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Patent Searching and Data


Matches 251 - 300 out of 57,454

Document Document Title
WO/2022/066922A1
The helicopter drizzle pipe allows for aerial wildfire suppression efforts in otherwise inaccessible areas. The pipe is balanced between the bottom legs of the helicopter as to prevent an imbalance or obstruction to the helicopter rotor ...  
WO/2022/061805A1
A spraying operation control method and device, a storage medium, and an agricultural unmanned aerial vehicle. The agricultural unmanned aerial vehicle comprises multiple propellers and multiple nozzles, and at least one nozzle is provid...  
WO/2022/062233A1
A fly-by-wire flight control system and a control method. The fly-by-wire flight control system comprises: a cockpit control device used to provide a cockpit control instruction; an electronic flight control apparatus communicatively con...  
WO/2022/056570A1
The invention relates to a method for treating stale air in an aircraft cabin (4) of an aircraft (1), in particular for rendering pathogens, such as viruses, harmless, said method having the steps of: removing stale air from the aircraft...  
WO/2022/058562A2
An aerodrome maintenance apparatus for monitoring runway and taxiway conditions and remotely reporting the status of the runway or taxiway. The apparatus comprises: a drive unit arranged to mount one or more rails to provide movement of ...  
WO/2022/060266A1
Embodiments herein disclose e.g. a method for handling inspection of a structure performed by a mobile device in a communications network. The network node obtains indications of parameters relating to network parameters, machine learnin...  
WO/2022/061021A1
A multi-segment oblique flying wing aircraft which has three distinct segments including two outer wing segments and a central wing segment. The central segment may be thicker in the vertical direction and adapted to hold pilots and pass...  
WO/2022/057115A1
An airplane wing fuel tank access cover and a structure of a peripheral area of the access cover, relating to the technical field of aviation. The airplane wing fuel tank access cover comprises an inner access cover (7), an outer access ...  
WO/2022/058903A1
The invention relates to a logistics station for drones, which can be adapted to different drones (12) and comprises at least one landing zone including means for holding a drone, a robot (30) for replacing the drone batteries and/or cha...  
WO/2022/060661A1
A reusable modular spacecraft has a spacecraft bus structure configured to support spacecraft subsystems, at least one interchangeable housing component configured to be interchangeably received and supported by the bus structure, and a ...  
WO/2022/058687A1
Disclosed is an aeronautical conveying and release device, actuated by a cartridge, comprising a housing provided in a body 60 comprising a recess having an open end and a bottom, a cartridge adapter 62 capable of closing the recess and ...  
WO/2022/059875A1
A drone station according to an embodiment of the present invention comprises: a roof (11) allowing a drone (100) to land thereon; a side wall (12) formed to be erected around all sides of the roof (11) from the lower side of the roof (1...  
WO/2022/059846A1
The present invention relates to a system and a method for controlling leader-following flight in an aerial vehicle swarm flight. The system for controlling leader-following flight in an aerial vehicle swarm flight according to the first...  
WO/2022/056597A1
An aircraft structure (10) comprising a fuselage (24), first and second forward wings (20, 22) mounted to and/or extending from opposing sides of the fuselage (24), a continuous rear wing span (34) defining first and second rear wings (3...  
WO/2022/056623A1
A landing gear for a vehicle includes a strut configured for reciprocating movement between a stowed position and a deployed position. A shock absorber has a first element slidingly disposed within the strut and a second element slidingl...  
WO/2022/061003A1
A hybrid airship-aerostat includes a hull, a motor, a fin, a controller, and a bridle system. The motor is coupled to the hull and is configured to rotate between a thrust configuration and a lift configuration. The motor is configured t...  
WO/2022/059047A1
A composite component (1) comprises: a first composite component (10) that is equipped with a base portion (11) to which a second composite component (20) is fixed, and a positioning portion (12) provided on the base portion (11) and pro...  
WO/2022/053759A1
The invention relates to a method for manufacturing a part made of composite material comprising a reinforcement area, by thermocompression of a first and a second material, the method comprising the following steps: - depositing the fir...  
WO/2022/055534A1
Described herein is a privacy panel for a passenger includes a main body positioned between adjacent passenger seats and an attachment mechanism removably coupled to the main body. The attachment mechanism may include a first attachment ...  
WO/2022/055795A1
Disclosed are devices, systems, apparatus, methods, products, and other implementations, including a method for detecting damage in a geographical area that includes receiving a first image of the geographical area, with the first image ...  
WO/2022/054931A1
The purpose of the present invention is to improve the recovery rate for lithium contained in a lithium ion cell. This method for recycling lithium ion cells includes: a first electrical discharge step S102 in which electrical discharg...  
WO/2022/055673A1
Mining apparatuses, systems, and methods related to using a rocket engine's plume and a collection manifold to efficiently displace, collect, process, and store frozen volatiles embedded within or below a surface are disclosed. The plume...  
WO/2022/054095A1
The present embodiment provides a scalable drone architecture or drone (100) having a frame (102), a number of arms (104), a number of landing gears (106), a number of modules (204, 206) and having an enhanced strength irrespective of th...  
WO/2022/053768A1
The invention relates to a method for manufacturing an aerospace and/or aeronautic tubular composite part (1), said tubular composite part (1) comprising a tubular body (10) and at least one flange (22). The method comprising the followi...  
WO/2022/053527A1
The invention relates to an aircraft radome (1) comprising a composite structure (10) comprising, or according to the circumstances configured to define, at least one housing (20) extending along the radome from a base (2) of said radome...  
