| Document |
Document Title |
|
WO/2023/218138A1 |
The invention relates to a method for detecting an anomaly in a system (110) of an aircraft (100), comprising: - obtaining a current series of measurements of one or more physical quantities (PT1, PT2) of the system (110), during a time ...
|
|
WO/2023/217807A1 |
A filling level monitoring device (100) for monitoring a filling level (210) of a fluid in a container (200) includes exciter(s) (10), sensor(s) (20), a signal source (30) connected to the exciter(s) (10), a processor (40), at least one ...
|
|
WO/2023/218674A1 |
This flying body comprises: a communication device; a receiver that acquires a current position; a flight controller that controls flight and is able to transmit current position information by using the communication device; a plurality...
|
|
WO/2023/220155A1 |
Methods, systems and processes to provide energy to power remote and industrial sampling and monitoring stations as well as other ancillary electrically powered pipeline equipment such as hydrogen collection and production units and the ...
|
|
WO/2023/217666A1 |
An inflatable bladder (33, 41) configured to be carried by an aircrew garment (35, 43, 34, 42) worn on the body of the aircrew and to apply pressure to the body when inflated by a gas to counteract effects of high G-forces during flight....
|
|
WO/2023/218282A1 |
Described is an integrated electronic control system including keypad with a keypad connector, one or more galley inserts controllable by the keypad; and a control board couplable with the keypad and the galley insert. The control board ...
|
|
WO/2023/219981A1 |
Various embodiments of the present disclosure provide methods of using a strap for supporting and transporting a package via an aerial vehicle.
|
|
WO/2023/220375A1 |
A technique provides a field service tool (FST) that allows customers to view and store engine performance data, including faults, in a convenient manner. The technique allows customers to gain insights into performance anomalies while p...
|
|
WO/2023/219424A1 |
A method and a device for verifying aircraft status information are disclosed. According to one embodiment of the present disclosure, a method by which a UAM aircraft verifies aircraft status information may comprise the steps of: receiv...
|
|
WO/2023/217918A1 |
The invention relates to a tachometer (10) for an aircraft wheel (R) mounted on an axle (E) so as to rotate about an axis (X) of rotation, the tachometer comprising a stator (20) that is intended to be attached to the axle (E) and a roto...
|
|
WO/2023/212788A1 |
The present patent application to a wing tip thruster rotation system describes a system for rotating wing tip thrusters (EDF or turbofan engines), belonging to the field of aircraft equipment, more precisely for use in aircraft of the c...
|
|
WO/2023/213006A1 |
An overwater life-saving device, comprising a closed cabin body (1), a propeller and a steering mechanism (2) which are located outside the closed cabin body, and, a lifting and lowering mechanism (3), a rotation platform (4), a mechanic...
|
|
WO/2023/214930A2 |
|
|
WO/2023/215326A1 |
The present disclosure provides modular hydrogen-fuel storage assemblies with an external form factor corresponding to Unit Load Device (ULD) cargo containers (100), allowing the assemblies to be easily loaded into and stored in a cargo ...
|
|
WO/2023/214128A1 |
The invention relates to a hybrid electrical architecture (101) for an aircraft (103) which comprises a turbomachine (107) and a reduction gearbox (111) intended to rotate at least one propulsion member (105) of the aircraft (103). The a...
|
|
WO/2023/213373A1 |
The invention relates to "mobile units" which inseparably include: a cylindrical outer casing with low taper or constant cross-section; one or more motorised longitudinal fluid channels which are each "convergent" at the inlet and subseq...
|
|
WO/2023/213598A1 |
The present disclosure relates to a method (50) for generating an image using a satellite (10), wherein partial zones are processed successively and the processing of each partial zone comprises: - receiving (S51) at least two basic part...
|
|
WO/2023/213420A1 |
The invention relates to a, preferably pumpless, pressure fed propulsion system for a spacecraft, preferably a satellite or microsatellite, the system comprising: - a propellant tank (101) for storing a propellant; - a first heat exchang...
|
|
WO/2023/214378A1 |
A first communication device can determine (410) that a second communication device is within an area. The first communication device can determine (420) an identifier of the second communication device. The first communication device ca...
|
|
WO/2023/215664A1 |
Described herein is a power processing unit (PPU) for use with a Hall Effect Thruster (HET) and a Propellant Management Assembly (PMA) of a spacecraft. The PPU comprises an anode and ignitor supply subsystem that provides anode and ignit...
|
|
WO/2023/215632A1 |
An aircraft lift enhancement system is provided. The aircraft lift enhancement system includes an airfoil and at least one rotor. The airfoil includes a leading edge and a trailing edge defining a longitudinal axis of the airfoil, and a ...
|
|
WO/2023/214179A1 |
A drone port has a set of autonomous transport robots (or rovers) that can collaborate with each other, are automated and can provide a scalable drone service unit or system within an existing building. The rovers are able to transport o...
|
|
WO/2023/214726A1 |
To solve three disadvantages of the currently used wildfire extinguishing methods (geographical constraints, inefficiency of the fire extinguishing method itself, and the risk of very low altitude flight), the present invention relates t...
|
|
WO/2023/215574A1 |
A method of moving a spacecraft from an initial orbit to a final orbit includes providing a spacecraft with thrusters traveling in an initial orbit that has a first RAAN. Thrusters are activated to move the spacecraft into a transfer orb...
|
|
WO/2023/214039A1 |
The invention relates to a sensor device (SV1, SV2, SV3) for a transmission of data and/or an evaluation of downlink signals (DL(H1,T1)) transmitted by at least one satellite (S1) for a reconnaissance system (AS), wherein the satellite (...
|
|
WO/2023/215530A1 |
A bridle system and roll control sheave for quickly and accurately directing the roll of an airborne wing in an airborne wind energy system is disclosed. A pair of medial bridle segments are connected to a sheave which is placed within t...
