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WO/2024/074680A1 |
The present invention relates to a recognition device (10) for recognizing empty trays (LW) in a conveying device (100) for trays (W) for transporting objects (O), comprising: an inspection light source (20) for generating inspection lig...
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WO/2024/076396A2 |
A method includes determining, by an unmanned aerial vehicle (UAV), a position of an autoloader device for the UAV; based on the determined position of the autoloader device, causing the UAV to follow a descent trajectory in which the UA...
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WO/2024/076447A1 |
An air hose includes a first component, a second, elastic component and one or more fastening positions and/or a continuous fastener. The first component has a first end and a second end, wherein the first and second ends of the first co...
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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/2024/071521A1 |
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/2024/068255A1 |
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/2024/065943A1 |
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/2024/061095A1 |
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/2024/061146A1 |
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/2024/061096A1 |
Provided are an automatic cargo loading and unloading system, and a hangar comprising the automatic cargo loading and unloading system. The automatic cargo loading and unloading system comprises a cargo box (10), a first cargo conveying ...
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WO/2024/061089A1 |
An aircraft towing apparatus, comprising a frame body (10), a driving mechanism and a connecting mechanism. The driving mechanism comprises first driving wheels (20) and second driving wheels (30) respectively rotatably connected to two ...
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WO/2024/061148A1 |
A test frame for the strength of wings under static loads, comprising: a test frame body (100); a plurality of fixed-pulley blocks (200), the fixed-pulley blocks (200) being spaced apart on the test frame body (100); a plurality of weigh...
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WO/2024/056971A1 |
The present application relates to a method for calibrating a model for estimating a torque supplied by an electric machine (10), which comprises the following steps: (E1) measuring an electric current in the electric machine (10) for an...
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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...
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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/2024/047632A1 |
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/2024/047312A1 |
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/2024/050065A1 |
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/2024/042029A1 |
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/2024/043164A1 |
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/2024/041584A1 |
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/2024/043207A1 |
Provided are an aircraft coating removal device and method. The device comprises: a travel cart that can move; a blast head that is mounted on the travel cart and that can spray a blast material; a raising/lowering device that can move t...
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WO/2024/044220A1 |
Embodiments are directed, to low-profile, low-weight cargo loader, including a pair of cargo loaders including a first cargo loader arranged in tandem with a second cargo loader in a first orientation..According to an embodiment, each of...
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WO/2024/043093A1 |
This prediction device (20) predicts the required performance and/or state of a battery, which is a driving apparatus installed in an eVTOL. The prediction device (20) comprises: an acquisition unit (21) that acquires information includi...
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WO/2024/041934A1 |
The invention relates to a device (1) for cleaning fuel in a tank (92) of an aircraft (90), and use thereof. The device has a predetermined flow direction (2) for the fuel and comprises units arranged in a fluid-connected manner to forwa...
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WO/2024/038249A1 |
A flow body unit (600) for a fluid flow rig (10) for simulating fluid flow patterns; the flow body unit (600) comprising: a flow body support frame (700); a core member (800) extending from the flow body support frame (700) along a flow ...
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WO/2024/038634A1 |
Provided is a flight method that makes it possible to prevent a collision of a drone and entanglement of a power supply cable. This flight control system relating to flight control of an electrically driven drone 3 that is connected to a...
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WO/2024/038489A1 |
[Problem] The ability to acquire information useful for the flight of an aircraft is demanded. [Solution] In the present invention, terminal devices 600 provided in the cabin space of a target aircraft 810 each comprises a sensor unit 68...
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WO/2024/038696A1 |
Provided are a device and a method for attaching an aircraft engine comprising: a linear movement device that supports a support frame, by which an aircraft engine is supported along the horizontal direction, so as to be movable along a ...
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WO/2024/033468A1 |
A computerized system of controlling a bag-drop process via a mobile device is provided. The system is arranged to create a virtual zone in front of a bag-drop station using signal emitter(s) located at the bag-drop station. Signals emit...
