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WO/2020/229750A1 |
The invention relates to an unmanned aerial vehicle (10) comprising an autonomous power supply source (12), a housing (14), in the internal volume of which is arranged electronic equipment which is electrically powered by the power sourc...
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WO/2020/230614A1 |
The present invention prevents a flying body from being detached and falling from a parachute device in which a parachute can be forcibly open by injecting the flying body. This parachute device (4) is characterized by comprising: a pa...
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WO/2020/185274A3 |
A hybrid electric engine control module (ECU) configured to be operatively connected to a hybrid electric aircraft powerplant having a heat engine system and an electric motor system to control a torque output from each of the heat engin...
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WO/2020/193411A3 |
The present invention relates in one aspect to a cushion for an aircraft seat comprising at least one upholstered element having an upper side and a lower side composed of plastic foam; at least one sensor system, wherein the at least on...
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WO/2020/208265A3 |
Aspects of the present invention relate to an aerial firefighting system for a helicopter, the firefighting system comprising: an external reservoir for storing water, wherein the reservoir comprises a water outlet; a supporting frame co...
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WO/2020/231591A1 |
Techniques are provided to improve routing of autonomous vehicles through highly congested areas. In some embodiments, routes that include sequences of timed space reservations are provided to autonomous vehicles by a route reservation s...
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WO/2020/231520A1 |
Embodiments of the present disclosure generally relate to protective coatings on an aerospace component and methods for depositing the protective coatings. The protective coating can be anti-coking coatings to reduce or suppress coke for...
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WO/2020/227837A1 |
An electric propulsion system for an aircraft includes a nacelle and an electric machine. The electric machine includes a stator positioned in the nacelle, and a rotor and fan assembly positioned in a primary flow path through the nacell...
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WO/2020/232352A1 |
Embodiments of the present disclosure are directed to systems and methods for autonomously performing and/or facilitating drone diagnostic functions. Prior to a mission of a UAV, an inspection station comprising at least one imaging sens...
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WO/2020/229020A1 |
Disclosed is an industrial truck comprising opposing masts for lifting and lowering a loading platform (11) located between the masts in a lifting and lowering direction, and comprising a chassis (1) that includes two lateral sections (3...
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WO/2020/232388A1 |
An array of antenna assemblies each generate solar power and utilize the generated solar power at that antenna assembly, which enables large amounts of power to be generated. An antenna assembly having a flat antenna layer forming a firs...
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WO/2020/229018A1 |
In an industrial truck (100) comprising opposing lifting masts (9, 10) and a loading platform (11) located between same, each of the lifting masts (9, 10) comprises at least two guide profiles (25, 26), each guide profile (25, 26) has an...
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WO/2020/229778A1 |
The present intention relates to a method for resetting the static pressure model (mod_Ps3(PCN25R)), called "Ps3 model", upstream of a combustion chamber in a turbine engine comprising a compressor (3), the Ps3 model being used to arbitr...
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WO/2020/229751A1 |
The invention relates to an unmanned aerial vehicle, comprising an autonomous power supply source (44), a central housing (14), in the internal volume of which is arranged electronic equipment electrically powered by the power source and...
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WO/2020/232386A1 |
An antenna array has a plurality of square or rectangular antenna assemblies. Each assembly includes a first antenna assembly surface with a solar cell and a second antenna assembly with one or more antenna elements. The antenna assembli...
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WO/2020/232337A1 |
A wafer-scale satellite bus and a manner of making the same include using wafer reconstruction techniques to stack functional diced circuits onto each other and bond them. The disclosed techniques allow for a variety of functions in each...
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WO/2020/231468A1 |
An apparatus includes multiple layers (102, 302) of phase-stable material, where adjacent layers of the phase-stable material are separated by multiple spaces (104, 304). The apparatus also includes liquid phase change material (106, 306...
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WO/2020/229236A1 |
A thermally insulated container for storing and serving frozen confectionery items, wherein the container is preferably arranged to be removably mounted within a service cart, such as an inflight service cart.
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WO/2020/231244A1 |
The invention relates to oscillating propulsors. A parallelogrammatic oscillating foil mechanism comprises a foil, a drive shaft with a crank attached thereto for translational movement of the foil, said shaft having a kinematic link to ...
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WO/2020/228281A1 |
Provided is an ice crystal detector, comprising an axially extending ice crystal collection probe and a detection device. The ice crystal collection probe comprises a windward surface on one side and a leeward surface opposite to the win...
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WO/2020/226591A1 |
The invention relates to an electrically driven mobile power and ground platform for UAVs (1) with cable connection. The platform comprises electrically driven wheels (10) at the bottom, a chassis (2) which forms the main frame at the mi...
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WO/2020/225307A1 |
A dispenser unit (1) for dispensing biological material, e.g. larvae or insects etc. The dispenser unit has a rotary arrangement (2) with a drive shaft (3) and a plurality of protruding vanes (4) positioned inside a housing (10) for enca...
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WO/2020/227694A1 |
People and packages are delivered to and picked up from delivery locations by autonomous vehicles that also carry autonomous robots. When a package needs to be picked up or delivered at a particular location, an autonomous robot is deplo...
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WO/2020/226708A2 |
An aircraft includes a fuselage and at least one primary wing having an upper surface, at least one recess in the upper surface and at least one conduit in fluid communication with the at least one recess. At least one ejector is dispose...
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WO/2020/225563A1 |
An acoustic panel for an aircraft comprising: a sound attenuating sheet comprising a plurality of cavities, a sound attenuating sheet having a first surface, a second surface opposite to the first surface and an end surface connecting th...
