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WO/2024/082667A1 |
The present invention relates to the field of airport towbarless tractors. Disclosed is a green intelligent comprehensive-energy-supply towbarless tractor, comprising a chassis unit, which comprises a vehicle control unit, a power supply...
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WO/2024/084490A1 |
The present invention "ERASS" provides an Unmanned Aerial Vehicle (UAV) based lifesaving vests/buoy and/or lifesaving kits dropping system. The UAV lifesaving kits dropping device comprises of a lifesaving kit which provides the connecti...
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WO/2024/084297A1 |
Apparatus for installing equipment at a remote location includes a gripper that is releasably coupled to a controller. The gripper includes a first grip member and a second grip member. The second grip member is pivotally joined to the f...
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WO/2024/084029A1 |
The invention relates to a method for destroying a satellite (10) comprising cycles (2000) of updating an onboard memory (11) when the satellite is in outer space (100). Each update cycle comprises receiving, by a communication device (1...
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WO/2024/084953A1 |
The present disclosure relates to an information processing device, an information processing method, and a program with which improved sound collection can be achieved. An information acquisition unit acquires information necessary for ...
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WO/2024/083722A1 |
An aircraft engine seal apparatus has an inflatable seal with a front wall (3, 803, 1103) a rear wall (9, 840) and a side wall (4, 804) forming a rim for pressing and sealing against an internal surface of an engine intake. There is at l...
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WO/2024/085765A1 |
Disclosed is a system and a method for projecting a solution onto a facade of a structure. The system comprises: a pump for pumping the solution; a tool for projecting the pumped solution onto the facade; a hose for connecting the pump t...
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WO/2024/082001A1 |
An embodiment provides a protective suit system that is configured for protecting an occupant in extreme environments. The system may comprise a base layer to be worn on the occupant that is configured for thermal regulation of the occup...
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WO/2024/084781A1 |
At the destination of a drone (10), a detection unit (12) detects a landing-possible area and a landing-impossible area for the drone (10). A safety level specifying unit (13) specifies one of a plurality of safety levels at the time of ...
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WO/2024/082833A1 |
A multirotor electric-manned aerial vehicle, comprising: a cabin (1) for carrying people; multiple rotor support arms (2), wherein each rotor support arm has one end fixedly connected to the top of the cabin by means of a central connect...
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WO/2024/085438A1 |
The present invention relates to a reverse propulsion overtilting tiltrotor drone, which is an unmanned aerial vehicle, consisting of: a main body (10); wings (20) extending from both sides of the main body (10); a tilt rotor (30) provid...
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WO/2024/083876A1 |
The present invention relates to an aerostat of the type comprising a lift enclosure (1), filled with gaseous dihydrogen, electric propulsion means allowing the propulsion of the aerostat and means for supplying electricity to the propul...
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WO/2024/083452A1 |
The invention relates to a method for taxiing an aircraft while anticipating an inability of a drive member equipping at least one wheel (RA) borne by a landing gear (AA) of the aircraft (A) to move said aircraft on the ground, the metho...
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WO/2024/084156A1 |
The present disclosure relates to an assembly for an aircraft comprising: a compensator (5) comprising: a chassis (50) intended to be fixedly mounted on a cell of the aircraft; and an actuator (52) movably mounted on the chassis (50); a ...
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WO/2024/084222A1 |
The present invention concerns a system for positioning an airborne vehicle (502) at a geographic location, the system comprising the airborne vehicle (502) having one or more infra-red ( I R) detectors, and a positioning beacon (504) lo...
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WO/2024/083756A1 |
The present invention relates to a crash handling system (10) for an aircraft, comprising an altitude surveillance system (20), which is adapted to receive altitude data from at least one altitude sensor (22) and to issue an altitude war...
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WO/2024/082392A1 |
A method and system for actively controlling the center of gravity of an aircraft, the method comprising: before an aircraft takes off, acquiring heading centers of gravity of a rear water tank (01) and a front water tank (02) on the air...
