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WO/2023/094242A1 |
The invention relates to a seat, in particular for an aircraft, comprising: - at least one seat-portion structure (22); and - an understructure (11) comprising at least one guide element (39) comprising a guide groove (43); - the guide g...
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WO/2023/094587A1 |
The present invention is related to a remotely-controlled flying device intended to approach and contact a high-voltage overhead power line for operation thereon, said flying device comprising : - a mechanical structure (1) bearing a plu...
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WO/2023/094590A1 |
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 me...
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WO/2023/096534A1 |
The group of inventions relates to means and methods for moving space objects between orbits, primarily for clearing near-Earth space of space debris. The proposed space transporter (1) comprises several modules (2) provided with solar p...
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WO/2023/096622A1 |
The invention relates to an unmanned aerial vehicle (1) arranged to self-destruct near a target (H), comprising a body (10), foldable wings (20) that comprise the wing body (21 ) connected to the body (10) and flaps (22) partially movabl...
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WO/2023/095924A1 |
This system comprises an unmanned transport machine (2660), a first winch (winding unit (2667)) capable of unwinding and winding a wire (2663), a luggage basket (2670) that is connected to the wire (2663) and used for containing luggage ...
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WO/2023/094723A1 |
The method in aerial firefighting and to an aerial firefighting vehicle (10) comprises maintaining fire-extinguishing liquid (100) in the aerial vehicle (10) and 5 maintaining solid liquid-absorbent preforms (90) in the aerial vehicle (1...
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WO/2023/094101A1 |
The present invention relates to a system (25) for converting and transporting electrical energy in a turbomachine-propelled aircraft, said system comprising: - at least a first rotary electric machine (26) connected mechanically to the ...
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WO/2023/094454A1 |
The present invention discloses a vacuum infusion system for infusing a fibre reinforcement with a resin comprising: a mould having a mould cavity comprising at least one moulding element for the reception of a fibre reinforcement, the s...
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WO/2023/096094A1 |
In an embodiment, a new type of wind power is developed through artificial intelligence, and electricity is generated using wind generated by vehicle traffic on a median strip of a road so as to implement an electric charging station and...
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WO/2023/094779A1 |
Disclosed is a device for generating electrical energy, comprising: a first loop for circulating a first two-phase element and comprising at least one first evaporating structure (2) fluidly connected to a first condensing structure (3);...
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WO/2023/092183A1 |
Embodiments relate generally to systems and VTOL aerial vehicles. An example central server system comprises: at least one central server system processor; and central server system memory storing central server system program instructio...
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WO/2023/094751A1 |
The present invention relates to an apparatus (100) for providing energy in an aircraft, comprising: - a DC bus (112); - at least one low-pressure electrical source (116BP) and at least one high-pressure electrical source (116HP). The ap...
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WO/2023/092962A1 |
An aircraft cockpit heating system, comprising a lubricating oil system and a vapor cycle system. The vapor cycle system comprises a heat exchanger (2) and a refrigerant-lubricating oil heat exchanger (3), wherein the heat exchanger is a...
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WO/2023/094746A1 |
The invention relates to a laminated glazing comprising a first outer glass sheet (1) and a second sheet (3), an adhesive layer (2), the edge of the sheet (1) being set back with respect to that of the sheet (3), a portion of the free su...
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WO/2023/093996A1 |
The invention relates to a boom assembly and a corresponding lifting assembly for helicopters (1), and a corresponding mounting method. The boom assembly is provided with: a base unit (8) having a first upper side and a first underside, ...
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WO/2023/095022A1 |
In an aircraft component where the aircraft component comprises a metal sheet (1.1, 1.2, 1.3, 1.4, 1.5, 1.6), the metal sheet (1.1, 1.2, 1.3, 1.4, 1.5, 1.6) comprises a normal region (5.1, 5.2, 5.3, 5.4) and a first surface milling regio...
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WO/2023/096965A1 |
A lighter than air platform an unfinned envelope having two or more propulsion elements coupled with the unfinned envelope proximate to the center of gravity. At least one navigation sensor is configured to monitor an actual flight path ...
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WO/2023/094289A1 |
An aircraft door (1) with lateral escape of the stops and opening by circular translation being provided with a pivoting manoeuvring arm (2) coupled to a forearm (3) articulated on the door and a mechanism for locking at least one actuat...
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WO/2023/092174A1 |
The present invention relates to a conveyor controlling apparatus and a conveyor controlling method for controlling a conveyor in accordance with environment parameters with respect to the conveyor. The conveyor controlling apparatus (Ba...
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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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