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WO/2024/009097A1 |
The present invention relates to a propulsion system for providing controllable propulsion comprising: a fuel cell arrangement (210) for generating electrical energy; a gas generator (250) comprising a compressor (256), a combustor (254)...
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WO/2024/009105A2 |
An enclosure is provided which defines an internal volume for housing an electrochemical power unit, wherein at least a region of the enclosure is formed of a material comprising a ceramic matrix composite (CMC). The enclosure disclosed ...
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WO/2024/009024A1 |
The invention relates to a propulsion unit comprising: an electric motor (10), which includes an annular stator (11) about a longitudinal axis (X) and a rotor arranged radially inside the stator (11), so as to be rotated about the longit...
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WO/2024/010967A1 |
The disclosure provides an example charging nest for wireless power transfer to drones is disclosed. The charging nest includes (a) a housing having an opening at a first end, (b) a plurality of antennas arranged around a periphery of th...
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WO/2024/009029A1 |
One aspect of the invention relates to a device for measuring the pitch angle of blades of a turbine engine with a first axis X, comprising: - a movable wheel which is centred on the first axis X and is provided with a plurality of blade...
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WO/2024/010856A1 |
A system for exploring unidentified aerial phenomena (UAP) includes a processor and a memory. The memory includes instructions stored thereon, which, when executed by the processor, cause the system to: access a UAP dataset comprising re...
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WO/2024/009090A1 |
The present invention relates to an aircraft propulsion system (100) comprising: a fuel cell arrangement comprising at least one fuel cell (110); an air source (130) for providing air to the fuel cell arrangement; a compressor arrangemen...
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WO/2024/007061A1 |
The inventions will find application in aviation, particularly for passenger and cargo transport, in emergency medical care, etc. The aircraft comprises a frame 2 with casing 3 and at least one engine 4 mounted to the frame 2, and at lea...
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WO/2024/009040A1 |
An assembly for a turbine engine, comprising: a first rotating body (222, 262, 282); a second rotating body (20, 220, 260, 280); and an electrical system (4) comprising: a bus (40); a first generator (411); a second generator (421); a fi...
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WO/2024/007564A1 |
A modular flight automobile, comprising an automobile body and a vehicle-mounted aircraft, wherein the vehicle-mounted aircraft can take off from and land on the automobile body; and the vehicle-mounted aircraft comprises a cockpit, and ...
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WO/2024/009293A1 |
Combined aerospace system is a multi-stage technology to deliver payloads to orbit and to midair. The system comprises a carrier aircraft, a tow aircraft, a towed spaceplane or a rocket plane or a glider. The carrier aircraft, coupled wi...
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WO/2024/010834A1 |
A vertical take-off and landing aircraft with a multi-element lifting system with integrated propulsion. The multi-element lifting system may have an upper wing element, a lower wing element, and a control wing element which is located b...
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WO/2024/008512A1 |
The present disclosure relates to a rotor fan (1) for an airborne vehicle, which comprises several rotor blades (2) arranged rotationally symmetric around a rotor axis (3). Each rotor blade (2) comprises a blade body (4) which is made of...
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WO/2024/009089A1 |
The present invention relates to electrical network comprising an electrical conductor and, a cryogen source configured to hold cryogen, the cryogen source arranged so that, in use, cryogen is provided to the conductor to maintain the co...
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WO/2024/008731A1 |
The invention relates to a payload carrier system for an aircraft, preferably for an unmanned aircraft, the payload carrier system comprising a plurality of carrier units, wherein: each carrier unit has one supporting body and one payloa...
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WO/2024/009298A1 |
A drone related transfer system comprises movably mounted, establishment-mounted and establishment-specific transfer assemblies for facilitating transfer of a package between an establishment interior and a drone, and a monitoring system...
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WO/2024/009443A1 |
A takeoff and landing site monitoring device (30) is configured to comprise: an image data acquisition unit (41) which acquires, from an imaging device (21) for imaging a takeoff and landing site (1), image data that represents an image ...
