| Document |
Document Title |
|
WO/2023/119354A1 |
Provided is an engine generator unit which is exclusively for electric power generation and is capable of dampening the vibration of a horizontally-opposed engine without coupling the vibration. An engine generator unit 1, which is exclu...
|
|
WO/2023/118724A1 |
The invention relates to a hydraulic control circuit (57) of a dual-action orientation actuator (61) for the orientation of fan blades of a turbojet engine, comprising an oil reservoir (63), a variable-displacement axial piston pump (26)...
|
|
WO/2023/113908A1 |
An unmanned aerial vehicle (UAV) includes lift rotors and control rotors. The lift rotors are mounted to the UAV and oriented to provide a first vertical thrust to the UAV. The control rotors are mounted to the UAV outboard of the lift r...
|
|
WO/2023/108578A1 |
An expert-type aerial robot system (100) for autonomous field work. The system comprises an unmanned aerial vehicle platform (110); a computer vision system (120), comprising a camera and a visual processor connected thereto; a robotic a...
|
|
WO/2023/113394A1 |
An operating method of a smart drone for crime prevention, according to an embodiment of the present invention, comprises the steps of: receiving, from a wearable sensor worn on a subject to be guarded, a rescue request signal, an electr...
|
|
WO/2023/111469A1 |
The present invention relates to an annular air intake lip (40) for a nacelle (3) of an aircraft propulsion assembly (1), the lip (40) extending about an axis of revolution (X) and comprising: - an external annular wall (42), - an intern...
|
|
WO/2023/112245A1 |
One of the purposes of the present invention is to provide a management device that make it possible to properly calculate the tolls required for corridor transit. A management device according to one embodiment of the present disclosure...
|
|
WO/2023/110542A1 |
An elevation system (1) for an aircraft seat (S), the elevation system (1) comprising a support base (2) comprising a right lateral part (21) and a left lateral part (22), a first frame (3) comprising a lower end (31) mounted such that i...
|
|
WO/2023/114895A1 |
An aircraft tire component is disclosed herein, including natural rubber, a peptizer, carbon black, graphene, wherein the graphene has a thickness of less than about 3.2 nm, a particle size of between about 50 nm and about 10 µm, and co...
|
|
WO/2023/113652A1 |
The invention relates to the field of aviation. The claimed rotary-wing aerial vehicle comprises a fuselage, a front wing having mounted at its ends propellers that are tilted forwards in the direction of flight, and a rear wing. Mounted...
|
|
WO/2023/114402A1 |
Systems, methods and computer-readable media for telemetry data visualization are described herein. The described system includes paths and reduced components in between reception of sensor data and display to an engineer, reducing time ...
|
|
WO/2023/112343A1 |
The present invention comprises at least two internal combustion engines, which are a first internal combustion engine (20) and a second internal combustion engine (22), and at least four rotary wings, which are a first rotary wing (12a)...
|
|
WO/2023/114353A2 |
A fuel cell system (100) configured to provide electrical power to an electrical motor (102) producing propulsive thrust for an aircraft includes a plurality of fuel cell stacks (106) radially arranged about a central cavity (108). Fuel ...
|
|
WO/2023/109154A1 |
Disclosed are a wing and a method for improving control efficiency of a two-dimensional airfoil rudder surface. According to the technical solution, an original symmetric airfoil rudder surface is transformed into an asymmetric airfoil r...
|
|
WO/2023/111438A1 |
The invention relates to a hydraulic assembly (450) for an aircraft engine, the assembly comprising: - a pump (54) comprising a housing (54a) and a rotor (54b) arranged inside the housing (54a), the housing (54a) having at least one hydr...
|
|
WO/2023/114523A1 |
Method and tools for manufacturing core foam sections for a propeller is disclosed. In an embodiment, a method comprises wrapping a first adhesive film around pre-drilled rods; placing the rods into a first mold using placement features;...
