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WO/2024/087315A1 |
Provided is a flying automobile (100). The flying automobile (100) comprises an automobile body (10), and a flight power system (20) and a land power system (30) which are connected to the automobile body (10). The flying automobile (100...
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WO/2024/090940A1 |
A method for guiding landing of an unmanned aerial vehicle and a system to which the method is applied are provided. One of several embodiments according to the present disclosure provides a method for guiding landing of an unmanned aeri...
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WO/2024/085438A1 |
The present invention relates to a reverse propulsion overtilting tiltrotor drone, which is an unmanned aerial vehicle, consisting of: a main body (10); wings (20) extending from both sides of the main body (10); a tilt rotor (30) provid...
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WO/2024/084222A1 |
The present invention concerns a system for positioning an airborne vehicle (502) at a geographic location, the system comprising the airborne vehicle (502) having one or more infra-red ( I R) detectors, and a positioning beacon (504) lo...
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WO/2024/083756A1 |
The present invention relates to a crash handling system (10) for an aircraft, comprising an altitude surveillance system (20), which is adapted to receive altitude data from at least one altitude sensor (22) and to issue an altitude war...
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WO/2023/059427A9 |
The systems/methods analyze the vast reservoir of data that is collected in-flight during a commercial aircraft's travels over several months. That data is analyzed to identify and remove data points that do not represent stable cruise. ...
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WO/2024/077280A1 |
An electric propulsion system for a vertical takeoff-and-landing aircraft having an inverter assembly, a gearbox assembly, an electric motor assembly. The inverter assembly, the gearbox assembly, and the electric motor assembly may be su...
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WO/2024/069095A1 |
Device (210) for measuring a rotational speed of an aircraft propeller (211), comprising: - an optical speed sensor (220); - an optical fiber (230) connected to the optical speed sensor and intended to be connected to a control unit of t...
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WO/2024/072355A1 |
The present invention relates to a body (2) on an air vehicle; at least one actuator (3) on the body (2), which enables avionics equipment to move; at least one detector (4) positioned on the body (2) by means of at least two actuators (...
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WO/2024/072533A2 |
A system may include a plurality of unmanned aerial vehicles (UAVs), the plurality of UAVs including a first UAV and a second UAV. The system may include at least one recharging station and a ground station configured to, during a missio...
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WO/2024/062704A1 |
The recording control device according to the present embodiment comprises: a video data acquisition unit (103) that acquires video data obtained by capturing a region including the periphery of a mobile body; an event detection unit (10...
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WO/2024/061514A1 |
The invention relates to a system for detecting a psychological state (10) of a passenger, comprising: - at least one detection sensor (11) capable of detecting at least one physiological parameter of the passenger, in particular a physi...
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WO/2024/058566A1 |
The present invention relates to a way to prevent the deterioration of batteries in drones, and in particular, provides a power distribution circuit for preventing the deterioration of a battery due to an instantaneous high output power ...
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WO/2024/057746A1 |
An operation control unit 11 controls a flight drive mechanism 1009 so as to perform an operation by which detection values of respective sensors included in a sensor group 1007 provided to a drone 10 match target values. A detection uni...
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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...
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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/2024/052286A1 |
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/2024/048196A1 |
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/2024/043092A1 |
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/2024/043459A1 |
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/2024/041370A1 |
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...
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WO/2024/033273A1 |
According to one aspect, the present disclosure relates to a device for reducing the electric charge of a space vehicle, the device comprising: a substrate (201) made of a conductor or semiconductor which is configured to be electrically...
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WO/2024/028571A1 |
An aircraft landing gear assembly comprising an oleo-pneumatic shock absorber (50) comprising an outer cylinder (52) and sliding tube (54) movable between a compressed position and an extended position, further comprising a sprung elemen...
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WO/2024/028573A1 |
An aircraft landing gear shock absorber strut (50) comprising: an outer cylinder (52) and a sliding tube (54) being movably mounted within the outer cylinder so as to be movable between a compressed position and an extended position, fur...
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WO/2024/028572A1 |
An aircraft landing gear shock absorber strut (50) comprising: an outer cylinder (52) defining an oleo chamber (O) for containing pressurised oleo-pneumatic shock absorber fluid; a sliding tube (52) including a piston head (56) movably m...
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WO/2024/023462A1 |
The invention relates to a method for monitoring a propulsion system (102) of an aircraft (100), comprising: - computing a margin of a parameter (NG, T4x) of a thermal chain (TH), this margin being taken as margin (PMD1, PMT1) of the the...
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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/2024/013482A1 |
The present invention relates to an Electronic Unit (1), EU, for a tactile cueing apparatus for a vehicle. The tactile cueing apparatus augments feel for an operator of the vehicle. The EU comprises a first channel (307A, 407A). The firs...
