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WO/2024/016045A1 |
Disclosed herein is a method for remote monitoring, comprising determining, from event signals obtained from an event-based vision sensor, a rate of those event signals generated in response to changes associated with a specific object a...
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WO/2024/019837A1 |
An object support includes a support structure that is connectable to a vehicle. The support structure has a top surface and a channel defined in the top surface. The channel extends curvilinearly at least partially around a central port...
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WO/2024/017810A1 |
The invention relates to a method for automated alignment of a stationary part (1) with a movable part (2) capable of being moved towards the stationary part by a robot (3), the stationary part (1) and the movable part (2) each comprisin...
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WO/2023/229790A9 |
In an aspect this disclosure is directed at a propulsor assembly powered by a dual motor system. The aircraft may comprise a propulsors. The electric aircraft may also include a driveshaft that is mechanically coupled to the propulsor, w...
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WO/2024/020013A1 |
A seat bottom assembly, movable between stowed and deployed configurations, includes a seat pan plate having a front side, a rear side, a left side, a right side, a top surface, and a bottom surface. The seat pan plate is configured to m...
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WO/2024/020423A1 |
A hydrogen boiloff capture system. The hydrogen boiloff capture system having a cryogenic tank for storing liquid hydrogen. The hydrogen boiloff capture system also includes an intermediate tank fluidically coupled with the cryogenic tan...
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WO/2024/013460A1 |
A reusable orbital vehicle (14) for a space transport system (10) comprises a fuselage (22) the shape of which widens in a direction extending from the front end (24) of the reusable orbital vehicle to a rear end (26) of said fuselage (2...
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WO/2024/013462A1 |
The present invention relates to a method and system for managing the drawing of mechanical power from a two-spool or three-spool turbine engine (1) for an aircraft, in which at least two electric machines (3, 4) are suitable for recover...
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WO/2024/013223A1 |
The invention is based on an aircraft seat control unit for an aircraft seat (10), having a function circuit unit (14) that has at least one function circuit (16, 18, 20, 22) for controlling the aircraft seat (10), and having a communica...
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WO/2024/015397A1 |
Embodiments of a recovery and deployment pylon (2000) for recovering and launching/relaunching a target aircraft (T) that can include a housing configured to be coupled with an aircraft, a motorized winch, a towline (102) coupled with th...
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WO/2024/015756A1 |
An unmanned aerial vehicle (UAV) including a fuselage body having a cavity that forms a cargo bay for transporting a payload, and a lower access opening for lowering the payload from the cargo bay, the lower access opening including a ca...
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WO/2024/015975A2 |
Methods and systems are provided to enable a virtual FlatSat and distributed node architecture. The virtual platform may be or include a SaaS platform that enables multiple users to access computing nodes. The computing nodes may enable ...
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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/2024/012587A1 |
The present invention provides a device allowing for connecting, combining, and fixing, in particular an apparatus allowing for aerial connecting, combining, and fixing, and a method therefor and an application thereof. The device or app...
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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/2024/014459A1 |
Provided are a flying mobile body, a flight position estimation method, a computer program, and a flight position estimation system that make it possible to estimate a flight position of the flying mobile body with higher accuracy. The f...
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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/2024/015746A2 |
Systems for transmitting power to and from flight vehicles, and associated devices and methods are described herein. A representative flight power-transmission system includes a surface-based transmitter on or adjacent to the surface of ...
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WO/2024/015732A1 |
An unmanned aerial vehicle (UAV) including a fuselage body having a cavity that forms a cargo bay for transporting a payload; an access opening positioned in the cargo bay adapted to receive the payload; a. winch system positioned in an ...
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WO/2024/012942A1 |
The present invention relates to an adjustable guide bushing (10) comprising a first bushing (20) with a first eccentric opening (30) and a second bushing (40) with a second eccentric opening (50), wherein the first bushing (20) is accom...
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WO/2024/015807A1 |
Systems and methods for a vehicle containing a structural column are disclosed. The vehicle includes: a structural column (102) positioned between a first and second interior surface (116,118) of the vehicle. The vehicle may further incl...
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WO/2024/015961A1 |
A unmanned aerial vehicle (UAV) includes a fuselage body including a cavity that forms a cargo bay for transporting a payload, an upper access opening for receiving the payload into the cargo bay from a first direction, and a lower acces...
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WO/2024/015232A1 |
Implementations of the disclosed subject matter provides a system having an artificial light source disposed at a distance from earth or other celestial body, where the artificial light source is configured to project one or more beams o...
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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/2024/014613A1 |
An unmanned aerial vehicle control duplex system and method using a mobile communication network and RF communication are provided. An unmanned mobility system according to an embodiment of the present invention comprises: a ground contr...
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WO/2024/014644A1 |
Provided are a steering system and a method for simultaneous control of an unmanned aerial vehicle and a gimbal device. An unmanned moving system according to an embodiment of the present invention comprises: a ground control system that...