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WO/2024/035019A1 |
The present invention relates to a low-impact landing system for a rotary wing aircraft for reducing landing impact transmitted to an airframe (11) upon landing of a rotary wing aircraft (10), comprising: a landing platform (110) having ...
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WO/2024/021319A1 |
A turntable type lifting airport device for a relative motion air kinetic energy aviation aircraft. A plurality of relative motion air kinetic energy reversal thrust generating devices (3) are provided on the periphery of a lower portion...
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WO/2024/022821A1 |
The present invention relates to a clamping device (6) for fitting a sheet (2) of a flexible material, wherein the clamping device comprises a sealing-strip rail (3) and a sealing-strip body (1), wherein the sealing-strip rail has a guid...
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WO/2024/025163A1 |
The present invention relates to a drone station having a function of guiding a drone to a correct position, the drone station comprising: a take-off/landing pad where a drone takes off and lands; and a plurality of landing skid movement...
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WO/2024/018491A1 |
Device (10) to secure a vehicle (110) to a platform (90) with a grid (91) provided with a plurality of through holes (92), said device (10) comprising hooking means (12) configured to selectively hooking to said grid (91) and moving mean...
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WO/2024/016767A1 |
A nest for an unmanned aerial vehicle. The nest is suitable for being arranged on a vehicle, and comprises: a nest body (100), which is used for accommodating an unmanned aerial vehicle; a charging device (200), which is arranged in the ...
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WO/2024/019640A1 |
The invention relates to takeoff and landing platforms for tethered unmanned aerial vehicles. The claimed aeroplatform is configured in the form of a container and comprises a takeoff and landing platform equipped with a cable reel, a te...
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WO/2024/018623A1 |
The present invention provides airport ground assistance equipment capable of calculating an error of an actual stop position with respect to a normal stop position of an aircraft without requiring input of aircraft model information. An...
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WO/2024/016807A1 |
An unmanned aerial vehicle rack, a hangar and a vehicle. The unmanned aerial vehicle rack comprises: a mounting body and an electrical connection line. The mounting body is used for mounting an unmanned aerial vehicle, and the mounting b...
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WO/2024/014086A1 |
The present invention provides a payload management apparatus that calculates a weight that can safely be loaded on an aircraft of the rotary wing type, suppresses a decrease in transport efficiency, and increases flight safety of the ai...
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WO/2024/015584A1 |
An energy management system (EMS) for an aircraft is provided. The aircraft may have one of a plurality of propulsion systems such as a parallel hybrid electric propulsion system, a parallel turbo electric propulsion system, an electric ...
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WO/2024/013413A1 |
The present invention relates to an unmanned aerial system for autonomously delivering and collecting products that is intended to optimise last-mile deliveries of goods and products to the final recipients and, furthermore, to drastical...
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WO/2024/015487A1 |
An airfield lighting system includes an approach lighting subsystem and a runway lighting subsystem. A power supply/controller is configured to provide electrical power to the approach lighting subsystem and the runway lighting subsystem...
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WO/2024/015421A1 |
A mobile hydrogen fueling system that is configured to provide hydrogen fuel to a hydrogen storage tank of an aircraft includes a mobile hydrogen storage tank, a robotic arm connected to the mobile hydrogen storage tank having a nozzle c...
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WO/2024/009166A1 |
Electronic system for managing emergencies and contingencies occurring in flight infrastructures, characterized in that it comprises the following elements: - a VHF radio (10); - a VHF antenna (20); - two computers (30); - a microprocess...
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WO/2024/008750A1 |
An aerodrome structure comprises a vertical airfield module having a primary landing pad for a vertical takeoff and landing aircraft. The primary landing pad is located in an upper plane and comprises an inner platform having an inner pl...
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WO/2024/000748A1 |
The present invention provides a lightweight modular general storage platform for an unmanned aerial vehicle, comprising a landing platform, a rotating platform, and a servo control unit. The landing platform is rotatably connected to th...
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WO/2024/003005A1 |
The invention relates to a ground power unit (10) for supplying an aircraft (20) with power via a first power supply output (140), which ground power unit comprises an electrical connection (135) connecting the output of a DC-to-AC conve...
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