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WO/2023/238194A1 |
This drone with a Faraday cage comprises: a conductor 30 which is in a grid form, exposes propellers 11 to the outside, and surrounds a drone body 10 (control unit); a lightning rod 31 which is arranged on the conductor 30 and is used to...
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WO/2023/240019A1 |
Provided is a passenger service unit (108) for an aircraft. The passenger service unit (108) includes a panel body (110) having a first surface, a second surface opposite the first surface, and at least two air passages (146, 148, 150, 1...
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WO/2023/238208A1 |
[Problem] To provide an aerial photography system, an aerial photography method, and an aerial mobile body management device that can facilitate the smooth running of a contest, an event, or other activities. [Solution] An alarm control ...
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WO/2023/236066A1 |
The present invention relates to an unmanned aerial vehicle terrain detection device for aerospace, comprising an unmanned aerial vehicle body, a protection box being arranged on the unmanned aerial vehicle body, a detection instrument b...
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WO/2023/233717A1 |
An unmanned rotorcraft 1 comprises a non-moving landing leg 60 that is fixed to a vehicle body 50. The landing leg 60 includes a ground-contact part 61 that is for making contact with the ground and a frame part 63 that connects the grou...
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WO/2023/234043A1 |
This flight control device performs a flight control process for causing eVTOL to fly. The flight control device determines whether to maintain eVTOL in a stable orientation in steps (S104-S106) of the flight control process. In a step (...
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WO/2023/233608A1 |
The present invention provides a landing assistance device comprising dollies 30 that can move over a port and catchers 31 which are disposed on the dollies 30 and which can engage with an attachment 11 attached to a drone 10. When the d...
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WO/2023/230398A1 |
A method for detection of air flow disruption includes monitoring air flow generated by an air propulsion system to detect one or more air flow anomalies indicating potentially blocked air flow. In response to detecting the one or more a...
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WO/2023/229287A1 |
A method for determining a collision candidate object for an object to be tracked is provided. The method comprises the steps of: acquiring location-related information regarding the object to be tracked at a target point in time; on the...
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WO/2023/220093A1 |
The present disclosure provides doorway protection assemblies with a base portion and two leg portions that can be positioned over and protect the exterior surrounding a doorway of a vehicle, such as an aircraft, from damage while cargo ...
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WO/2023/218138A1 |
The invention relates to a method for detecting an anomaly in a system (110) of an aircraft (100), comprising: - obtaining a current series of measurements of one or more physical quantities (PT1, PT2) of the system (110), during a time ...
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WO/2023/219424A1 |
A method and a device for verifying aircraft status information are disclosed. According to one embodiment of the present disclosure, a method by which a UAM aircraft verifies aircraft status information may comprise the steps of: receiv...
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WO/2023/209612A1 |
A film includes a conductive substrate layer having a conductive trace region, a plurality of nonconductive regions, and a plurality of conductive attachment regions. The film may be applied to a nonconductive support and electrically co...
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WO/2023/209717A1 |
A system for detecting a state of a mechanism includes processing circuitry. The mechanism includes multiple components, at least some of which are capable of moving relative to each other. At least one state is specified for the mechani...
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WO/2023/207169A1 |
A navigation light system, a rotary wing aircraft and a navigation light control system. The navigation light system comprises a left navigation light assembly and a right navigation light assembly, which is opposite the left navigation ...
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WO/2023/204737A1 |
The invention is a device placed in a hidden place and operated remotely by remote control and designed to protect aircraft from hijacking and explosion as well as to protect sensitive facilities such as banks, museums, ships, malls, sch...
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WO/2023/200852A1 |
Principles described herein allow for wings to be optimized for aerodynamic and structural efficiency while reducing planform compromises required to address wing tip stall problems. All-moving outboard wings allow the outboard wing loca...
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WO/2023/196755A1 |
A display system is provided for a vehicle having a windshield (500) and vehicle structure (506) outside the windshield. The vehicle structure (506) is visible within a field of view defined by the windshield (500). Certain embodiments o...
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WO/2023/195571A1 |
A precision navigation device for a UAM route, and an operation method of the precision navigation device are disclosed. According to an embodiment of the present invention, a precision navigation device for a UAM route may comprise: a s...
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WO/2023/191752A1 |
The present invention relates to a body (2) which is an air vehicle; at least one rotor (3) on the body (2), which allows the body (2) to move; at least one wire cutter on the body (2), which cuts various obstacles such as electrical wir...
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WO/2023/189613A1 |
In the present invention, the operations of a drone 10a and a drone 10b are controlled by different subjects, and in a case where an operation control device 20a has not ascertained flight plan information or cargo information of the dro...
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WO/2023/174678A1 |
The present invention provides a visual aid (200) for improving a pilot's awareness of the situation and status of an aircraft, which comprises means for: (202) determining, on the basis of information relating to the current navigation ...
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