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WO/2023/233091A1 |
The invention relates to a device (1) for monitoring objects in space orbit around the Earth, the device (1) comprising a frame (2), a plate (3), at least three optical monitoring modules (4), and a power supply and control unit (5) hous...
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WO/2023/234226A1 |
A mobile object 1 according to the present disclosure is provided with a body unit 10 which is formed as a first polyhedron, and a rotary blade module 20 which is positioned at each vertex of the first polyhedron and is mounted to the bo...
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WO/2023/233373A2 |
An aircraft structure for removal of impurities from the atmosphere, especially carbon dioxide, comprises a fuselage, one or more wings extending from the fuselage, and a impurity removal device attached to the fuselage. The impurity rem...
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WO/2023/233717A1 |
An unmanned rotorcraft 1 comprises a non-moving landing leg 60 that is fixed to a vehicle body 50. The landing leg 60 includes a ground-contact part 61 that is for making contact with the ground and a frame part 63 that connects the grou...
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WO/2023/233870A1 |
An estimation unit (12) estimates whether a person is present inside a door on the basis of sound data acquired by an acquisition unit (11). The wording "inside a door" refers to a place where a user takes off his or her shoes in an entr...
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WO/2023/233097A1 |
Propulsion assembly (100) for an aircraft, in particular a multi-engine helicopter, comprising at least a first engine (1) and a second engine (2) that are configured to operate in at least one standby mode, a primary air-circulation dev...
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WO/2023/233150A1 |
A lightbar (100) for mounting to a vehicle (140) is provided. The lightbar (100) comprises one or more warning lights (106), a compartment (126) configured to receive a drone (128), the compartment (126) being located within the lightbar...
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WO/2023/234043A1 |
This flight control device performs a flight control process for causing eVTOL to fly. The flight control device determines whether to maintain eVTOL in a stable orientation in steps (S104-S106) of the flight control process. In a step (...
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WO/2023/233608A1 |
The present invention provides a landing assistance device comprising dollies 30 that can move over a port and catchers 31 which are disposed on the dollies 30 and which can engage with an attachment 11 attached to a drone 10. When the d...
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WO/2023/232648A1 |
A power electronics converter is disclosed. The power electronics converter comprises a converter commutation cell comprising a power circuit and a gate driver circuit, the power circuit comprising at least one power semiconductor switch...
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WO/2023/233092A1 |
The invention relates to a blade comprising: - a blade body (12) having an aerodynamic profile comprising a first fibrous reinforcement obtained by three-dimensional weaving and comprising a first matrix in which the first fibrous reinfo...
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WO/2023/234420A1 |
A computer-implemented method for maintaining a spacecraft near an orbit comprises steps of detecting (3) that a distance from the spacecraft to the orbit is greater than a spacecraft threshold and in response, linearizing (5) dynamics o...
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WO/2023/227587A1 |
The present invention relates to a battery assembly (10), comprising a battery box (100), comprising a housing (100a) including a base plate (102) and a cover (104); at least one battery cell stack mounted inside the housing (100a), wher...
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WO/2023/228921A1 |
[Problem] To provide a safety device that can be easily mounted to a flying object without requiring linking of a link member to the flying object, and a flying object equipped with the safety device. [Solution] A safety device 100 compr...
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WO/2023/225762A1 |
A controlled reactor comprises a reactor core thermally coupled to one or more heat pipes and an active cooling loop. A fluid may be circulated through the active cooling loop. A heat exchanger is thermally coupled to the active cooling ...
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WO/2023/228178A1 |
System and method for initiating a combustion of a rechargeable lithium battery powering an unmanned electronic device. A cell state regulator coupled to battery is configured to alter a state of a selected initiation cell of battery, by...
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WO/2023/228702A1 |
[Problem] There has been a problem of addressing laser leakage onto the ground during power/energy transfer from the space to the ground for use in space solar power systems (SSPS) and the like. Further, a problem of lesser charge carrie...
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WO/2023/230140A1 |
A foldable reflector with tensioned cable spoke system includes a foldable reflector. A central cone extends outward from a center of the foldable reflector. An outer reflector ring is hingedly coupled to the foldable reflector at an out...
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WO/2023/230148A2 |
An apparatus, system, or method for performing work on electrical power lines and/or splices on electrical power lines that may include an unmanned aerial vehicle (UAV), a power line measurement device, a support frame selectively releas...
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WO/2023/229835A1 |
A system includes a power optimized energy source, an energy storage optimized source, and a network that combines a first current from the power optimized energy source and a second current from the energy storage optimized source in or...
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WO/2023/225819A1 |
Embodiments of the present application provide an aircraft. The aircraft is characterized by comprising: a fuselage; main wings, which are fixedly connected to the fuselage, the main wings being used to provide lift to the aircraft; cana...
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WO/2023/229545A1 |
The present invention relates to a vending machine drone delivery system that provides the process of automatically transferring products via drone to vending machines located in public areas, the feature of which is; a smart station (1)...
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WO/2023/229526A1 |
A multi-monocopter system is provided, including a plurality of monocopters operable cooperatively in a cooperative flight mode and operable individually in an individual flight mode. Each monocopter includes: a housing member having dis...
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WO/2023/227847A1 |
The invention relates to a seat unit (100) for a passenger on an aircraft (10), comprising a seat (110) and a shell (150), the seat having a seat portion (130) and a backrest (140) that are movable on a base (120) and that are each actua...
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WO/2023/229702A1 |
A drive mechanism for actuating a control surface of a vehicle that moves through a fluid medium. The mechanism directly translates the rotational motion provided by an input drive to a control surface that is used to direct the vehicle....