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WO/2024/009166A1 |
Electronic system for managing emergencies and contingencies occurring in flight infrastructures, characterized in that it comprises the following elements: - a VHF radio (10); - a VHF antenna (20); - two computers (30); - a microprocess...
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WO/2024/010528A1 |
An aerial payload deployment system is provided, including: an aerial vehicle including a flight controller operable to control a flight of the aerial vehicle; and a payload deployment system coupled or couplable to the aerial vehicle an...
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WO/2024/009062A1 |
A drone (10) operable for flight. The drone has a fuselage (100) having a length (L) extending along an x-axis, the fuselage (100) comprising a port side fuselage section (102) spaced apart from a starboard side fuselage section (104) to...
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WO/2024/009028A1 |
The device for charging a battery (15, 16) of an aircraft (1) comprises a reversible electrical power converter (13) comprising a power inlet (132) configured to be connected to the battery (16) and a power outlet (134) configured to be ...
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WO/2024/008750A1 |
An aerodrome structure comprises a vertical airfield module having a primary landing pad for a vertical takeoff and landing aircraft. The primary landing pad is located in an upper plane and comprises an inner platform having an inner pl...
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WO/2024/002772A1 |
A system (1) for thermal regulation of a spacecraft (S), comprising: - a hot source (C) interface, - a radiator (10) having a thermally conductive body (11) comprising at least one radiative surface (12), - two separate single-phase cool...
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WO/2024/003622A1 |
Fire fighting drone comprising an exoskeleton (2) defining an internal space (3) extending along an axis H and a flexible bag (4) stably housed in the internal space (3), provided with a release valve (6) and configured to contain a fire...
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WO/2024/000748A1 |
The present invention provides a lightweight modular general storage platform for an unmanned aerial vehicle, comprising a landing platform, a rotating platform, and a servo control unit. The landing platform is rotatably connected to th...
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WO/2024/006680A1 |
A modular satellite apparatus (10) for testing materials in a space setting is provided. The apparatus (10) includes a lower member (101) and an upper member (102), as well as rear support members (103), medial support members (104), fro...
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WO/2024/005984A1 |
An inert blanket system includes a reformer (128) that produces hydrogen gas (130) and carbon dioxide (135). The hydrogen gas (130) is separated from the carbon dioxide (135). The carbon dioxide (135) is ported to a vapor region (122) of...
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WO/2024/006087A1 |
A pulsar-based timing and lateration system includes a detector system. In according with certain embodiments, the detector system includes a plurality of detectors, each one configured for detecting X-ray photons and generating output s...
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WO/2024/006584A2 |
An adaptive duct fan propulsion device includes a nacelle body defining a pathway for air to flow through the nacelle body along a longitudinal axis of the nacelle body; a plurality of primary slats defining a variable geometry inlet duc...
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WO/2024/004158A1 |
Provided is an unmanned aircraft that has horizontal wings and that is compact overall. An unmanned aircraft 100 comprises: an unmanned aircraft body 101; a plurality of rotors 104A, 104B and 104C which each have a rotary shaft extendi...
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WO/2024/004443A1 |
A locking device (100) can transition between a locked state and an unlocked state. The locking device (100) comprises a lock pin (101), a solenoid (110), and a pressing unit (120). The lock pin (101) can be moved between a locked positi...
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WO/2024/003620A1 |
A drone is disclosed having a low acoustic signature. The drone includes a fuselage, a main inboard wing attached to the fuselage, a pylon located towards an aft end of the fuselage and having an end that is higher than the main inboard ...
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WO/2024/006170A2 |
A propulsion system includes a first plurality of rotor blades configured to rotate about an engine longitudinal axis and a motor module. The motor module includes a plurality of electric motors for rotating the first plurality of rotor ...
