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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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WO/2024/001445A1 |
Disclosed in the present application are a helicopter platform profile structure and a platform fire-fighting system thereof, belonging to the technical field of ship and marine engineering helicopter platforms. The helicopter platform p...
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WO/2024/000024A1 |
A method of controlling an internal combustion engine of a UAV (100) where the engine (102) has a fuel delivery means (123) operable to deliver a fuel to a combustion chamber of the engine (102). The method comprises controlling the engi...
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WO/2024/000009A1 |
Some embodiments relate to a control device for a pilot valve of a pit valve. The device includes: a housing; an air inlet coupling, configured to receive pressurized air from a pressurized air supply; an outlet coupling, configured to s...
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WO/2024/006730A1 |
Dynamic ram accelerator operation permits operation with lower acceleration, permitting launch of acceleration sensitive payloads such as crewed vehicles. Operational cost is reduced, and reliability improved, by reducing or eliminating ...
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WO/2024/006078A1 |
Systems and methods for protecting an aerodynamic structure, e.g., a wind turbine blade, rotor blade, aerodynamic aerostructure, etc., are provided. Long fiber reinforced composites having a helicoidal architecture with material aligned ...
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WO/2024/006322A1 |
A flight vehicle includes a frame, a propulsion system coupled to the frame, a first source of power coupled to the frame and configured to power the propulsion system, a traction wheel coupled to the frame and configured for tractional ...
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WO/2024/005705A1 |
A double bed compartment (5) for an aircraft cabin (3) and an aircraft cabin that comprises the double bed compartment are also disclosed. The double bed compartment has two passenger doorways (9) and two passenger chairs (31) positioned...
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WO/2024/004315A1 |
Provided is a heat control structure comprising a heat-insulating material, which is disposed between a housing that accommodates a heat control installed in a satellite and the heat control subject, wherein the heat-insulating material ...
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WO/2024/003483A1 |
The invention relates to improving the propulsion of a HET, RIT or GIT engine during solar eclipses and comprises, before the solar eclipse: deactivating the thrust and then disconnecting the bus supplied with power by the solar panel (T...
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WO/2024/006171A1 |
An aircraft has a fuselage, a propulsion system, and a vacuum control system. The vacuum control system includes a conduit having an inlet configured to receive exhaust air from the propulsion system. The conduit can be configured to dir...
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WO/2024/006465A1 |
A fixed lighting assembly that is able to change between configurations, including from a floodlight to a spotlight and any configuration in between, allows for a substantial improvement in performance and safety of a vehicle. Additional...
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WO/2024/005248A1 |
The present invention relates to a duct with improved crosswind stability, in which when crosswinds occur, deterioration in operating characteristics by the separation of airflow is minimized and, more specifically, to a duct mounted to ...
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WO/2023/249723A1 |
Disclosed herein is an unmanned aerial vehicle (UAV) for facilitating aerial deliveries of cargo. Accordingly, the UAV may include a body defining a receptacle with a receptacle opening within the body. Further, the UAV may include a pro...
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WO/2023/246948A1 |
A new foldable convenient manned aircraft comprises a fuselage, four arms arranged on the fuselage, a rotor motor, a rotor and an anti-collision radar which are symmetrically arranged on the outer end of each arm, four anti-collision air...
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WO/2023/247869A1 |
The invention relates to a method for manufacturing a fibre preform for a part, comprising: - weaving a first core texture of elongate shape extending in a longitudinal direction and comprising, in cross section, a central portion (10) h...
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WO/2023/247334A1 |
The invention relates to an electrical distribution system (1) configured to supply power to at least a first electric motor (M1) and a second electric motor (M2) from at least a first electrical source (B1) and a second electrical sourc...
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WO/2023/249652A1 |
A peripheral propulsion system having a propulsion unit (3), an upper section (36), and a lower section (37). The propulsion unit (3) has a motor (31), a motor engagement section (34), an extension (32) coupled to the motor engagement se...
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WO/2023/248982A1 |
[Problem] To enable the number of mobile bodies to be changed while transport of a payload is in progress. [Solution] An information processing method according to the present disclosure: acquires information representing the operating s...
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WO/2023/249573A1 |
The invention is related to the radiation-proof radiation barrier, which aims to reduce the radiation that may emanate from the Sun by being inserted between the Sun and the Mars, as well as aiming to achieve a healthier life with the mo...
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WO/2023/250214A1 |
Embodiments are directed to an anti-rattle device, including a plurality of handle bracket assemblies, and a wedge assembly. Each of the handle bracket assemblies includes an adjustable handle, a bracket, and a threaded rod. The wedge as...
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WO/2023/247982A1 |
The smart drone system (100) for simulating a moving object comprises at least one drone (200) comprising (a) a stabilizing unit (210), a projection unit (220), an analytical unit (230) for processing and evaluating motion information of...
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WO/2023/248121A1 |
A vertical take-off and landing aircraft of the tail-sitting type comprises a cockpit integrated into a body having delta wings in the rear section with respect to the cockpit and a propulsion system placed in the front section with resp...
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WO/2023/247907A1 |
The invention relates to a pitch-change mechanism (70) which comprises a frame (72), a moving part (102) which can be translated along a longitudinal axis (X), and a locking device (160). The locking device (160) comprises a support memb...
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WO/2023/246424A1 |
An electrically controlled variable pitch propeller, and a multirotor and a control method therefor. The electrically controlled variable pitch propeller comprises a main shaft (10), a variable pitch blade (20) and a brake module (30), w...
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WO/2023/247868A1 |
The present invention relates to a fibrous preform (1) of a core part of a fibrous reinforcement for a part made of composite material, the preform having a slender shape along a longitudinal direction (X) and being formed by three-dimen...
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