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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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WO/2023/217282A1 |
An ornithopter, comprising a frame (1), a flapping wing mechanism (2), a tail wing (3), a driving mechanism (4) and a transmission mechanism (5), wherein the flapping wing mechanism (2) comprises paired flapping wings symmetrically arran...
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WO/2023/220588A1 |
Disclosed are systems, methods, and media for using a secure dataloading system for updating an aerospace system. The secure dataloading system includes a communications module that is configured to communicatively couple the secure data...
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WO/2023/217713A1 |
The invention relates to a propulsion stage of a launch vehicle comprising a rocket body (2, fig. 2) having a longitudinal axis (Z, fig. 1), wherein the propulsion stage (3, fig.1) is provided with at least one jet propulsion drive (36; ...
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WO/2023/218138A1 |
The invention relates to a method for detecting an anomaly in a system (110) of an aircraft (100), comprising: - obtaining a current series of measurements of one or more physical quantities (PT1, PT2) of the system (110), during a time ...
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WO/2023/217807A1 |
A filling level monitoring device (100) for monitoring a filling level (210) of a fluid in a container (200) includes exciter(s) (10), sensor(s) (20), a signal source (30) connected to the exciter(s) (10), a processor (40), at least one ...
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WO/2023/218674A1 |
This flying body comprises: a communication device; a receiver that acquires a current position; a flight controller that controls flight and is able to transmit current position information by using the communication device; a plurality...
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WO/2023/220155A1 |
Methods, systems and processes to provide energy to power remote and industrial sampling and monitoring stations as well as other ancillary electrically powered pipeline equipment such as hydrogen collection and production units and the ...
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WO/2023/217666A1 |
An inflatable bladder (33, 41) configured to be carried by an aircrew garment (35, 43, 34, 42) worn on the body of the aircrew and to apply pressure to the body when inflated by a gas to counteract effects of high G-forces during flight....
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WO/2023/218282A1 |
Described is an integrated electronic control system including keypad with a keypad connector, one or more galley inserts controllable by the keypad; and a control board couplable with the keypad and the galley insert. The control board ...
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WO/2023/219981A1 |
Various embodiments of the present disclosure provide methods of using a strap for supporting and transporting a package via an aerial vehicle.
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WO/2023/220375A1 |
A technique provides a field service tool (FST) that allows customers to view and store engine performance data, including faults, in a convenient manner. The technique allows customers to gain insights into performance anomalies while p...
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WO/2023/219424A1 |
A method and a device for verifying aircraft status information are disclosed. According to one embodiment of the present disclosure, a method by which a UAM aircraft verifies aircraft status information may comprise the steps of: receiv...
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WO/2023/217918A1 |
The invention relates to a tachometer (10) for an aircraft wheel (R) mounted on an axle (E) so as to rotate about an axis (X) of rotation, the tachometer comprising a stator (20) that is intended to be attached to the axle (E) and a roto...
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WO/2023/212788A1 |
The present patent application to a wing tip thruster rotation system describes a system for rotating wing tip thrusters (EDF or turbofan engines), belonging to the field of aircraft equipment, more precisely for use in aircraft of the c...
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WO/2023/213006A1 |
An overwater life-saving device, comprising a closed cabin body (1), a propeller and a steering mechanism (2) which are located outside the closed cabin body, and, a lifting and lowering mechanism (3), a rotation platform (4), a mechanic...
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WO/2023/214930A2 |
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WO/2023/215326A1 |
The present disclosure provides modular hydrogen-fuel storage assemblies with an external form factor corresponding to Unit Load Device (ULD) cargo containers (100), allowing the assemblies to be easily loaded into and stored in a cargo ...
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WO/2023/214128A1 |
The invention relates to a hybrid electrical architecture (101) for an aircraft (103) which comprises a turbomachine (107) and a reduction gearbox (111) intended to rotate at least one propulsion member (105) of the aircraft (103). The a...
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WO/2023/213373A1 |
The invention relates to "mobile units" which inseparably include: a cylindrical outer casing with low taper or constant cross-section; one or more motorised longitudinal fluid channels which are each "convergent" at the inlet and subseq...
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WO/2023/213598A1 |
The present disclosure relates to a method (50) for generating an image using a satellite (10), wherein partial zones are processed successively and the processing of each partial zone comprises: - receiving (S51) at least two basic part...
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WO/2023/213420A1 |
The invention relates to a, preferably pumpless, pressure fed propulsion system for a spacecraft, preferably a satellite or microsatellite, the system comprising: - a propellant tank (101) for storing a propellant; - a first heat exchang...
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WO/2023/214378A1 |
A first communication device can determine (410) that a second communication device is within an area. The first communication device can determine (420) an identifier of the second communication device. The first communication device ca...
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WO/2023/215664A1 |
Described herein is a power processing unit (PPU) for use with a Hall Effect Thruster (HET) and a Propellant Management Assembly (PMA) of a spacecraft. The PPU comprises an anode and ignitor supply subsystem that provides anode and ignit...
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WO/2023/215632A1 |
An aircraft lift enhancement system is provided. The aircraft lift enhancement system includes an airfoil and at least one rotor. The airfoil includes a leading edge and a trailing edge defining a longitudinal axis of the airfoil, and a ...
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