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WO/2023/060350A1 |
An aerial vehicle with adjustable vertical lift and methods of using thereof for agricultural and/or pest control applications, such as on farms, golf courses, parks, and/or along roadways, power lines, etc. is provided by the present di...
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WO/2023/064679A1 |
An aircraft (20, 22) propulsion system includes an engine. The propulsion system further includes an inlet (36) having a forward cowl lip (38, 3, 40) and an aft cowl lip (40). The forward cowl lip (38, 3, 40) moves between retracted and ...
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WO/2023/062254A1 |
The present invention relates to an apparatus and system for extinguishing forest fires by a continuous, uninterrupted supply of water and flame-retardant products to the fire front. It consists of an apparatus suspended in the air by dr...
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WO/2023/062765A1 |
A shape/posture estimation device (50) is configured to comprise: a light intensity curve acquisition unit (54) which acquires, from a light intensity measurement device (10) for measuring light intensity of a moving body (1) to be monit...
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WO/2023/062514A1 |
A vertical take-off and landing (VTOL) vehicle (1) has a main body (10) including airfoil sections (13) on either side of a central module (20) in which a load may be carried. Articulated forward thrust systems (SOL, 50R) are mounted on ...
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WO/2023/062747A1 |
Provided is a system for using an unmanned aerial vehicle to image, for inspection, a blade of a wind power generation device, the unmanned aerial vehicle flying on the basis of a flight plan path set in advance and comprising an imaging...
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WO/2023/062912A1 |
Provided are a cable protection member advantageous for making cable protection work efficient and an aircraft lavatory unit equipped with the cable protection member advantageous for making the protection work of a cable used in the air...
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WO/2023/060326A1 |
The present application to a utility model pertains to the sector of devices and accessories for operating unmanned aerial vehicles, more specifically those designated as "drones"; the solution provides an extremely versatile platform en...
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WO/2023/062691A1 |
This flight vehicle comprises: attachment sections that are disposed at the tips of a pair of fixed wings disposed to the left and the right with a main body therebetween, and that have side surfaces on sides facing away from the main bo...
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WO/2023/062350A1 |
A method is provided of arranging an aircraft interior dependent on whether the aircraft is a twin aisle or single aisle aircraft. A passenger seating arrangement is provided, dependent on whether the aircraft is twin or single aisle.
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WO/2023/062675A1 |
Provided is a drone protection system for protecting a drone 2 from thunderstroke, the drone protection system comprising a Faraday cage 1 which surrounds the drone 2 and a wire 3 which can move on the Faraday cage 1 while an end portion...
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WO/2023/060712A1 |
The present invention relates to the technical field of aircraft deicing, and in particular, to a novel steam jet multifunctional aircraft deicing vehicle, comprising a vehicle body. A steam generation assembly is provided in the vehicle...
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WO/2023/061587A1 |
The present invention describes a technology to simulate extraterrestrial conditions for investigating the effect of microgravity and CO2 rich atmosphere on animal and vegetable cells cultivation and a process thereof exploiting extrater...
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WO/2023/062286A1 |
An electrical engine mounting arrangement (1) for providing propulsion power to a vehicle (90V, 90AV) is disclosed. The arrangement (1) comprises a mounting block (10), an electric motor (40, 41), a power transfer shaft (43, 43a, 43b) ar...
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WO/2023/064188A1 |
The disclosed invention describes a method for determining a current state of a gas cell in an airship, particularly the lift. A computing device receives depth measurements of the interior of the gas cell using a lidar sensor positioned...
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WO/2023/062439A1 |
The present disclosure relates to conveyance means for aerial vehicles, and discloses a cable-powered conveyance system (100) for an aerial vehicle. The system (100) comprises a structure (20) defined by a plurality of columns having ele...
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WO/2023/062646A1 |
The present invention relates to a system and method of mobile orbital launchers. The mobile launcher of the present invention mainly consists of the launch vehicle and launch related subsystems. All the systems will fit on a trailer whi...
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WO/2023/062689A1 |
An aerial vehicle according to the present invention comprises: a structure for flying as an aircraft; a control system for flying as an aircraft; a structure for flying as a multicopter; and a control system for flying as a multicopter;...
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WO/2023/063141A1 |
An EDS (50) includes a motor housing (70) and an inverter housing (90). The inverter housing (90) includes inverter fins (92). The motor housing (70) includes motor fins (72) and motor guide plates (77). The motor fins (72) and the motor...
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WO/2023/062290A1 |
The invention relates to a firefighting device (2) comprising a removable tank (3) configured to be removably installed in an aircraft, a liquid discharge opening (7) configured to be located facing the rear loading door of the aircraft,...
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WO/2023/064215A1 |
An ejector nozzles for an aircraft can include ducts that transition axially from a first cross-sectional shape, to a second cross-sectional shape that is geometrically non-similar or dissimilar to the first shape. In representative embo...
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WO/2023/064713A1 |
An aircraft skin coating assembly for an aircraft. The coating assembly includes a primer layer (34) deposited on the aircraft skin (32), an optical stop-etch layer (52) deposited on the primer layer (34) that is reflective at a predeter...
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WO/2023/061897A1 |
A dispersion system (10) for a vehicle (1) is described, wherein the vehicle has at least one door opening (5). The dispersion system comprises at least two tank modules (100) including a reservoir (110) for storing a medium to be disper...
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WO/2023/062611A1 |
Disclosed is a multicopter foldable between a stowed state and an operational state, the multicopter comprising a hub configured to receive one or more payloads and a battery, two or more flight arms that extend substantially horizontall...
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WO/2023/064944A1 |
A lighter-than-air craft including an envelope. A mixture of helium and hydrogen disposed within the envelope. The mixture having a ratio of helium to hydrogen such that the mixture is nonflammable during operating conditions for the lig...