|
|
WO/2023/112023A1 |
A boom member for in-flight refueling includes a first boom member portion, a second boom member portion, and a connect/disconnect mechanism. The first boom member portion includes a first boom lumen, a first boom axis, and a fuel receiv...
|
|
WO/2023/111445A1 |
The invention relates to a method for regulating the speed of a propulsion device of a hybrid propulsion unit for an aircraft comprising: the propulsion device and an MGB; the heat engine and at least one electric motor, mounted in paral...
|
|
WO/2023/111476A1 |
A method for managing the torque of an aircraft turbomachine comprising a fan (6) or a propeller of variable pitch connected to a turbine (5) by a shaft (7) and a reduction gear (8), and an electric generator (9) connected to the shaft (...
|
|
WO/2023/113654A1 |
The invention relates to the field of video and audio communication, and more particularly to devices for receive, transmit and display purposes. An arrangement of devices for receiving, processing, storing, transmitting and reproducing ...
|
|
WO/2023/113058A1 |
Disclosed is a drone control method for precise landing. The drone control method according to an embodiment of the present invention may comprise the steps of: when a drone is switched to an arming mode in a drone station, setting curre...
|
|
WO/2023/111517A1 |
An interface node for enabling a robotic arm to be used as a reconfigurable fixture for vehicle manufacture is described. The interface node comprises an attachment element for attaching the interface node to the robotic arm. The interfa...
|
|
WO/2023/115004A1 |
A package coupling apparatus for securing a package to an unmanned aerial vehicle (UAV) is provided. The package coupling apparatus includes a hanger and a strap coupled to the hanger. The hanger includes a base configured, to be positio...
|
|
WO/2023/114373A1 |
Described herein is an aerial material delivery system (100), which includes an unmanned aerial vehicle (UAV) (102) and a material dispensing assembly (114) mounted to the UAV (102). The material dispensing assembly (114) includes a rota...
|
|
WO/2023/113651A1 |
The invention relates to nautical and aeronautical design, and more particularly to flow propellers for use in water or air, and can also be used as a generator for converting water and air flows into electrical energy. A flow propeller ...
|
|
WO/2023/113753A1 |
The present invention comprises a stratospheric unmanned aerial vehicle in which 5 solar panels and internal electric power unit are used as hybrids, and particularly, in order to ensure the security of civilians and military personnel, ...
|
|
WO/2023/112681A1 |
Provided is an information processing device comprising: a status-related information reception unit that, with respect to a flying object that, functions as a stratosphere platform and emits, from a service link (SL) antenna, an SL beam...
|
|
WO/2023/111199A1 |
An aerodrome structure (100) for use in cooperation with a loading dock (20) of a building comprises a lift structure and a cargo transition structure (150). The lift structure comprises an upstanding structure (130); a platform (110) lo...
|
|
WO/2023/108817A1 |
The present invention relates to the technical field of flight, and provides a propeller, a power assembly, and an aircraft, used for solving the technical problems of high noise and an increase in resistance caused by the fact that blad...
|
|
WO/2023/114078A1 |
A ground-based content curation platform identifies geographically-relevant content having metadata indicating a geographic relevance area which satisfies a relevance rule relative to the present location of the aircraft. The platform di...
|
|
WO/2023/109114A1 |
Disclosed in the present invention is a reconstructable flying car. A car body main body is detachably connected to a wing assembly, a propulsion assembly, an empennage assembly, and multi-axis rotor assemblies by means of a connecting m...
|
|
WO/2023/110533A1 |
The invention relates to a manned aircraft (1) with wing parts (3, 5), an internal combustion engine (9) which is connected via a shaft (11) to a left-hand thrust nacelle (13) and to a right-hand thrust nacelle (15) which can be pivoted ...
|
|
WO/2023/112034A1 |
A method for converting a conventional airplane having at least one thermic reaction propulsion engine and at least one fuel tank fluidly connected through fuel pipes to an electric propulsion airplane is disclosed that comprises: removi...
