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Patent Searching and Data


Matches 51 - 100 out of 62,256

Document Document Title
WO/2024/058565A1
The present invention relates to a method for preventing drone battery degradation, and in particular, provides: an apparatus for preventing battery degradation caused by a momentary high output exceeding the rating of the battery, where...  
WO/2024/059215A1
A method includes receiving configuration data for an unmanned aerial vehicle (UAV) simulation system, the configuration data indicating at least one base location specification, at least one aircraft specification, and at least one virt...  
WO/2024/055899A1
A connector and method for connecting a motor and an arm of a multi-rotor aircraft. The connector comprises a base (1), a locking disk component (2), and a guided positioning component (3), wherein one side of the base (1) is connected t...  
WO/2024/058887A1
The present invention is directed to systems and methods for aerially detecting and identifying explosives on the ground, and more specifically systems and methods for detecting and identifying landmines and unexploded ordnance (UXO) on ...  
WO/2024/056959A1
The invention relates to a propeller blade or vane (10) for a turboprop engine, made from composite material and comprising a matrix-densified fibrous reinforcement, the propeller blade or vane comprising, in the direction of its span (D...  
WO/2024/055069A1
Provided is a hybrid aerial hydro drone (10) comprising a body (12) with a plurality of hydraulic thrusters (14) supported on an outer surface of the body (12) and configured to propel said body (12) in a marine environment. Drone (10) a...  
WO/2024/059230A1
An aircraft boarding vehicle to transport passengers between airport gate area and to a front door or a rear door of an airplane positioned on a tarmac of an airport without impeding ground transportation and plane traffic having a passe...  
WO/2024/055506A1
The present invention relates to the field of aviation machinery. Provided is a locking mechanism used for a helicopter tail cabin door. The locking mechanism comprises: two lock box assemblies, respectively installed on two sides of a t...  
WO/2024/056195A1
The present invention concerns a device for a multicopter that allows the multicopter to move without tipping over. This device generates propulsion according to the x- and/or Y-axis using the air displacement of the drive propellers and...  
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 ...  
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...  
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 ...  
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 ...  
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...  
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...  
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...  
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...  
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 ...  
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...  
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 ...  
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...  
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; ...  
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...  
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,...  
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...  
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) ...  
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...  
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...  
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...  
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, ...  
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 ...  
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...  
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...  
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,...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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) ...  
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...  
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...  
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...  
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...  
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 ...  
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...  
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...  
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)...  

Matches 51 - 100 out of 62,256