 |
An unmanned aerial vehicle comprises a central body; at least one rotor motor configured to drive at least one propeller to rotate, rotation of the at least one propeller generating thrust and causing the unmanned aerial vehicle to fly; ...
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WO/2024/053047A1 |
The present invention comprises at least one processor that outputs information about a mission on a celestial body other than the Earth by executing the processing corresponding to the operation by a user in accordance with the operatio...
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WO/2024/053375A1 |
Provided are a flight device and a method for controlling the same, by which it is possible to accurately measure the power remaining in a battery with a simple configuration. A flight device 10 is provided with a rotor 11, a motor 12,...
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WO/2024/052237A1 |
The invention relates to a hybrid metal/plastic spring rod (1) comprising a guiding system (3) made up of a metal pin (4) and a plastic sliding body (5), a compression spring (2) and two plastic-moulded connecting members (6a, 6e). The c...
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WO/2024/052190A1 |
During the transition of a vertical take-off and landing (VTOL) aircraft (1) from hover flight to cruise flight and vice versa, a method for controlling this transition is configured to push propulsion units (2) of the VTOL aircraft (1) ...
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WO/2024/054197A1 |
The invention relates to space engineering and can be used in the creation of a suborbital rocket plane with substantially vertical takeoff and landing. A rocket plane comprises a body (1), movable front and rear aerodynamic control surf...
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WO/2024/052505A1 |
The invention relates to a wing arrangement (10) that comprises a main wing (12) and a slat (14) mounted to the main wing in front of the main wing (12) and counter to a direction of flow. A gap (16) with a flow inlet (18) and a flow out...
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WO/2024/054310A2 |
A method may include a first UAV of a plurality of UAVs flying a first vector comprising a first heading and speed; a second UAV of the plurality of UAVs flying a second vector comprising a second heading and speed; at a first time, whil...
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WO/2024/053327A1 |
Provided are a flying device and a control method therefor capable of suppressing a flight in a state in which the weight of a transported body is excessively large. A flying device 10 comprises a fuselage base portion 16, a rotor 11, ...
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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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