|
|
WO/2023/111484A1 |
One aspect of the invention relates to a system (20) for transmitting commands to at least one hydraulic servo actuator (30), comprising: - a mechanical system (21) including: o a rotary electrical actuator (211) comprising a first and a...
|
|
WO/2023/115001A1 |
A package coupling apparatus for securing a package to an unmanned aerial vehicle (UAV) is provided. The package coupling apparatus includes a support plate configured to be secured to an upper surface of the package and a handle extendi...
|
|
WO/2023/113647A1 |
The invention relates to the field of temperature measurement and heat measurement and can be used for the remote detection of icing. A method for determining the phase transition temperature and volume of a sample of liquid includes det...
|
|
WO/2023/112242A1 |
To enable a route that satisfies a request of a user who operates an unmanned aerial vehicle to be presented in a style according to a predetermined format, the present invention involves: acquiring departure location information indicat...
|
|
WO/2023/105659A1 |
Provided is a management device comprising a reception unit which receives transport information corresponding to an application for use of an aerial transport path formed indoors in order to form indoors the aerial transport path used b...
|
|
WO/2023/105525A1 |
Disclosed is an autonomous vehicle configured for locomotion on an extraterrestrial body (e.g., a planet such as the Moon) and carrying out one or more missions thereon. The vehicle can be configured to ascend, translate, and descend to ...
|
|
WO/2023/105514A1 |
A system for object measurement including one or more user devices having a camera, one or more modules performing one or more tasks, a memory unit for storing, loading, and/or maintain the modules. The user's device further having a pro...
|
|
WO/2023/105220A1 |
A seat assembly for a vehicle is provided, the seat assembly comprising: a support assembly comprising a front spar and a rear spar; a seat base mounted to the support assembly; a seat back pivotally mounted to the support assembly and m...
|
|
WO/2023/107541A1 |
A tray table indicator includes a channel, a cover, and a magnetic ball. The channel has a first extension, a curve, and a second extension, and the cover encloses the channel. A magnetic ball is contained within the channel and is movab...
|
|
WO/2023/102911A1 |
A data collection method, a data presentation method, a data processing method, an aircraft landing method, a data presentation system and a storage medium. The data presentation system comprises a vehicle and an aircraft, wherein the ve...
|
|
WO/2023/104777A1 |
The invention relates to a method for checking the maximum power available to members of a propulsion system of an aircraft (1) comprising first members (M1.1, M2.1, D10, TG, BAT1) that are sized to compensate for the failure of second m...
|
|
WO/2023/106538A1 |
The present invention relates to a drone having a movable propeller shaft, the drone comprising: a drone body having an opening; a plurality of propeller shafts arranged radially on the drone body, each propeller shaft having one side po...
|
|
WO/2023/102670A1 |
The present invention relates to the calibration of antennas by means of autonomous or unmanned aircraft vehicles (UAVs) also known as drones. In particular, the invention discloses a system and a method to calibrate antennas by means of...
|
|
WO/2023/106369A1 |
Provided are: a polyimide film which, when used as a spacecraft material, exhibits excellent resistance to atomic oxygen derived from oxygen molecules which are a residual atmosphere component, and produces few outgassing components when...
|
|
WO/2023/104965A1 |
The invention relates to an acoustic system (10) for use in an interior of an aircraft (300), including an upper body support section (12) for use with an aircraft seat (100) and/or an aircraft bed (200). The upper body support section (...
|
|
WO/2023/105634A1 |
The present invention is equipped with: a flying vehicle 20 contained in a Faraday cage 10; a power supply unit 30 which supplies power to the flying vehicle 20 and is built into the Faraday cage 10; a first voltage-dependent switch 31 w...
|
|
WO/2023/107037A1 |
The present invention relates to at least one main housing (2) which is located on the helicopter between the engine and the rotor and contains the elements for transmitting power from the engine to the rotor; a main shaft (A) that provi...
|