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WO/2023/060678A1 |
An aircraft (1), comprising a fuselage (10), a wing assembly (20), a tilt rotor assembly (50), and a coaxial dual-rotor assembly (60). The wing assembly (20) is connected to the fuselage (10); the tilt rotor assembly (50) is tiltably con...
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WO/2023/063828A1 |
The present disclosure relates to remote accumulation of an analyte from a fluid medium in a fluid sampler that comprises a collection medium for accumulating the analyte. There is provided a mobile platform (20) configured to perform de...
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WO/2023/062690A1 |
This flight vehicle comprises: a plurality of arms one end of each of which is connected to a body; an attachment part that is provided to the other end of each of the plurality of arms; propellors that are attached to the attachment par...
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WO/2023/063140A1 |
An EDS (50) has a motor housing (70) and an inverter housing (90). The inverter housing (90) has inverter fins (92). The motor housing (70) has forward inclined fins (721) as motor fins (72). The forward inclined fins (721) are provided ...
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WO/2023/063680A1 |
A catapult is disclosed. The catapult according to an embodiment of the present invention, comprises: a take-off assisting member contacting an aircraft to push the aircraft; a power source coupled to the take-off assisting member to dri...
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WO/2023/061155A1 |
A space station common-view time comparison orbit error correction method, comprising five parts, i.e., determination of simultaneous visual moments of two stations, calculation of projection coefficients of orbit errors, calculation of ...
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WO/2023/062329A1 |
Rear assembly for a turbojet engine nacelle, comprising at least one composite wall (20) separating a cold portion (8) from a hot portion (12) comprising an element to be cooled (23), the composite wall (20) comprising first and second s...
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WO/2023/062751A1 |
A controller according to one example of the present disclosure is provided with: a body module including an operating machine that outputs an operation signal in response to input of a user's operation for steering a drone equipped with...
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WO/2023/062731A1 |
A detection satellite (220) of a satellite constellation (200) detects launch of a flying object and transmits launch detection information to each artificial satellite on a detection orbital plane via communication with front and rear a...
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WO/2023/059427A1 |
The systems/methods analyze the vast reservoir of data that is collected in-flight during a commercial aircraft's travels over several months. That data is analyzed to identify and remove data points that do not represent stable cruise. ...
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WO/2023/059820A1 |
Embodiments of the invention provide a carrier for the organization and delivery of payload when used in conjunction with a motorized vehicle. The carrier comprises a housing defining an interior; at least one holder, wherein the interio...
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WO/2023/057198A1 |
A signal transmitter apparatus configured for use in an aircraft moveable element monitoring system. The signal transmitter apparatus comprising a signal transmitter circuit. The signal transmitter circuit comprises: a first electrical p...
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WO/2023/059650A1 |
Methods and systems for testing an aircraft in-flight are described herein. The method can include receiving a test deck including one or more test cards, with an individual test card including an ordered list of points. For an individua...
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WO/2023/057433A1 |
The invention relates to a method for aligning at least one object (3) that reflects and/or emits radiation (1) onto a reflection point (2), using at least one unmanned aerial device (4) having a camera for capturing the radiation (1), t...
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WO/2023/057440A1 |
A passenger seating arrangement for an aircraft cabin is disclosed. A plurality of seat units each comprise at least a first reclining seat and a second reclining seat. The seat units are located in a column adjacent to a longitudinal ai...
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WO/2023/057377A1 |
The present invention relates to a method for manufacturing a connection part (10) between a wing box (20) and a leading edge module (30). The method comprises the steps of carrying out a three-dimensional digitization of a first part re...
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WO/2023/059257A1 |
The invention relates to a repellence system (50) and method for repelling animals (40). The repellence system (50) comprises an imaging device (14, 24) arranged to generate image data from a surveillance area (30, 31), one or more deter...
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WO/2023/058721A1 |
Provided is a flight device with a simplified mechanism for transmitting motive power.　The flight device 10 comprises an airframe 19, a main rotor 14, an engine 30, and a power transmission shaft 25. The main rotor 14 rotates to thereb...
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WO/2023/057672A1 |
The invention provides aerodynamic lift, or downward thrust for the amphibious environment, by means of two conical frames that are opposed at the bases and counter-rotating, thus cancelling out the opposing torque moment when rotating, ...
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WO/2023/059219A1 |
The invention relates primarily to means for carrying out extra-vehicular activity on the surface of celestial bodies. The proposed hermetic coupling device comprises: a hermetic cabin (1); a frame (2) with an interface (3); electrically...
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WO/2023/057606A1 |
The invention relates to a rocket stage (1) for a multistage space launch vehicle (3, fig. 3), comprising a main engine (5) and being configured for stage separation from the remaining parts of the space launch vehicle (3, fig. 3) such t...
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WO/2023/059178A1 |
Embodiments relate to methods, systems, and devices for performing an inspection on a telecommunication structure and/or one or more objects that are attached on the telecommunication structure. The system includes an unmanned aerial veh...
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WO/2023/058329A1 |
Provided is a wall surface work device 1 comprising: a travelling body 2 which can travel with respect to a wall surface W; an ascending/descending support device 3 which is provided with support columns 3a that are installed to the left...
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WO/2023/056516A1 |
A drone system and method for deploying and autonomously refuelling. The drone system includes a base station and a drone. The base station and drone are configured for autonomous refuelling when the drone has landed in the base station....
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WO/2023/059413A1 |
Electroaerodynamic devices and their methods of operation are disclosed. In one embodiment, ions are formed by dielectric barrier discharge using a time-varying voltage differential applied between a first electrode and a second electrod...
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