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WO/2023/095630A1 |
This flight vehicle comprises a rotor shaft projecting upward from a body, a rotor head connected to the rotor shaft above the body, and a pair of plate units that are disposed above the body and extend in the longitudinal direction on t...
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WO/2023/092164A1 |
A space based solar power system comprising Braggs mirrors.
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WO/2023/089274A1 |
Module for mounting a turbomachine fan blade, comprising: - a blade force absorption device (24), - a blade carrier (22) capable of pivoting around a radial axis (A) and configured to be engaged axially inside the device (24), the carrie...
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WO/2023/087038A1 |
According to the invention, a ground effect vehicle is provided, comprising a first hull (1) and a second hull (2) which are arranged substantially parallel to each other, and a leading wing (4) and a trailing wing (5), the ends of which...
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WO/2023/087602A1 |
A detachable fixed-wing unmanned aerial vehicle (UAV), the UAV comprising: a body, an end plate (20), a first wing (31) and a second wing (32), wherein: one side of the body is connected to the first wing (31), the other side of the body...
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WO/2023/091640A1 |
Adjustable gravity simulators, mechanical loading devices, and methods for simulating gravitational loads and cell culturing are described.
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WO/2023/091113A1 |
The present invention relates to an input element (2) provided in an air vehicle, which provides a force for movement energy; an output element (3) which performs a movement requested by the user using the force applied by the input elem...
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WO/2023/091672A1 |
An aerial device is provided. The aerial device includes a processor and a memory that includes instructions configured to cause the processor to perform certain operations when the processor executes the instructions. The operations may...
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WO/2023/091235A2 |
The present invention is a system and methods for preconditioning a power source of an electric aircraft. The system may include a sensor attached to a power source of an electric aircraft, where the sensor is configured to detect a cond...
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WO/2023/091991A1 |
A system, method and apparatus are proposed to assist in assembling the frame, attaching the skin, and performing other tasks in manufacturing an airship and constructing other structures that are otherwise challenging, inefficient, or u...
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WO/2023/091559A1 |
A lever for adjusting output of a hybrid-electric powerplant of an aircraft includes a lever configured to move over an overall range of positions. Movement of the lever adjusts the output of the hybrid-electric powerplant between at lea...
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WO/2023/090465A1 |
Provided is a drone comprising: a body, which is connected to a plurality of arms and includes propellers provided at each of the plurality of arms; a driving part for supplying propulsive power to the propellers provided at each of the ...
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WO/2023/091132A1 |
Features for in-flight recovery of an unmanned aerial vehicle (UAV). A towline may be deployed by a host aircraft in-flight to recover an in-flight target UAV. The towline or portion thereof may be oriented nearly vertical. The towline m...
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WO/2023/088923A1 |
The present invention relates to a removable separation device (20) for separating off a space, in particular for an aircraft cabin, comprising: - a fixed frame (21), - a movable shutter (23), and - two slide connections (27.1, 27.2) mou...
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WO/2023/088529A1 |
The present invention relates to a mechanism comprising a frame (10), levers (7), pedals (19, 17, 13), clutches (1) and/or freewheels, gears and/or pulleys, rotation shafts (8, 9, 11, 14, 15) and/or lever pushrods (20) which convert the ...
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WO/2023/088915A1 |
The present invention relates to a removable closure device for closing off a space, in particular for an aircraft cabin, comprising: - a frame (25) comprising a housing (26), and - a movable door (27) able to move translationally with r...
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WO/2023/091114A1 |
The present invention relates to a body (2) located at an air vehicle; at least one control stick (3) extending outward from the body (2) and enabling the pilot to control tasks such as position and speed of the air vehicle; at least one...
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WO/2023/091492A1 |
A satellite having a cooling system to remove heat from an electric rocket engine using a working fluid. The cooling system can include a pump that circulates working fluid along a cooling loop between the rocket engine and a radiator. T...
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WO/2023/089273A1 |
The invention relates to an open composite panel (10), comprising: - a composite skin (12) having an inner surface (18) and an outer surface (16), - a plurality of stiffening ribs (14), each rib (14) extending over the inner surface (18)...
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WO/2023/091123A1 |
A novel gas propulsion device comprises one or more high-frequency linear actuators (such as a voice coil linear actuator or a piezoelectric linear actuator) attached to one or more gas propulsion elements having a concave internal surfa...
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WO/2023/089532A1 |
An automated container (1 ) for receiving objects (0), in particular parcels or the like, delivered by means of aerial vehicles (Va), in particular by means of drones (D). Said automated container (1 ) comprises a box-like structure (2) ...
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WO/2023/091583A1 |
An enclosure for an aircraft powerplant includes an air inlet, an air outlet, and at least one sidewall forming the enclosure and fluidly connecting the air inlet and the air outlet. The enclosure further includes a cavity configured to ...
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WO/2023/091600A1 |
A hybrid-electric genset includes a direct current (DC) bus, an engine, and an electric generator configured to receive mechanical power from the engine and generate first alternating current (AC) power. The hybrid-electric genset furthe...
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WO/2023/091481A1 |
A satellite having a longitudinally elongated body and being capable of operating in the thermosphere. The satellite can be powered by an electric rocket engine, and includes a remote sensing system configured to obtain images of Earth. ...
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WO/2023/090209A1 |
The purpose of the present invention is to suppress the occurrence of biases in ground support equipment to be used and to reduce working time when allocating ground support equipment in an airport. An automatic allocation system 10 comp...