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WO/2024/003527A1 |
The disclosure concerns an unmanned aircraft for carrying of cargo, comprising a fuselage (10) extending in a fore-aft direction and configured to receive cargo in an unpressurized interior space thereof; a wing (20) extending in a spanw...
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WO/2024/004402A1 |
This propulsion device (15) has a propeller (20) and an EPU (50). The EPU (50) has a motor device (60) and an inverter device (80). The motor device (60) has a motor (61) and a motor housing (70). The inverter device (80) has an inverter...
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WO/2024/004442A1 |
An EPU (50) has a first DS (100) and a second DS (110). The first DS (100) has a first motor (61) and a first inverter control unit (81). The second DS (110) has a second motor (71) and a second inverter control unit (91). The first moto...
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WO/2024/003005A1 |
The invention relates to a ground power unit (10) for supplying an aircraft (20) with power via a first power supply output (140), which ground power unit comprises an electrical connection (135) connecting the output of a DC-to-AC conve...
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WO/2024/004301A1 |
The purpose of the present invention is to provide a panel member that is lightweight and has high strength with respect to an impact from the outside. This panel member (100) comprises a first skin member (1) and a second skin member ...
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WO/2024/000855A1 |
A gyroscope assembly, a turbine blade, an impeller, and a wind power generator set. The turbine blade comprises a blade body (10), a web (11), and a gyroscope assembly. The blade body (10) has an inner cavity; the web (11) is fixedly dis...
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WO/2024/005359A1 |
The present invention relates to a method and system for VR-based drone practical test evaluation using real time kinematic GPS (RTK GPS), wherein the location and orientation of a drone are measured using RTK GPS, and the trajectory of ...
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WO/2024/006372A1 |
Methods (700, 750, 780) and systems (100) for inspecting a product (214), such as a wire harness, including product features for inspection. A camera (204) of an inspection station (104) may capture a product image. A machine learning (M...
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WO/2024/004355A1 |
This heat control structure comprises: a plurality of sheet-like or plate-like graphite members; a first holding member that holds the plurality of graphite members at a first end portion in the longitudinal direction of the plurality of...
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WO/2024/001143A1 |
A ducted fan (2), an aircraft and an attitude control method and system therefor, and a related apparatus. The ducted fan (2) comprises: a first ducted fan unit (201) comprising a first fan assembly (21) and a first duct (22), which is a...
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WO/2024/003902A1 |
An air intake module for a projectile includes a module forward end (MFE), a module aft end (MAE), and an aft facing intake cone arrangement (AFICA). The air intake module is configured for connection to the forward portion and the propu...
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WO/2024/003013A1 |
The invention relates to a satellite comprising: a satellite body including at least one radiative surface configured to emit satellite heat to space; and an attitude determination and control 'ADCS' system for controlling an orientation...
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WO/2024/001980A1 |
Provided is a glass stacking and a preparation process thereof, comprising: a glass substrate; a low-emissivity layer; and an overcoat layer; wherein the low-emissivity layer is between the glass substrate and the overcoat layer; the low...
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WO/2024/004162A1 |
Provided is an unmanned aerial vehicle that can ensure the stability of communication with a piloting apparatus. An unmanned aerial vehicle 1 comprising: an antenna 115 for communicating with a piloting apparatus that pilots the unmanned...
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WO/2024/006164A1 |
An aircraft has a boom, a propulsion assembly coupled to a first end of the boom, and a first wing coupled to a second end of the boom. The first wing can be coupled to the boom by a (first) articulated joint. The propulsion assembly can...
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WO/2024/003642A1 |
A ducted wing is configured to be connected to an aircraft. The ducted wing includes an array of integrated jetfoils. Each jetfoil includes a propulsor fan, an upper wing portion, and a lower wing portion that extends past an end of the ...
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WO/2023/229923A9 |
A radio communication system includes non-orbiting aerial nodes providing a radio route between terrestrial nodes. The non-orbiting nodes have a plurality of directional antennas pointing horizontally in multiple directions for sending r...
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