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WO/2024/069129A1 |
Systems and methods for supplying cooled air in a vehicle, for example an aircraft, are disclosed. The system comprises: an air cycle machine (ACM) configured to compress and cool a flow of air so as to produce a flow of cooled air; an a...
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WO/2024/072350A1 |
A hybrid air vehicle comprising a body (2); at least one motor (3) which provides required power for flight; at least one rotor (4) extending outward from the body (2) connected to the motor (3); a plurality of blades (5) located on the ...
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WO/2024/069080A1 |
The invention relates to a system for transmitting commands to N hydraulic servo-actuators, N being an integer greater than or equal to 2, the system comprising: N mechanical systems, each mechanical system comprising: - a rotary electri...
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WO/2024/072355A1 |
The present invention relates to a body (2) on an air vehicle; at least one actuator (3) on the body (2), which enables avionics equipment to move; at least one detector (4) positioned on the body (2) by means of at least two actuators (...
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WO/2024/072559A1 |
An unmanned aerial vehicle (UAV) includes a fuselage, a pair of fixed wings attached to the fuselage, a tail assembly attached to an aft portion of the fuselage and including a pair of stabilizers, a plurality of distributed propulsion u...
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WO/2024/072533A2 |
A system may include a plurality of unmanned aerial vehicles (UAVs), the plurality of UAVs including a first UAV and a second UAV. The system may include at least one recharging station and a ground station configured to, during a missio...
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WO/2024/073514A1 |
Systems and methods described herein include collapsible and deployable structures that may be used as antenna, collectors, reflectors, or other large structures. The systems and methods may use modular designs so that larger structures ...
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WO/2024/065915A1 |
A device for measuring carbon emissions of a passive house, arranged on a metal rain cap (2) at the top of a chimney (1). The device comprises an unmanned aerial vehicle (5), a guide assembly (3), and two landing support assemblies (6); ...
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WO/2024/069789A1 |
[Problem] To ensure safety in aerial imaging. [Solution] An aerial imaging system 1 comprises a mobile object 100 that flies over a target area F, a camera 141 mounted on the mobile object to capture an image of the target area, an event...
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WO/2024/069215A1 |
using UAV technology can be applied to road crack detection and using image processing techniques, the captured or scanned images of the infrastructure parts can be analyzed to identify any possible defects. Apart from image processing, ...
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WO/2024/072353A1 |
Invention relates to the unmanned aerial vehicle (I) wing deployment element (80) to enable the wings (20) to be deployed, wing deployment shaft (84) to enable the wing deployment element (80) to function and to enable the wings (20) to ...
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WO/2024/068255A1 |
A control system for apparatus to be operated on an aircraft or spacecraft, such as a satellite attitude determination and control system "ADCS", comprises a controller configured to implement one or more real time processes during norma...
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WO/2024/072359A1 |
The present invention relates to a body (2) on an air vehicle; at least one load (W) hitting the body (2); at least one main armor (3) on the body (2), which allows the protection of an area it covers on the body (2) against the impacts ...
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WO/2024/065022A1 |
The invention consists of a wind turbine that produces electrical energy when said turbine is rising through the atmosphere with the aid of a balloon filled with a gas that carries the turbine to high altitude, and that produces electric...
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WO/2024/065943A1 |
A deicing vehicle having a function of one-key return and a method for controlling the return of a boom. The deicing vehicle comprises an electric vehicle chassis (100), a power battery pack (200), a high-altitude operation device (300),...
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WO/2024/068918A1 |
The invention is directed to a site cabin (2) comprising an enclosure (4) comprising a floor (4.1), side walls (4.2, 4.3, 4.4, 4.5) and a roof (4.6), delimiting an inner volume; and anchoring points (4.7) on the side walls (4.2, 4.3, 4.4...
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WO/2024/066433A1 |
The present invention provides an unmanned aerial vehicle remote power switch apparatus having an identity information identification function, comprising a primary controller module, a secondary controller module, a primary Bluetooth mo...
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WO/2024/061159A1 |
A method for rapidly monitoring and determining the drought condition of summer corn on the basis of chlorophyll content by using an unmanned aerial vehicle. The method comprises the following steps: 1) calculating vegetation indexes, i....
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WO/2024/063791A1 |
Described is a fan assembly for an electrical aircraft motor having an axial fan with an inner hub of a first diameter and an outer hub of a second diameter. The outer hub may be concentrically aligned with the inner hub. A plurality of ...
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WO/2024/064626A1 |
The present invention provides methods and systems for remote operation of a vehicle with the capability to deal with communications jitter and intermittency. In particular, the methods and systems herein may safely predict a remote oper...
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WO/2024/060585A1 |
The present invention relates to a wing system integrated with a power battery module. The wing system comprises: a wing box, the wing box comprising a plurality of wing support members, and the plurality of wing support members being co...
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WO/2024/061095A1 |
An adjustment device for an aircraft entering a hangar, comprising sliding rails (10) and a conveying mechanism. The sliding rails (10) are connected to the ground. The conveying mechanism comprises a sliding base (20) and belt-type conv...
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WO/2024/062704A1 |
The recording control device according to the present embodiment comprises: a video data acquisition unit (103) that acquires video data obtained by capturing a region including the periphery of a mobile body; an event detection unit (10...
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WO/2024/062928A1 |
The present technology relates to an unmanned aircraft and a propeller in which it is possible to improve stability in a state in which a foldable unmanned aircraft propeller is opened. This unmanned aircraft comprises a propeller and a ...
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WO/2024/061146A1 |
A measuring device, which is used for measuring an assembly under test. Said assembly comprises an electric motor and a propeller, wherein the propeller is connected to an output end of the electric motor. The measuring device comprises:...