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WO/2023/091397A1 |
In an aspect of the present disclosure is a system for in-flight re-routing of an electric aircraft including a battery pack configured to provide electrical power to the electric aircraft; a sensor configured to detect at least a temper...
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WO/2023/091389A1 |
Various implementations include a rotor control device including a shaft extending along a rotational axis, a hub, first and second pitch control components, and a swashplate. The hub has a hub axis and is hingedly coupled to the shaft s...
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WO/2023/091133A1 |
Features for in-flight recovery of an unmanned aerial vehicle (UAV). A towline may be deployed by a host aircraft in-flight to recover an in-flight target UAV. The towline or portion thereof may be oriented nearly vertical. The towline m...
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WO/2023/089735A1 |
[Problem] The present invention provides a flying object with which any decrease in flight efficiency while the flying object is cruising can be minimized while safety is improved. [Solution] This flying object is provided with a safety ...
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WO/2023/091788A1 |
The methods and systems provide for increasing the accuracy of aircraft (1) weight and center of gravity determination through the use of filtered strut pressure measurements. Aircraft (1) vertical and horizontal accelerations are determ...
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WO/2023/087080A1 |
The inventions relate to a method and system for automatically measuring the weight, centre of gravity, pitch, yaw and roll angles and centre of gravity shift of an aircraft on the ground and in flight. For performing automatic measureme...
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WO/2023/082292A1 |
A multi-rotor unmanned aerial vehicle (UAV), comprising: a center body (10); a landing frame (11), which is located below the center body (10); two pairs of arms (12), which are rotatably connected to the center body (10), so as to achie...
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WO/2023/085198A1 |
The present invention provides a blade in which the specific rigidity of a flap part is further increased. This blade has a thick body part and a thin flap part integrally formed in the rear end of the body part. The flap part has a skin...
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WO/2023/086078A1 |
In some examples, a system may receive, from a first user, a request to create a team folder from a folder associated with the first user. The request may indicate a requested storage quota from a team folder storage pool to associate wi...
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WO/2023/083813A1 |
The reversible hydraulic pump (12) for setting the propellor pitch (3) of a turboprop (2) comprises two cylinders (20, 21) connected by a transmission shaft (28). The first and second cylinders (20, 21) are connected to the transmission ...
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WO/2023/086622A1 |
This invention relates to devices that transport cargo. Previously, weight constraints and fuel capacity of an aircraft limited efficiency for transporting cargo. Embodiments of the present invention use at least one unmanned autonomous ...
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WO/2023/084303A1 |
A system (10) for enabling descent control of a payload (50) is provided. The system includes drag generating units (20) coupled to open canopies (30). The open canopies are coupled together by a connector (40) to support a payload. The ...
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WO/2023/084018A1 |
The security inspection system according to the invention consists substantially of • a luggage loading region for loading luggage of a person into at least one load carrier, • a luggage inspection station for an imaging examination ...
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WO/2023/084019A1 |
The invention relates to a security inspection system substantially consisting of • a baggage delivery area (1) having one or more delivery stations (1a, 1b, 1c) for delivering baggage belonging to a person into a load carrier (2), •...
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WO/2023/085027A1 |
This device (300) is installed in a moving object (100) and is purposed for controlling the moving object (100). The device (300) is provided with a holding part (310) and a control unit (302). The holding part (310) holds an information...
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WO/2023/082293A1 |
A centrifugal spray nozzle, a spraying system, and a plant protection unmanned aerial vehicle. The centrifugal spray nozzle comprises a motor (10), a liquid supply assembly (20), a valve core (30), a centrifugal disc assembly (40), a liq...
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WO/2023/083990A1 |
An aerodrome structure comprising a core and a peripheral portion, wherein the peripheral portion is radially outside the core. The core comprises an upstanding structure, a platform located within the upstanding structure and a lift mec...
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WO/2023/084017A1 |
The invention relates to a follow-up inspection region of a security inspection system, comprising at least one follow-up inspection station accessible from two sides for the manual follow-up inspection of luggage objected to in a luggag...
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WO/2023/082000A1 |
There is provided an improved weight-shift control flexible wing aircraft and improved systems and methods for recovering or preventing a spiral dive or a stall of a weight-shift control flexible wing aircraft. The aircraft including a f...
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WO/2023/082254A1 |
An unmanned aerial vehicle (UAV), comprising a body (10), arms (20), power assemblies (30), a first radar (40) and a second radar (50). The body (10) comprises a frame (11) and foot stands (12) that are mounted at the bottom portion of t...
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WO/2023/086757A1 |
In an aspect, a method for monitoring recurrent aircraft faults is disclosed. The method comprises (a) retrieving a plurality of data entries from an aircraft. The plurality of data entries may comprise semantic information about a plura...
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WO/2023/082528A1 |
The present invention provides a thermal protection structure and a preparation method therefor. The thermal protection structure comprises a thermal insulating layer, a cavity layer, and a skin which are sequentially arranged. The therm...
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WO/2023/083642A1 |
The invention relates to a method for producing a stiffened one-piece composite structure comprising a panel (2a) and at least one stiffener which are draped in fibres by resin infusion in an infusion tool (1) that performs shaping of th...
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WO/2023/085338A1 |
Provided are a mechanism and device that can increase the degree of freedom of the placement of the center of rotation of a rotating body relative to a rotation reference. Also provided is a system using the same that suppresses changes ...
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WO/2023/086991A2 |
A novel method has been proposed for implementing artificial gravity in the micro-gravity environment of space habitats (or other space environments). This will allow a number of human activities and services performed in an environment ...
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