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WO/2024/065001A1 |
Slope monitoring systems, prism assemblies and drones are provided, which alleviate the need for personnel to access a slope to be monitored, significantly reducing risk associated with rockfall. The slope monitoring system includes a pl...
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WO/2024/068275A1 |
The invention relates to an assembly with a mechanism (2) for locking a door (1a) in circular translation, the door being of the vehicle semi-plug type. The mechanism (2) comprises a handle (3) actuating a rotation of the door (1a) on it...
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WO/2024/068607A1 |
According to a first aspect of the disclosure, there is provided a firearm mount assembly for a wearable flight system. The firearm mount assembly comprises a firearm mount and an actuator. The firearm mount is configured to rotate about...
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WO/2024/066918A1 |
A fixed-wing aircraft having vertical take-off and landing electric rotors and driven by a fuel power to fly forwards, comprising vertical take-off and landing electric rotor mechanisms (6) embedded in a fixed wing (2) or/and in an empen...
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WO/2024/066601A1 |
A preparation method for an aircraft cargo hold floor, and an aircraft cargo hold floor. The preparation method comprises the following preparation steps: separately preparing phenolic resin upper panel layers (4), phenolic resin lower p...
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WO/2024/069788A1 |
[Problem] To ensure safety during aerial photography. [Solution] A mobile body system 1 comprising a mobile body 100 that flies in a subject area F and a flight mode switching unit 330 for switching flight modes M102 and M105 in which fl...
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WO/2024/067896A1 |
The invention relates to an aircraft, comprising a body, at least four arms and/or supporting surfaces arranged on the body at a respective one end and extending away from the body with a respective free end, vertical and/or lateral rudd...
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WO/2024/073763A1 |
Carbon nanostructure-based composites and methods of making and using thereof are described. The carbon nanostructure-based composites may be single-layered or multi-tiered composites. Such composites can be useful for radiation shieldin...
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WO/2024/073166A2 |
Systems and methods for charging unmanned aerial vehicles (UAVs) using ultra-low frequency wireless power transfer technology are disclosed herein. In some embodiments, a UAV can carry a wireless power transfer (WPT) unit configured to t...
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WO/2024/068395A1 |
The invention relates to a rocket engine (100, 200, 300, 400) comprising a first tank (102) and a second tank (106), wherein the first tank is filled with a fuel and the second tank with an oxidising agent, such as liquid hydrogen peroxi...
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WO/2024/073373A1 |
Rudder pedal input control devices (100, 200, 300, 400A, 400B, 500, 600) are described that utilize a straight-line mechanism and rotary joints to achieve straight line motion in a compact volume. The devices include bar linkages (106, 1...
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WO/2024/069790A1 |
[Problem] To achieve labor efficiency in photography work and to make it possible to perform appropriate photography according to the situation of a photography subject. [Solution] An aerial photography system 1 comprises: a mobile body ...
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WO/2024/068661A1 |
A control unit (6, 7) is indicated for controlling the pitch of an aircraft (1), the control unit (6, 7) comprising at least one adjustable control element (6) and an adjustment mechanism (7) for actively adjusting the at least one contr...
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WO/2024/065917A1 |
A reconfigurable blended wing vertical take-off and landing aircraft, comprising a fuselage, wings, canards, and a cabin door. The wings are respectively arranged on the two sides of the fuselage, two rotor wing modules are respectively ...
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WO/2024/069669A1 |
[Problem] To provide an information processing system or the like capable of extracting only an edge of a near or far object. [Solution] According to one embodiment of the present invention, provided is an information processing system o...
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WO/2024/071521A1 |
The present invention relates to a sensing structure for diagnosing a drone drive system, and a block-type diagnostic device for a drone drive system, including the sensing structure, in which a plurality of diagnostic sensors for measur...
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WO/2024/072361A1 |
The present invention relates to a body (B); at least a first piece (2) located on the body (B); at least a second piece (3) positioned opposite the first piece (2); a plurality of extensions (201) made of a flexible material, located on...
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WO/2024/072596A1 |
A roller-and-rail cargo handling system that includes tracked rollers and side rails for receiving cargo pallets. A trolley system is used to move the pallets along the tracked rollers, which includes a trolley movable along a trolley tr...
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WO/2024/069633A1 |
During aircraft descent, flight control systems seek and maintain a glide slope determined from a single pilot input parameter; e.g., the position of a control axis of a flight stick. Appropriate guide slope selection by the pilot is rea...
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WO/2024/071577A1 |
The present invention relates to a lunar gravity simulation system for testing performance of a lander, characterized by comprising: a plurality of first frames extending in the height direction; a plurality of second frames extending in...
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WO/2024/071410A1 |
Provided is a liquid storage container in which a device is disposed and with which high durability can be achieved.　This liquid storage container includes: a seamless cylindrical container body in which a storage chamber capable of st...
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WO/2024/069210A1 |
The present invention concerns a method of manoeuvring a vertical take-off and landing, unmanned aerial drone (100) comprising at least an aerodynamic surface (101), wherein, during a flight of the drone, the aerodynamic surface generate...
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WO/2024/065886A1 |
A fire-fighting unmanned aerial vehicle cluster (1), comprising a ground platform (200) and N unmanned aerial vehicles (100) arranged at intervals. The ground platform (200) comprises a main water pump. Each unmanned aerial vehicle (100)...