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WO/2023/229586A1 |
Embodiments of an active object mounting system secure an object of interest to a surface of a secured-to object using one or more vacuum mounting modules, wherein each vacuum mounting module comprises at least one vacuum pump controllab...
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WO/2023/230398A1 |
A method for detection of air flow disruption includes monitoring air flow generated by an air propulsion system to detect one or more air flow anomalies indicating potentially blocked air flow. In response to detecting the one or more a...
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WO/2023/227850A1 |
Flexible door (10) for accessing a seat unit (100) for an aircraft passenger, in particular for an aeroplane passenger, characterized in that the door comprises a plurality of parallel slats (11) articulated longitudinally with respect t...
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WO/2023/230569A1 |
A landing station can include a package manipulation system, an anchoring system, a climate control system, and/or a convertible storage locker. In some embodiments, a temperature control carrier is used with the landing station. In some...
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WO/2023/225745A1 |
A load detection system detects loads applied to a landing gear assembly during landing. The landing gear assembly includes an axle coupled to a piston rod of a compressible shock strut and a wheel rotatably mounted the axle. A torque li...
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WO/2023/230266A1 |
Embodiments of a payload attachment system secure a payload to a wing or fuselage of the drone (102) (or another type of aircraft) using one or more vacuum mounting modules, wherein each vacuum mounting module comprises at least one vacu...
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WO/2023/229287A1 |
A method for determining a collision candidate object for an object to be tracked is provided. The method comprises the steps of: acquiring location-related information regarding the object to be tracked at a target point in time; on the...
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WO/2023/220790A1 |
Hypergravity system comprising a mechanical shaft connected to at least one central motor designed to rotate the mechanical shaft, at least one connection arm connected to the mechanical shaft, at least one housing chamber, wherein each ...
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WO/2023/224840A1 |
This disclosure relates to improved techniques for electronic noise cancellation in aircraft and other enclosures. In certain embodiments, an electronic noise cancellation device can be installed in an aircraft. In certain embodiments, t...
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WO/2023/224820A1 |
Systems and methods are described herein that utilize a decentralized control panel architecture to monitor or control components or (sub-)systems of an aircraft or other vehicle. A controller can be used to receive information from mult...
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WO/2023/224991A1 |
A dock assembly includes a docking station and a stand or mount coupled to the docking station. The dock assembly may be configured for an unmanned aerial vehicle (UAV). The docking station may include a landing surface configured to int...
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WO/2023/224592A1 |
The present invention relates to an unmanned aerial vehicle system comprising at least one master unmanned aerial vehicle (10), at least one subordinate unmanned aerial vehicle (20), an authorization element (A) configured to generate a ...
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WO/2023/222549A1 |
The invention relates to a de-icing system configured to be mounted on a surface (3A, 3B) of a mechanical part (1) to be de-iced, said system comprising at least: - a piezoelectric actuator (9), - a fastening device (11) configured to fa...
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WO/2023/223119A1 |
A fuselage (2, 2', 2'') for a convertible aircraft (1) is described, comprising a nose (4) and a tail (5) arranged on mutually opposite sides along a first longitudinal axis (Y) of the fuselage (2); a first portion (100) and a second por...
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WO/2023/222560A1 |
A VTOL UAV (1) comprising a chassis (3), a propulsion system (5) mounted on the chassis (3), electronics (12) including a flight control system, and a 3D LIDAR sensor (10) mounted on the chassis. The 3D LIDAR sensor has a laser beam 360Â...
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WO/2023/224018A1 |
Provided is an unmanned aircraft which has uniform lift and the overall airframe dimensions of which can be made small.　This unmanned aircraft is provided with four propeller shafts jutting horizontally along diagonals from the airfram...
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WO/2023/224710A1 |
A UAV package delivery system includes a cabinet for deployment inside a merchant facility. The cabinet is configured for storing and charging UAVs on-site at the merchant facility remote from a command and control of the UAVs. The cabin...
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WO/2023/221310A1 |
Disclosed in the present invention are a wing, and a method for improving the control efficiency of a rudder by means of air blowing. In the technical solution of the present invention, an original symmetrical airfoil rudder is deformed ...
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WO/2023/224090A1 |
Provided is a flying apparatus that can effectively cool components of the flying apparatus.　A flying apparatus 10 comprises an airframe base 14, a power supply section, an arm 11 extending toward the periphery of the airframe base 14,...
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WO/2023/223120A1 |
An aircraft (1) comprising a fuselage (2, 2', 2'') with a nose (4) and a tail (5) arranged on opposite parts to each other along a first longitudinal axis (Y) is described; a pair of half-wings (3) arranged on respective mutually opposit...
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WO/2023/223251A1 |
This invention relates to a security system (1) and method more particularly a security system (1) and method which makes use of a drone (2) placed on a protectable asset. The security system comprises a vehicle (3) such as a cash-in-tra...
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WO/2023/222966A1 |
The invention relates to thermoregulated space equipment (10) which comprises at least one mechanical support structure (1) comprising a first metal portion (2) for interfacing with the equipment, which first metal portion is rigidly con...
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WO/2023/223006A1 |
The present disclosure relates to a joint assembly configured to define a tubular body having a first end, a second end and a passage therebetween. The tubular body is configured for articulation between a first state in which the first ...
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WO/2023/223781A1 |
A movable range calculation unit (12) calculates a movable range of a opening/closing door, which is provided to a destination of a drone (10). Specifically, the movable range calculation unit (12) detects the appearance or the shape of ...
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WO/2023/220093A1 |
The present disclosure provides doorway protection assemblies with a base portion and two leg portions that can be positioned over and protect the exterior surrounding a doorway of a vehicle, such as an aircraft, from damage while cargo ...
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