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WO/2024/014614A1 |
An image acquisition/pre-processing/transmission system and method based on an unmanned aerial vehicle are provided. An unmanned mobility system according to an embodiment of the present invention comprises: a ground control system for t...
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WO/2024/013698A1 |
A stage of a rocket is disclosed. The rocket stage may include: a body, and a plurality of foldable propulsion units spaced around a circumference of the body, where each propulsion unit comprises: a folding beam; at least one motor moun...
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WO/2024/012000A1 |
A linear multi-rotor plant protection unmanned aerial vehicle structure based on tilt rotors and a control method therefor. The structure comprises main lifting power structures, tilt power structures and a main rack structure, wherein t...
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WO/2024/015326A1 |
The current disclosure provides systems and methods of directly measuring angular velocity and angular acceleration of space objects and using the measured angular velocity and angular acceleration as inputs into new and unique algorithm...
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WO/2024/014135A1 |
[Problem] To rapidly return an aerial vehicle to normal after a sudden change in position thereof due to a disturbance. [Solution] This position control device is provided to an aerial vehicle 30 that produces thrust corresponding to a c...
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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/2024/015482A1 |
A vehicle (600, 700) is disclosed. The vehicle (600, 700) includes a body forming a door opening. The vehicle (600, 700) also includes a first hinge (607, 707) coupled to the body. The vehicle (600, 700) further includes a door (608, 708...
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WO/2024/011267A1 |
The invention relates to an aircraft (1) and to a method for controlling the aircraft (1), wherein: the aircraft (1) comprises a wing assembly (2); the wing assembly (2) is designed such that the wing assembly (2) generates lift (4) of t...
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WO/2024/013496A1 |
The present invention is concerned with an aircraft comprising an elongate fuselage for containing cargo or passengers. The fuselage comprises a lower floor and an upper ceiling and opposing fuselage sides extending between the ceiling a...
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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/2024/015450A2 |
A self-contained identification tag arranged to be attachable to a resident space object (RSO) comprising: a processor; an antenna, an energy gatherer arranged to gather energy from the environment; and an energy store arranged to receiv...
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WO/2024/013527A1 |
The invention is a seating unit comprising - a seat element (102), - a thigh rest element (104) adapted to be fixed in a plurality of rotated positions relative to the seat element (102), and - a lower-leg rest element (106) rotatably at...
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WO/2024/015401A1 |
A method includes causing an aerial vehicle to deploy a tethered component to a particular distance beneath the aerial vehicle by releasing a tether connecting the tethered component to the aerial vehicle. The method also includes obtain...
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WO/2024/013392A1 |
The invention relates to a vertical take-off aircraft (1) which is designed as a tail-sitter and, after the take-off, transitions in full from the substantially vertical hover attitude into the horizontal attitude, comprising: an aircraf...
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WO/2024/013570A1 |
There is described a spacecraft docking system (D) for and method of capturing and coupling a target spacecraft (T) to a servicing spacecraft (S) provided with the spacecraft docking system (D), the target spacecraft (T) having a propuls...
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WO/2024/013476A1 |
An aerial vehicle capture device (10) for capturing a target aerial vehicle (30) is provided. The capture device (10) includes a capture mechanism having at least one restraining arm (RA1-8). The at least one restraining arm (RA1-8) is d...
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WO/2024/014460A1 |
There is provided a technique for achieving inter-satellite optical communication for a satellite having a limited calculation capability. One aspect of the present disclosure relates to an earth station, including: a data acquisition un...
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WO/2024/015588A1 |
A laminate material for an aircraft component is provided. The laminate material includes a first layer, a second layer and a rib disposed between the first and second layer. One or more connectors are configured to couple the ends of th...
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WO/2024/014615A1 |
An image file/transmission validity verification system and method based on an unmanned aerial vehicle are provided. An unmanned mobility system according to an embodiment of the present invention comprises: a ground control system for t...
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WO/2024/015207A1 |
An unmanned aerial vehicle (UAV) includes a fuselage, a pair of wings attached to the fuselage, and a propulsion system mounted to the wings to provide propulsion to the UAV. The fuselage has an outer fuselage shell that is a first mecha...
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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/2024/014645A1 |
Provided are a mobile communication network-based system and method for radio controlling an unmanned aerial vehicle. An unmanned mobile system according to an embodiment of the present invention comprises: a ground control system that t...
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WO/2024/008982A1 |
The invention relates to a medium-high speed seaplane that uses a system that allows it to travel on land, on water and in the air. The seaplane is formed by one or more parallel hulls or half hulls (1) comprising on the underside thereo...
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WO/2024/009044A1 |
The invention relates to a hydraulic control circuit (17) of a steering actuator (21) having a first and a second chamber (18, 19), for orienting the blades of an aircraft engine propeller, this circuit (17) comprising a high-pressure li...
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