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WO/2024/097203A2 |
A payload receiver apparatus including a base configured to receive a payload, suspended from an uncrewed aerial vehicle (UAV), an extending member having an upper end positioned above the base, a first tether engager that extends in a f...
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WO/2024/096860A1 |
Disclosed herein are parts of an electrical connector that are suitable for direct earth burial, submergence in water, and capable of withstanding limited exposure to chemicals typically present on an airfield, including but not limited ...
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WO/2024/093500A1 |
A full-vector survey cluster system and an operation control method therefor. The full-vector survey cluster system (8) comprises a plurality of robots. The plurality of robots comprise a survey robot (200) and at least one cable-bearing...
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WO/2024/094435A1 |
A land vehicle (12) for launching a drone (14) with a span greater than 2 metres equipped with one or more turbojets or turboprops (16) is provided with a system for catapulting (26) the drone (14), comprising a launch ramp (28) and a mo...
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WO/2023/057377A9 |
The present invention relates to a method for manufacturing a connection part (10) between a wing box (20) and a leading edge module (30). The method comprises the steps of carrying out a three-dimensional digitization of a first part re...
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WO/2024/094186A1 |
An airplane cabin door protection apparatus, comprising a deployment mechanism, a return mechanism, and a detection element. The deployment mechanism comprises a deployment portion (10) and a power conversion portion, one end of the depl...
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WO/2024/088977A1 |
There is provided a system for determining a route for an item and/or a passenger, the system comprising a processor. The processor is configured to: determine whether the item and/or passenger has missed or is expected to miss a first p...
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WO/2024/088976A1 |
There is provided a system for notifying a delayed arrival of an item at a destination, wherein, according to an original schedule, the item and a passenger associated with the item are scheduled travel from an origin and arrive at a des...
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WO/2024/092018A1 |
A computer-implemented method includes receiving design and/or engineering data (D/E data) corresponding to a prototype representation of a product and transmitting one or more inputs derived from the D/E data to one or more digital engi...
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WO/2024/088974A1 |
An item handling system for moving an item between an origin and a destination according to a first scheduled route which departs the origin at a first predetermined departure time is provided. The item handling system comprises processi...
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WO/2024/089998A1 |
Provided are a flight route generation device and a flight route generation method which are for generating, with respect to various flight bodies, a safe flight route by suitably considering the weather resistance of the flight body. ...
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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/2024/082667A1 |
The present invention relates to the field of airport towbarless tractors. Disclosed is a green intelligent comprehensive-energy-supply towbarless tractor, comprising a chassis unit, which comprises a vehicle control unit, a power supply...
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WO/2024/083722A1 |
An aircraft engine seal apparatus has an inflatable seal with a front wall (3, 803, 1103) a rear wall (9, 840) and a side wall (4, 804) forming a rim for pressing and sealing against an internal surface of an engine intake. There is at l...
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WO/2024/084781A1 |
At the destination of a drone (10), a detection unit (12) detects a landing-possible area and a landing-impossible area for the drone (10). A safety level specifying unit (13) specifies one of a plurality of safety levels at the time of ...
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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/2024/077365A1 |
The present patent application relates to a support ladder (E) for a boarding region or landing structure (A1) of an aircraft (A), such as a helicopter. The ladder (E) comprises an attachment region (1) for attaching a ladder structure (...
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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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