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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/2024/094378A1 |
A system (10) for real-time remote viewing of a site comprises micro-drone (11) mounted with a camera (12), an observer with an observer's personal computing device (13), a system server (15), and a remote viewer with a remote viewer's p...
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WO/2024/095853A1 |
In the present invention, an air conditioning control unit acquires vehicle internal environment information, vehicle external environment information, and flight information via steps S101-S103 of an air conditioning control process. Th...
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WO/2024/094247A1 |
The present invention relates to a power supply system (1) for a propulsion system (40) of an aircraft (50), comprising a first heat source (11) in the form of a fuel cell unit (21), a second heat source (12) and a heat exchanger (13), t...
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WO/2024/096932A1 |
The present disclosure is directed to composite focal plane array (CFPA) imaging systems, aerial vehicles comprising the same, methods for forming composite images using a CFPA imaging system, and techniques for calibrating such imaging ...
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WO/2024/096512A1 |
The present disclosure relates to a 5G or 6G communication system for supporting higher data transmission rates.The present disclosure relates to a 5G or 6G communication system for supporting higher data transmission rates. A method, ac...
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WO/2024/095873A1 |
Provided is a spacecraft apparatus that enables total electrification in a substantial sense.　This spacecraft apparatus is characterized in that it is possible to offset or reduce at least one location with respect to a reaction force ...
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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/2024/095266A1 |
The present subject matter provides an electromagnetic propulsion system comprising: at least one electromagnetic thrustor configured to intake air, ionize the air to produce ionized air, pass the ionized air through at least one electro...
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WO/2024/097180A1 |
In an example embodiment, a method may be carried out by an uncrewed aerial vehicle (UAV). The method may involve establishing a wireless local area network (WLAN) network connection with one or more other UAVs via a WLAN communications ...
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WO/2024/094623A1 |
A garment adjustment system is disclosed for adjusting the fit of a garment to a wearer, the system including a lacing arrangement (38) for attachment to the garment and a reel assembly (60), the reel assembly and the lacing arrangement ...
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WO/2024/096387A1 |
The present invention relates to cooperative navigation of multiple drones using GNSS error sharing and a method for operating a navigation device. The cooperative navigation of multiple drones including a first drone and a second drone ...
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WO/2024/095029A1 |
The present invention relates a holder (10) for fixing one or more channels to a panel, the holder (10) comprising a fixing interface to the panel with double-sided adhesive tape and at least one clip (161, 162), and a fastening part (26...
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WO/2024/096876A1 |
A satellite rescue system (SRS) (1) for rescue and recertification of dormant satellites, said SRS having a thruster end (13) with a primary propulsion nozzle (11) and maneuvering thrusters (12) and a satellite connection end (8) with a ...
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WO/2024/093476A1 |
The present invention provides a coaxial dual-rotor unmanned aerial vehicle, comprising a main shaft, an upper rotor assembly, a lower rotor assembly, an upper motor, a lower motor, and a rotor control device. The upper rotor assembly is...
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WO/2024/097197A1 |
A UAV having a fuselage body including a cavity that forms a cargo bay for transporting a payload, and a lower access opening providing an exit for the payload from the cargo bay, the lower access opening including a lower cargo bay door...
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WO/2024/094949A1 |
Aeronautical thruster (40) having a longitudinal axis (X) and comprising an upstream rotor row and a downstream stator row (16) having unducted blades (18). Two adjacent blades of the downstream stator row (16) have between them, about t...
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WO/2024/097888A1 |
Embodiments provide an animated graphical user interface for simultaneously monitoring multiple autonomous aircraft. More specifically, techniques disclosed herein provide a GUI that allows for one-to-many supervision where a remote supe...
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WO/2024/096826A1 |
The present invention provides the development of a mechanism in parachute jump training simulators, in which the height value in the entangled rope release simulator is sensitive, is not affected by oscillatory movements, and ensures st...
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WO/2024/094352A1 |
Disclosed is an aircraft power system (800) comprising a hydraulic reservoir (801, 803), a bidirectional hydraulic pump (212) for pumping hydraulic fluid to and from the reservoir, and an electric motor (230), wherein the hydraulic pump ...
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WO/2024/094590A1 |
The invention relates to a grey water tank (20) for vehicles, said grey water tank comprising: a tank housing (24) having an interior for holding grey water; a filter wall (22) inside the tank housing (24), an inner tank chamber (25) bei...
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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/2024/097480A1 |
A backlit button assembly is provided for aircraft, ship, train, or bus seats. The backlit button assembly may provide changing colors, flashing, or similar features to reflect status information associated with the seat, the vehicle, or...
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WO/2024/097669A1 |
A noise-reducing propeller with three-dimensional (3D) serrations and a cicada wing planform alters the propeller airflow characteristics and improves both aeroacoustic and aerodynamic performance. The propeller configuration increases p...
