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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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WO/2023/218116A1 |
The present invention relates to a seat/chair structure (E) for a collective transport vehicle, wherein a longitudinal direction (L), a transverse direction (T) and a height direction (H) are defined, comprising a first chair (R1) orient...
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WO/2023/218164A1 |
There is provided a control surface arrangement for influencing fluid flow about a vehicle, the control surface arrangement comprising: a first control surface portion; a second control surface portion, the second control surface provide...
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WO/2023/220311A1 |
An ejector system is constructed of a soft yet strong material such as silicone-based material which can be pressed to conform within a small space and stowed when inactive and can be expanded or stretched by mechanical, pneumatic or hyd...
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WO/2023/219532A1 |
The present invention relates to aircraft having two rotors on a single shaft, which are disposed inside a housing, one of which is a rotor with rotor blades, and the other of which is a counter-rotating rotor, the rotors being configure...
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WO/2023/220313A1 |
One variation of a system for generating thrust at an aerial vehicle includes: a primary electric motor; a rotor coupled to the motor; an internal-combustion engine; a disengagement mechanism interposed between the motor and an output sh...
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WO/2023/217524A1 |
The invention relates to a construction work drone (10) for performing construction work on a construction site object. Said drone comprises: a flight platform (12); an end effector (18) which is mounted and/or formed on the flight platf...
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WO/2023/218595A1 |
A control device 20 comprises: a processing unit 21 that identifies the incoming direction of radiation using a detector 10 that uses a scintillator; and a control unit 22 that controls a solenoid coil so that the magnetic field null poi...
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WO/2023/219710A1 |
A flow deflector for an aerial vehicle system has a flow deflector body, a clip arranged in an interior of the flow deflector body, and a spring within the clip. The flow deflector body includes a first portion at a forward end shaped to...
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WO/2023/220356A1 |
A computer-implemented method of controlling autonomous movement of a mobile object (110) in an aircraft operating area (104) is provided. An autonomous control computing system receives an image (102) from a digital camera (604) positio...
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WO/2023/216120A1 |
A dual-frequency antenna (100), a remote controller (200), and an unmanned aerial vehicle system (300). The dual-frequency antenna (100) comprises a substrate (10), a first radiation branch (20), a second radiation branch (30), and a thi...
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WO/2023/217714A1 |
The invention relates to a propulsion stage of a launch vehicle, in particular a reusable propulsion stage, comprising a rocket body (2) having longitudinal axis (Z), wherein the propulsion stage (3) is provided with at least one jet pro...
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WO/2023/220209A1 |
An unmanned helicopter system and method for delivering a blood product to a target includes a body, a plurality of spinning rotors, each rotor comprising at least one propeller, and a cord coupled to a container configured to contain a ...
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WO/2023/219837A1 |
Technology is disclosed herein for a power control and distribution unit, PCDU, (206) of a spacecraft that has a microcontroller (208) to control battery charging from solar arrays (104). Using a microcontroller (208) within the PCDU (20...
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WO/2023/218207A1 |
An unmanned aerial vehicle having: a first rotor system including at least first and second rotor blades connected to a first rotor hub, the first rotor hub being supported for rotation about a first axis such that rotation of the first ...
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