WO/2022/055766A1
A 3D printed additively manufactured (AM) elliptical bifurcating torsion flexure assembly system includes a base section; elliptical bifurcating torsion springs, each including a bifurcated legs section supported by the base; a bifurcate...  
WO/2022/052645A1
An unmanned aerial vehicle (100), comprising: a fuselage assembly (1), the fuselage assembly comprising a storage device (11); vehicle arm devices (2), the number of the vehicle arm devices being two, the vehicle arm devices being locate...  
WO/2022/053984A1
An aircraft frame includes a fuselage, at least one boom and a wing structure including a first lifting surface having a first root portion located proximate the at least one boom and a first tip portion where at least a portion of the f...  
WO/2022/053177A1
An actuator control system can include a plurality of electro-mechanical actuators for operating one or more end effectors, a plurality of position sensors associated with the plurality of electromechanical actuators, each of the plurali...  
WO/2022/052644A1
An unmanned aerial vehicle (100), comprising a vehicle body assembly (1), vehicle arm devices (2) and power devices (3). There are two vehicle arm devices (2) respectively located at two opposite sides of the vehicle body assembly (1), t...  
WO/2022/052349A1
A boarding bridge (1) anti-collision method and a boarding bridge anti-collision system. The boarding bridge anti-collision method comprises: obtaining a pre-configured boarding bridge protection area; performing scanning and obtaining t...  
WO/2022/054388A1
This method for manufacturing a sandwich panel (100) includes: a step for preparing a plurality of sheet-like prepregs (211); a step for obtaining a composite surface material (40) by performing a first heating and pressing treatment via...  
WO/2022/053806A1
A contactless credential reader which is arranged to be installed in a rearward portion of a passenger seat of a transportation vehicle, such as an aircraft, in which the reader is arranged to be capable of being installed as either a re...  
WO/2022/053972A1
Device for aerial release of flexible elements with a closed profile. The invention relates to a device for efficient and fast aerial release, one by one, of a large number of ring-type flexible elements with a closed profile. The device...  
WO/2022/055629A1
Systems and methods for machine-learning-based aircraft (102) icing (204, 212, 222) prediction use supervised and unsupervised learning (328) to process real-time environmental data, such as onboard measurements of outside air temperatur...  
WO/2022/053178A1
An actuator control system can include a plurality of electro-mechanical actuators for operating one or more end effectors, a plurality of position sensors associated with the plurality of electro- mechanical actuators, each of the plura...  
WO/2022/055677A1
A landing pad for an unmanned aerial vehicle ("UAV") is disclosed. The landing pad includes a support structure, a charging pad, and a plurality of movable UAV supports. The charging pad is coupled to the support structure and able to mo...  
WO/2022/052339A1
A lens, a camera, and an unmanned aerial vehicle. The lens (100) comprises: a lens body; a first lens assembly (102), fixed on the lens body; a second lens assembly (103), configured to move relative to the lens body to change a focal le...  
WO/2022/053583A1
Disclosed is a device for actuating a leg (2) of an aircraft landing gear, comprising an electronic control assembly and a leg deployment/retraction actuator (10), the actuator comprising an electric motor having a stator comprising at l...  
WO/2022/054523A1
The present invention provides a discharge device that is capable of having an aerosol container attached thereto and detached therefrom, and that is provided with: a pressing part for pressing a stem for opening and closing a valve of t...  
WO/2022/050031A1
The present invention provides a flying device comprising a flight communication unit (24), a device fall determination unit (25, S101), and a flight notification unit (25, S104, S105). The flight communication unit performs wireless com...  
WO/2022/050290A1
Provided are: a silicon nitride sintered body that has good mechanical properties, in particular fracture toughness, and has good product life when processed into a product; a rolling body using same; and a bearing. The silicon nitride s...  
WO/2022/050320A1
This supply-airlifting system comprises: a self-propelled robot 1; an aircraft 2, on which supplies 21 and the robot 1 can be loaded; and a descent/loading device 3 that allows for at least the robot 1 to descend from the aircraft 2 to t...  
WO/2022/049332A1
The invention relates to a telescopic mast (100) comprising: • - coaxial segments (101_1,..., 101_N) that can be controlled from a stowed position to a deployed position, • - a set of guide systems (104, 104P) arranged between the ad...  
WO/2022/049568A1
A flight safety drone stabilization system for drones, comprising an onboard controller which is configured to continuously detect in-flight unbalancing loading by receiving signals from suitable onboard sensors (e.g., gyroscopes) and/or...  
WO/2022/050507A1
A method and a system for monitoring a photovoltaic power generation module, according to one embodiment of the present invention, comprises: an unmanned aerial vehicle which flies over a plurality of photovoltaic panels included in a ph...  
WO/2022/051511A1
A spacecraft propulsion system comprises an attitude adjustment thruster system with multiple thrusters (488a-d) receiving heated propellant via a shared thermal capacitance block (275). The thermal capacitance block (275) with integrate...  
WO/2022/051409A1
A system and method for improving the flight control and efficiency of an aerial vehicle. Many embodiments are directed to a rotor-shroud assembly system where a plurality of rotor blades are connected to the internal side of a shroud an...  
WO/2022/050928A1
A wing (1) for a vertical takeoff and landing aircraft (2) consists of an airfoil portion (3) and, hingedly attached thereto, a first high lift section (4) comprising a set of propulsors (6) arranged above the profile of the wing. The wi...  
WO/2022/049379A1
A hybrid VTOL drone is provided and comprises a minimum of four propellers fixedly mounted and disposed onto a frame that includes a pitch shaft, and a wing rotatably mounted to the pitch shaft, wherein the wing is rotatable around a pit...  

Matches 251 - 300 out of 57,454