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WO/2024/060313A1 |
Disclosed in the present invention is an SMA-wire-driven reusable release mechanism with a self-resetting function. The present invention uses a two-stage load reduction and one-stage release structure. First-stage load reduction involve...
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WO/2024/060105A1 |
The present application provides a gimbal control method. A gimbal comprises a shaft arm assembly, the shaft arm assembly is used for carrying a load device, and the shaft arm assembly comprises at least one shaft arm and a motor for con...
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WO/2024/061691A1 |
A system for cleaning a waste tank (4) in an aircraft is proposed, comprising a service device, at least one spray nozzle, and a first adaptor (12) for each of the at least one spray nozzle, wherein the service device comprises a descali...
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WO/2024/062301A1 |
Provided is a vehicle comprising a fuselage provided with at least one storage module configured each to accommodate therein unmanned aerial systems and at least one docking module configured each to detachably interact with at least one...
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WO/2024/062249A1 |
A linear actuator (100) comprising a stroke axis (102), an actuator rod (104)extending along the stroke axis. The actuator rod comprises: an actuator rod outer surface (110), and a first screw thread (108) on a portion of the actuator ro...
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WO/2024/062181A1 |
One aspect of the invention relates to a method (100) for selecting an activation logic of an inerting system (3122) of at least one fuel tank of an aircraft (31) for at least one mission of the aircraft (31), the method (100) comprising...
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WO/2024/064128A1 |
Systems, methods, and device include a vehicle for providing horizontal directional control in a first transportation mode and a second transportation mode. The vehicle is an unmanned aerial vehicle with the duct defining a ducted air pa...
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WO/2024/060987A1 |
The present invention discloses a rotary actuator integrated with a gear nonius encoder and a control method, which relates to the field of aircraft devices. The rotary actuator comprises a permanent magnet synchronous motor, a gear noni...
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WO/2024/061514A1 |
The invention relates to a system for detecting a psychological state (10) of a passenger, comprising: - at least one detection sensor (11) capable of detecting at least one physiological parameter of the passenger, in particular a physi...
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WO/2024/060971A1 |
A linear actuator integrated with a gear nonius encoder and a control method therefor. The linear actuator comprises a motor (9), a control circuit module, a gear nonius encoder, and a ball screw pair for pushing a push rod (15) to perfo...
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WO/2024/061096A1 |
Provided are an automatic cargo loading and unloading system, and a hangar comprising the automatic cargo loading and unloading system. The automatic cargo loading and unloading system comprises a cargo box (10), a first cargo conveying ...
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WO/2024/062185A1 |
The invention relates to a spacecraft stack comprising: a stack of spacecraft (1) made up of a plurality of stages which are placed one on top of the other and each comprise a number of vehicles greater than or equal to N; a lower adapte...
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WO/2024/064434A1 |
A mechanism for attachment and detachment of a fixed or controllable airfoil to an airframe includes a base adapted for attachment to a root of the airfoil and a slot beam adapted for attachment along the airframe (e.g., parallel to the ...
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WO/2024/060567A1 |
An integrated electric propulsion system for electric aircrafts. A distributed electric propulsion system and a fly-by-wire flight control actuation system which are integrated on aircraft wings can be unified, thereby providing for the ...
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WO/2024/063723A1 |
This invention relates to a triple integrated camera system for the development of an autonomous vehicle that can avoid obstacles that allows successful autonomous flight by detecting both the width and height of the surrounding objects ...
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WO/2024/060633A1 |
An aircraft wing (10) having an integrated distributed ducted fan, the aircraft wing (10) being attached to a fuselage (20) and being provided with a ducted fan power set (30), wherein the ducted fan power set (30) is provided on an inbo...
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WO/2024/062370A2 |
A system for reconfiguring (1) the layout of a boat (100) is described, comprising a first fixed component (2) of coupling and a second movable component (3) of coupling; the first component (2) is configured to be attached to a fixed el...
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WO/2024/061089A1 |
An aircraft towing apparatus, comprising a frame body (10), a driving mechanism and a connecting mechanism. The driving mechanism comprises first driving wheels (20) and second driving wheels (30) respectively rotatably connected to two ...
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WO/2024/060123A1 |
A gimbal and an unmanned aerial vehicle. The gimbal specifically comprises: a support (10), which is used for carrying a camera device (20); an electric motor (11), which is used for driving the support (10) to rotate, and comprises a st...
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WO/2024/064122A1 |
Embodiments provide a flight supervision platform including a server computer and an animated graphical user interface for simultaneously monitoring multiple autonomous aircraft. More specifically, techniques disclosed herein provide a f...
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WO/2024/064270A1 |
An aircraft propulsion system includes a core engine that includes a core flow path where a core airflow is compressed in a compressor section, communicated to a combustor section, mixed with fuel and ignited to generate a gas flow that ...
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WO/2024/061016A1 |
Disclosed in the present invention are a single-encoder actuator for an aircraft and a power-on self-test method therefor. By means of a vector control algorithm, a controller controls a servo motor to rotate, and by means of a harmonic ...
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WO/2024/061148A1 |
A test frame for the strength of wings under static loads, comprising: a test frame body (100); a plurality of fixed-pulley blocks (200), the fixed-pulley blocks (200) being spaced apart on the test frame body (100); a plurality of weigh...
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WO/2024/061147A1 |
A cargo hold applied to an unmanned aerial vehicle, the cargo hold comprising a cargo hold door (700), and the cargo hold door being connected to the cargo hold of the unmanned aerial vehicle. The cargo hold also comprises a cable releas...
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WO/2024/056866A1 |
The present invention concerns a device for a multicopter that allows the multicopter to move without tipping over. This device generates propulsion according to the x- and/or Y-axis using the air displacement of the drive propellers and...
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