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WO/2024/084523A1 |
This invention is designed to solve the problem of drone and helicopter landing in uneven and sloping areas and landing on the variable deck slope during a storm, which is very difficult or even impossible for a helicopter with a simple ...
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WO/2024/084009A1 |
A gap cover (3) for a device component (1), preferably for a cabin attendant seat, for visually closing a gap (2) relative to a further cabin component (6) in a passenger cabin (7) is provided. The gap cover (3) has at least one covering...
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WO/2024/082367A1 |
An airborne real-time three-dimensional imaging radar, and an aircraft. The radar comprises: double antennas (2), which are used for acquiring observation signals from an observation area; a signal transceiver, which is used for transcei...
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WO/2024/086324A1 |
The disclosed embodiments are directed to an eVTOL aircraft comprising a fuselage, wings mounted to the fuselage, where the wings comprise an undercambered lower surface, and an array of ducted fans mounted to the undercambered lower sur...
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WO/2024/085793A1 |
Disclosed is the use of an aqueous deicing/anti-icing composition for reducing carbon fibre degradation. Said composition comprises 40-60% by weight of at least one alkali metal carboxylate and 0.1-2.0% by weight of microfibrillated cell...
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WO/2024/085012A1 |
[Problem] To provide a flapping device that is compact and that is capable of providing a large moving force. [Solution] A flapping device 1 comprises blades 2, 2 and a pair of drive units 3, 3 provided to correspond to the blades 2, 2, ...
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WO/2024/085943A1 |
An aircraft has an electric motor to generate thrust and a power electronic module to provide power to the electric motor. The power electronic (PE) module has an output power to fluidly couple the electric motor and the PE module. The a...
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WO/2024/086044A1 |
A seat back assembly for a passenger seat, such as but not limited to an aircraft passenger seat, includes a seat back and a backrest assembly. The backrest assembly includes a backrest and a headrest. The backrest is movable relative to...
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WO/2024/054628A3 |
The operation of multiple unmanned vehicles (UAV) commanded and supported by a manned "Tender" air vehicle carrying a pilot and flight manager(s). The "Tender" is equipped to flexibly and economically monitor and manage multiple diverse ...
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WO/2024/078900A1 |
Locking/unlocking mechanism for controlling the passage of an aircraft door, with lateral escape of the stops, from the closure position to the unlocking position, and vice versa, said mechanism having: - a guide track (29) extending alo...
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WO/2024/079426A1 |
Disclosed is a variable pitch vane for a turbomachine fan comprising a blade (60) and a root (62). The root (62) comprises a bulb (72) and an upright support (74) connecting the bulb (72) to the blade (60), the bulb (72) being connected ...
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WO/2024/080006A1 |
Provided is a system comprising: a plurality of switching units connected in parallel with a bus to which power generation units and loads are connected and each switching between connection and disconnection of battery packs to and from...
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WO/2024/081396A1 |
A system and method for using unrecoverable energy in a battery cell is disclosed in this application. A system includes a battery cell, the battery cell includes an excess amount of cathode or anode that can function as half cells in an...
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WO/2024/080060A1 |
A control device (60) controls flight of an eVTOL comprising: rotating blades (13) which are driven by a drive apparatus (15) and which generate a rotational lifting force; a fixed blade for generating a glide lifting force; and a liftin...
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WO/2024/079769A1 |
The invention which is the subject of the present patent application consists of a hybrid locomotion robotic device (100) for the inspection of plants, particularly but not exclusively oil, chemical or electric power generation plants, s...
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WO/2024/080181A1 |
Provided is a transmission device for an unmanned aerial vehicle, wherein arms that drive propellers can be positioned so as not to interfere with an air cleaner and a radiator. A transmission device for an unmanned aerial vehicle in w...