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WO/2020/225305A1 |
The present invention relates to a force application device for a control stick of an aircraft, wherein the control stick comprises a control lever (1) rotating a shaft (A1) about a first axis (A), the device comprising a magnetic brake ...
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WO/2020/188200A3 |
The invention relates to a nacelle (10A) for an aircraft bypass turbomachine (100), comprising: •an annular envelope (11) extending about a longitudinal axis (104), • a thrust reverser (13) comprising: • an annular movable cowl (14...
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WO/2020/224793A1 |
The invention relates to a closing device for an on-board device (1) having a structure (2) and a door (10), which can be moved, preferably pivoted, relative to the structure, the closing device comprising: - a locking mechanism (30), wh...
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WO/2020/190344A3 |
A hybrid propulsion system includes a heat engine configured to drive a heat engine shaft An electric motor is configured to drive an electric motor shaft. A transmission system includes at least one gearbox. The transmission system is c...
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WO/2020/209915A3 |
The present disclosure provides systems and methods for delivery using unmanned aerial vehicles (UAVs). In an aspect, the present disclosure provides an unmanned aircraft system, comprising: a communications unit; and a UAV comprising: a...
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WO/2020/226239A1 |
Disclosed is a low-altitude unmanned aerial vehicle surveillance system. According to an embodiment, the low-altitude unmanned aerial vehicle surveillance system comprises: a balloon body which stays in the air and is filled with gas; a ...
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WO/2020/225979A1 |
An information processing device according to one aspect of the present technique comprises an acquisition unit, an image generation unit, and a presentation unit. The acquisition unit acquires image data related to a predetermined regio...
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WO/2020/139188A8 |
An ion thruster (1, 1a) and a method for providing trust is disclosed. The ion thruster (1, 1a) comprises a first electrode (3, 3a), magnetic field generating device (2, 2a) providing a magnetic trap zone (MT) at the first electrode, and...
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WO/2020/225510A1 |
The invention relates to a hybrid propulsion system (10) for a vertical take-off and landing (VTOL) aircraft comprising at least one combustion engine (120, 140) driving an electricity generator (122, 142), at least one electrical energy...
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WO/2020/224871A1 |
An aircraft (100) with a rotary wing (40) is equipped with a propulsion system (10). The aircraft (100) includes a rotating mast (50) that rotates the rotor wing (40). The propulsion system (10) includes a pole (20) mechanically connecte...
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WO/2020/227247A1 |
An unmanned vehicle control system is disclosed, comprising a ground control station in operable communication with a plurality of unmanned vehicles via a communications network. The ground control station receives unmanned vehicle missi...
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WO/2020/225397A1 |
Noise-attenuating devices, such as acoustic liners, and associated methods of manufacture are disclosed herein. The noise-attenuating devices have a perforated facing sheet with a coating applied thereto. The coating defines an exposed s...
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WO/2020/225815A1 |
A vehicle adapted to travel on a road and to fly in the air comprises a vehicle fuselage, right and left foldable and deployable wings where each of the wings comprises two folding mechanisms and one tillable ducted fan. The vehicle also...
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WO/2020/226988A1 |
A method is provided for realigning or relieving mechanical stress in a spacecraft frame. The process includes providing a spacecraft which includes at least two frame subsections connected by a mechanical connector. The mechanical conne...
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WO/2020/225518A1 |
Apparatus is provided, and method of communicating between drones. Two drones are provided, a remote drone able to perform predetermined stored gestures and a local drone having a sensor to detect such gestures (e.g. a camera) and determ...
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WO/2020/226719A1 |
A vehicle architecture and the associated method of operation for fixed wing aircraft transition from operation underwater to flight in air. More particularly, the vehicle architecture and method allow transition and long-range operation...
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WO/2020/223246A1 |
An aircraft that includes a fuselage that includes a cabin interior that is at least partially defined by a floor, a ceiling and first and second side walls, a cockpit, a forward passenger zone positioned aft of the cockpit that includes...
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WO/2020/149801A3 |
This invention is related to the bag drop system developed in order to provide bag drop process at the passenger terminals of the airports in a practical and fast way without having to make any changes to the existing counter system at t...
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WO/2020/220202A1 |
Disclosed are a quick-release connecting assembly (100), an airscrew (200), a power device (300), a power assembly and an unmanned aerial vehicle (1000). The quick-release connecting assembly (100) comprises a first connecting member (10...
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WO/2020/220654A1 |
A maritime patrol device employing unmanned ship carrying unmanned aerial vehicle and method of use. The patrol device comprises an unmanned ship, an unmanned aerial vehicle, an unmanned aerial vehicle landing platform system, and an aut...
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WO/2020/180376A3 |
An aircraft includes a fuselage defining a longitudinal axis between a forward end and a aft end. At least one airfoil is laterally extending from the fuselage defining an airfoil axis. An electrical system has an electric storage. The e...
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WO/2020/221692A1 |
A leading-edge component (2, 31, 37) for an aircraft (44) is shown, comprising at least a part of a flow body (4) having a front skin (6) and a rib (8), wherein front skin comprises a top section (10), a bottom section (12) and a leading...
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WO/2020/222250A1 |
The invention relates to a dynamic wing assembly system for the re-entry vehicles comprising four cup-type oval shaped wings (33, 34, 35, 36) attached to the body of the re-entry vehicle by a movable connecting means; four inertial senso...
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WO/2020/222836A1 |
A circuit for igniting and sustaining an electron discharge includes an ignitor circuit. The igniter circuit includes a high voltage transformer and a switch connected in series between a primary of the transformer and a DC source return...
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WO/2020/222634A1 |
The present invention describes a rotary wing that provides lift to an aircraft and that is propelled by autorotation. It is a naturally stable rotary wing, since it does not generate torque, and is very safe because it uses autorotation...
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