|
|
WO/2023/214348A1 |
Method for identifying malfunction conditions of the sensors that measure the amount of fuel in the tanks of an aircraft (1) provided with at least one first tank (2/6) arranged on a first side of the aircraft and at least one second tan...
|
|
WO/2023/213196A1 |
A forward jet drag reduction and heat shielding method for a hypersonic pointed-cone aircraft. A jet drag reduction and heat shielding system is arranged at a windward wall surface of the aircraft, the jet drag reduction and heat shieldi...
|
|
WO/2023/214943A1 |
This invention relates to the landing gear bracket that can be mounted on the chassis of small and medium-sized flying vehicles, especially helicopters and flying cars, to carry the landing gear, and its feature is; a body (1) produced a...
|
|
WO/2023/215203A1 |
This disclosure relates to improved techniques for upgrading legacy flight management systems (FMSs) installed in an aircraft. In certain embodiments, an integrated guidance system (IGS) can be installed in an aircraft having a legacy FM...
|
|
WO/2023/215459A1 |
In some embodiments, an electric aircraft may include a plurality of flight components including a plurality of control surfaces; a plurality of lift propulsors; at least a thrust propulsor; and a plurality of electric motors configured ...
|
|
WO/2023/214173A1 |
A method for managing a plurality of drone ports is disclosed herein. The method comprises operating a trained machine learning model to control a plurality of drone ports. Each of the plurality of drone ports comprises: a plurality of l...
|
|
WO/2023/209772A1 |
In this delivery system S comprising a UAV 1 and management server 2, the UAV 1 controls at least one among the position and orientation of the UAV 1 such that cargo placed at a release location and a surrounding area of the cargo fall w...
|
|
WO/2023/208722A1 |
An omnidirectionally orientable vehicle comprising a main body, arms extending radially therefrom and orientable propulsion modules. Each propulsion module is coupled to an arm and comprises at least three propulsion units rigidly attach...
|
|
WO/2023/208366A1 |
The invention is notably directed to an aircraft carrier ground vehicle (10), which comprises a chassis (102), a landing platform (104), a coupling mechanism (106), and an actuation mechanism (108). The landing platform is designed to ac...
|
|
WO/2023/210148A1 |
The present invention generates a movement route for a mobile body according to conditions of the mobile body and the status of a movement region. This route generation device stores spatial region data formed from a plurality of spatial...
|
|
WO/2023/209289A1 |
The invention relates to a propeller blade or airfoil (10) for a turboprop engine, made from composite material and comprising a matrix-densified fibrous reinforcement, the propeller blade or airfoil comprising, in a spanwise direction (...
|
|
WO/2023/211307A1 |
The present technical solution relates to computing, and more particularly to automated stock-taking technology. The technical result achieved by the proposed technical solution consists in significantly increasing the speed with which w...
|
|
WO/2023/209612A1 |
A film includes a conductive substrate layer having a conductive trace region, a plurality of nonconductive regions, and a plurality of conductive attachment regions. The film may be applied to a nonconductive support and electrically co...
|
|
WO/2023/210398A1 |
The present invention comprises: a base member 11 to which one ends of springs 13 are connected; and a shaft 12 to which the other ends of the springs 13 are connected and which, when the shaft 12 comes into contact with an object, makes...
|
|
WO/2023/211639A1 |
A hybrid electric vertical takeoff and landing (VTOL) aircraft. The hybrid electric VTOL aircraft generally includes a fuselage, a pair of wings, a pair of booms, a plurality of flight components and a power system. The wings are connect...
|
|
WO/2023/209717A1 |
A system for detecting a state of a mechanism includes processing circuitry. The mechanism includes multiple components, at least some of which are capable of moving relative to each other. At least one state is specified for the mechani...
|
|
WO/2023/209335A1 |
According to an aspect of the present invention, there is provided a control unit in an active inceptor configurable to generate force feedback in a linked active inceptor system, comprising: a first connection configured when an operati...
|
|
WO/2023/208887A1 |
An aeronautical vehicle (1) performs horizontal flight and/or vertical flight, and has a fuselage (2), a wing assembly (3) having a first wing part (3a) and a second wing part (3b) rigidly coupled to one another, a rotor assembly (4), a ...
|
|
WO/2023/206864A1 |
A dynamic take-off and landing device and method for an unmanned aerial vehicle. The dynamic take-off and landing device for an unmanned aerial vehicle is mounted on a carrier base and comprises an attitude adjustment mechanism (1) and a...
|
|
WO/2023/208829A1 |
A propulsion system (1A; 1B), more particularly for an aircraft (2), comprises: a number of rotors (12), which are disposed in at least four sectors (Q1-Q4), each of the rotors (12) being assigned to a pair (P) of rotors (12) which are d...
|
|
WO/2023/209288A1 |
A turbojet engine fan blade or vane (10) made of composite material comprises a fibrous reinforcement densified by a matrix, the fan blade or vane comprising, in the direction of its span (DL), a root (12) and an aerodynamic profile (11)...
|
|
WO/2023/211996A1 |
A UAV including a shroud with cooling openings to cool electronics in the UAV. The shroud includes propeller openings surrounding respective propellers. The propeller openings include intake openings that draw air from outside the shroud...
|
|
WO/2023/209312A1 |
The invention relates to a propeller blade or airfoil (10) for a turboprop engine, made from composite material and comprising a matrix-densified fibrous reinforcement, the propeller blade or airfoil comprising, in a longitudinal directi...
|
|
WO/2023/207169A1 |
A navigation light system, a rotary wing aircraft and a navigation light control system. The navigation light system comprises a left navigation light assembly and a right navigation light assembly, which is opposite the left navigation ...
|