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WO/2024/077668A1 |
The present invention relates to the technical field of unmanned aerial vehicles. Disclosed are a variable topdressing device based on a six-rotor multispectral unmanned aerial vehicle and a use method therefor. The device comprises: an ...
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WO/2024/079609A1 |
The invention provides a method for the space debris detection, and a system that implements the method, which provides an algorithm for estimating the performance of a network of optical sensors distributed globally in different ground ...
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WO/2024/079265A1 |
The invention relates to a multicopter comprising a plurality of rotor devices (14), a rotor device (14) comprising at least one rotor blade (20) which is rotatable about a rotor blade axis (22). It is proposed that the rotor device (14)...
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WO/2024/079407A1 |
The invention relates to laminated glazing comprising a first outer glass sheet (2) having a thickness of between 0.5 and 5 mm and at least one structural glass sheet (3, 3') bonded in pairs by an intermediate adhesive layer (4, 6), the ...
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WO/2024/078437A1 |
The present disclosure relates to an aircraft seat and an aircraft. The aircraft seat includes: a headrest; a backrest; and a seat plate pivotably mounted to the backrest and configured to be pivotable relative to the backrest from a sea...
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WO/2024/077523A1 |
An unmanned aerial vehicle (100). The unmanned aerial vehicle (100) comprises a vehicle body (10) and vehicle arm assemblies (20), wherein two vehicle arm assemblies (20) are provided, and the two vehicle arm assemblies (20) are symmetri...
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WO/2024/081182A1 |
A fluid flow powered system for generating electrical power including a rotating turbine blade comprising an outer rim, a tension airfoil central hub assembly, tension elements extending between the outer rim and the tension airfoil cent...
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WO/2024/077365A1 |
The present patent application relates to a support ladder (E) for a boarding region or landing structure (A1) of an aircraft (A), such as a helicopter. The ladder (E) comprises an attachment region (1) for attaching a ladder structure (...
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WO/2024/079423A1 |
The invention relates to a lock system (30) for a turbine engine nacelle, comprising: - a support (41) supporting a hook (42); - a three-point lock (51) including a support (52), a yoke (53) and a three-point mechanism (54) hingedly conn...
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WO/2024/081443A1 |
An apparatus for an inertial separation of air in an electric aircraft, wherein the apparatus includes an intake duct configured to intake an airflow, an inertial air separator configured to separate the airflow into a clean airflow and ...
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WO/2024/077308A1 |
A VTOL aircraft includes a plurality of lift propellers configured to rotated by lift motors to provide vertical thrust during takeoff, landing and hovering operations. The lift propellers are configured to generate a cooling airflow to ...
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WO/2024/074662A1 |
The invention relates to a method (100) for producing a spar cap for a rotor blade of a wind turbine, said method comprising the steps of: - Providing (110) a plurality of pultruded planks, said pultruded planks being a thermoplastic com...
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WO/2024/076837A1 |
A method for carrying a payload (150) using a multi-rotor flight vehicle (MRFV) (130), including receiving an indication that the payload (150) is connected to the MRFV (130), receiving an input from the payload (150), determining, from ...
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WO/2024/074775A1 |
The invention relates to a radiant heating device (2) for an aircraft, the device comprising a heating layer (4) provided with at least one anode (6) and at least one cathode (8), a front protective layer (10) and a rear protective layer...
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WO/2024/076290A1 |
A single-wing rotorcraft with multiple flight modes is provided, including: a frame member; a wing member coupled to the frame member; a flap member rotatably coupled to the frame member; a first thrust unit rotatably coupled to the fram...
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WO/2024/076124A1 |
Proposed are a method by which a first device performs wireless communication and an apparatus supporting same. For example, the first device may acquire information related to a PRS configuration. For example, the information related to...
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WO/2024/073807A1 |
A portable power hub comprising a housing comprising one or more batteries for storing energy; one or more photovoltaic arrangements adjustable relative to the housing and electrically connected to the one or more batteries for charging ...
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