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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/2024/094948A1 |
Aeronautical thruster (40) having a longitudinal axis (X) and comprising an upstream rotor row and a downstream stator row (16) having unducted blades (18). Two adjacent blades of the downstream stator row (16) have between them, about t...
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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/2024/095204A1 |
A computerized method for disrupting a time division multiplex communication between a target remotely-controlled aerial vehicle related communication unit (RCU) and another RCU. The method may include determining a timing of a transmiss...
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WO/2024/072479A3 |
Radiation shielding technologies for radioisotope battery-powered vehicles to protect computer systems and humans and increase the energy efficiency, mass efficiency, and duration capability of the vehicle during operation. A radioisotop...
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WO/2024/093087A1 |
An adapting device (10) for assisting in orbital transfer, and an orbital transfer method. The adapting device (10) comprises a target module (2), a docking module (3), and a connection module (4) that are provided on a substrate (1). Th...
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WO/2024/094351A1 |
Disclosed is an aircraft power system 800 comprising a first driveable component 120, 130 of the aircraft, and a mechanical flywheel 250, wherein the mechanical flywheel is connectable to the first driveable component such that the mecha...
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WO/2024/096691A1 |
Provided are a method and device for estimating the GPS coordinates of multiple target objects and tracking the target objects on the basis of camera image information from an unmanned aerial vehicle according to an embodiment. The devic...
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WO/2024/095581A1 |
Propulsion　systems,　methods　and　aircraft　relatedã€
€to　boundary　layer　ingestion　are　described.　Inã€
€some　embodiments,　an　aircraft　may　include　a　f
uselage　with　a　plurality　of　boundary　layer...
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WO/2024/096879A1 |
A gas turbine engine including a turbomachine. The turbomachine including a compressor section, a combustion section, and a turbine section arranged in serial flow order. The turbomachine including an inlet duct defining an engine inlet,...
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WO/2024/073438A3 |
A satellite includes a bus and a payload disposed relative to the bus. The payload includes a remote sensing system with a telescope that defines a line of sight. The bus is configured such that, in a cross-sectional plane that extends a...
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WO/2024/093481A1 |
A variable-rotating-speed rotor blade, a coaxial unmanned helicopter, and a single-rotor unmanned helicopter. The variable-rotating-speed rotor blade comprises: a blade root (10), a blade middle section (20), and a blade tip (30) which a...
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WO/2024/094565A1 |
A space station includes a housing that defines an interior space. An inner chamber is located in the interior space and defines an inner cavity that is sealable from the remainder of the interior space. At least one bulkhead is arranged...
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WO/2024/097873A1 |
A selectively engageable and interlocking cupholder assembly, comprising a bottom member defining a lower surface and a generally circular container receiver opposite the lower surface; comprising one or more teeth arranged around said r...
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WO/2024/091311A2 |
A modular drone containment system including a plurality of modular stacked drone containers. Each modular drone container is configured to house a drone device and be removably disposed in a stacked orientation relative to one another. ...
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WO/2024/091313A2 |
A computer-implemented system and method for operating one or more uncrewed vehicles (UxSs) in autonomous navigation modes. A software module is provided and executed for operation in a portable user computer device for enabling control ...
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WO/2024/088114A1 |
A power plant with variable thrust direction, the power plant comprising a fan (10), a housing (20) and an adjusting mechanism (30). The housing (20) is internally provided with an air intake duct (23), a first air output duct (21) and a...
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WO/2024/088901A1 |
A system (1) for an aircraft (2, 2') comprises: an electric machine (10) which defines an axis of rotation (D), and an even number of elements (11) which each have a housing (110) and are arranged in pairs on opposite sides of the axis o...
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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/2024/087990A1 |
An aircraft and a control surface hinge structure thereof. The hinge structure comprises a stabilizer hinge (1) and a movable-surface hinge (2), which are arranged opposite each other, wherein the stabilizer hinge (1) comprises a stabili...
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WO/2024/086932A1 |
A landing gear assembly for a vehicle, such as a helicopter, includes a linkage coupled to the vehicle and configured to reciprocate between a stowed position and a deployed position. A shock strut forms a part of the linkage. The landin...
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WO/2024/091312A2 |
An uncrewed aerial vehicle (UAV) configured and operable for controllable flight, including autonomous flight. A generally planar body defining opposing front and back planar surfaces includes a plurality of circular duct openings provid...
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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/2024/090689A1 |
The present embodiments propose an online shooting system comprising: at least one online shooting machine for performing shooting by a shooter; a content server for operating in conjunction with each of at least one shooting machine and...
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WO/2024/089959A1 |
A display system according to the present invention obtains data indicating an orbit of an artificial satellite and time-series data related to the artificial satellite. The display system performs 3D graphics display of the orbit of the...
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