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WO/2024/073696A1 |
A method and apparatus for aerial delivery of a package dropped from an elevated location. The apparatus includes a main body having an internal compartment for receiving a package to be delivered. A controllable component is detachably ...
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WO/2024/069129A1 |
Systems and methods for supplying cooled air in a vehicle, for example an aircraft, are disclosed. The system comprises: an air cycle machine (ACM) configured to compress and cool a flow of air so as to produce a flow of cooled air; an a...
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WO/2024/072350A1 |
A hybrid air vehicle comprising a body (2); at least one motor (3) which provides required power for flight; at least one rotor (4) extending outward from the body (2) connected to the motor (3); a plurality of blades (5) located on the ...
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WO/2024/069080A1 |
The invention relates to a system for transmitting commands to N hydraulic servo-actuators, N being an integer greater than or equal to 2, the system comprising: N mechanical systems, each mechanical system comprising: - a rotary electri...
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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/2024/072559A1 |
An unmanned aerial vehicle (UAV) includes a fuselage, a pair of fixed wings attached to the fuselage, a tail assembly attached to an aft portion of the fuselage and including a pair of stabilizers, a plurality of distributed propulsion u...
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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/2024/073514A1 |
Systems and methods described herein include collapsible and deployable structures that may be used as antenna, collectors, reflectors, or other large structures. The systems and methods may use modular designs so that larger structures ...
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WO/2024/065915A1 |
A device for measuring carbon emissions of a passive house, arranged on a metal rain cap (2) at the top of a chimney (1). The device comprises an unmanned aerial vehicle (5), a guide assembly (3), and two landing support assemblies (6); ...
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WO/2024/069789A1 |
[Problem] To ensure safety in aerial imaging. [Solution] An aerial imaging system 1 comprises a mobile object 100 that flies over a target area F, a camera 141 mounted on the mobile object to capture an image of the target area, an event...
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WO/2024/069215A1 |
using UAV technology can be applied to road crack detection and using image processing techniques, the captured or scanned images of the infrastructure parts can be analyzed to identify any possible defects. Apart from image processing, ...
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WO/2024/072353A1 |
Invention relates to the unmanned aerial vehicle (I) wing deployment element (80) to enable the wings (20) to be deployed, wing deployment shaft (84) to enable the wing deployment element (80) to function and to enable the wings (20) to ...
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WO/2024/068255A1 |
A control system for apparatus to be operated on an aircraft or spacecraft, such as a satellite attitude determination and control system "ADCS", comprises a controller configured to implement one or more real time processes during norma...
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WO/2024/072359A1 |
The present invention relates to a body (2) on an air vehicle; at least one load (W) hitting the body (2); at least one main armor (3) on the body (2), which allows the protection of an area it covers on the body (2) against the impacts ...
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WO/2024/065022A1 |
The invention consists of a wind turbine that produces electrical energy when said turbine is rising through the atmosphere with the aid of a balloon filled with a gas that carries the turbine to high altitude, and that produces electric...
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WO/2024/065943A1 |
A deicing vehicle having a function of one-key return and a method for controlling the return of a boom. The deicing vehicle comprises an electric vehicle chassis (100), a power battery pack (200), a high-altitude operation device (300),...
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WO/2024/068918A1 |
The invention is directed to a site cabin (2) comprising an enclosure (4) comprising a floor (4.1), side walls (4.2, 4.3, 4.4, 4.5) and a roof (4.6), delimiting an inner volume; and anchoring points (4.7) on the side walls (4.2, 4.3, 4.4...
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WO/2024/066433A1 |
The present invention provides an unmanned aerial vehicle remote power switch apparatus having an identity information identification function, comprising a primary controller module, a secondary controller module, a primary Bluetooth mo...
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WO/2024/061159A1 |
A method for rapidly monitoring and determining the drought condition of summer corn on the basis of chlorophyll content by using an unmanned aerial vehicle. The method comprises the following steps: 1) calculating vegetation indexes, i....
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WO/2024/063791A1 |
Described is a fan assembly for an electrical aircraft motor having an axial fan with an inner hub of a first diameter and an outer hub of a second diameter. The outer hub may be concentrically aligned with the inner hub. A plurality of ...
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WO/2024/064626A1 |
The present invention provides methods and systems for remote operation of a vehicle with the capability to deal with communications jitter and intermittency. In particular, the methods and systems herein may safely predict a remote oper...
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WO/2024/060585A1 |
The present invention relates to a wing system integrated with a power battery module. The wing system comprises: a wing box, the wing box comprising a plurality of wing support members, and the plurality of wing support members being co...
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WO/2024/061095A1 |
An adjustment device for an aircraft entering a hangar, comprising sliding rails (10) and a conveying mechanism. The sliding rails (10) are connected to the ground. The conveying mechanism comprises a sliding base (20) and belt-type conv...
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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/2024/062928A1 |
The present technology relates to an unmanned aircraft and a propeller in which it is possible to improve stability in a state in which a foldable unmanned aircraft propeller is opened. This unmanned aircraft comprises a propeller and a ...
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WO/2024/061146A1 |
A measuring device, which is used for measuring an assembly under test. Said assembly comprises an electric motor and a propeller, wherein the propeller is connected to an output end of the electric motor. The measuring device comprises:...
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WO/2024/060313A1 |
Disclosed in the present invention is an SMA-wire-driven reusable release mechanism with a self-resetting function. The present invention uses a two-stage load reduction and one-stage release structure. First-stage load reduction involve...
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