| Document |
Document Title |
|
WO/2023/281309A1 |
A scanning camera includes a camera assembly associated with curved scan paths. Each camera assembly includes an image sensor and a lens, and has a camera optical axis. Also included are a scanning mirror, and a drive to rotate the scann...
|
|
WO/2023/280903A1 |
The present invention relates to a rotor (1, 1', 1'', 1''', 1'''', 1''''') for helicopter comprising a shaft (2) adapted to be put into rotation by at least one engine element, a hub (3) splined to the shaft (2), at least four blades (4)...
|
|
WO/2023/282949A2 |
Methods, devices, and systems are described for a core of a space habitat. The core includes a plurality of internal beams extending a length of the core. The core also includes a plurality of end rings at a first end of the core and a s...
|
|
WO/2023/281179A1 |
The invention relates to an electrical architecture (2) for an aircraft, comprising: - a first propulsion power distribution network (16) distributing a high DC voltage, - a second propulsion power distribution network (18) distributing ...
|
|
WO/2023/282402A1 |
A drone station according to an embodiment of the present invention may comprise: a station main body (10) having, mounted thereon, a charging device (20) allowing a drone to land thereon so as to be charged with drone power; a cover (30...
|
|
WO/2023/281210A1 |
The invention relates to an electrical architecture for a hybrid thermal/electric aircraft, comprising the following for each turboshaft engine: - an AC aeroplane electrical system (120); - at least one first electrical machine (HPMG1, H...
|
|
WO/2023/281180A1 |
The invention relates to a three-dimensional electroconductive mat formed of an electroconductive knitted fabric capable of homogeneously distributing electrical charges over the entire surface thereof, characterised in that the knitted ...
|
|
WO/2023/282948A2 |
Methods, devices, and systems are described for a bracket fixture for securing a load to a soft goods layer in a space habitat. The bracket fixture includes a base having a plurality of sides, the plurality of sides having a pin parallel...
|
|
WO/2023/281193A1 |
The invention relates to an aeronautical thruster (10) having a longitudinal axis (X) and comprising a hub (12), an upstream annular row (14) and a downstream annular row (16) spaced apart from one another along said longitudinal axis (X...
|
|
WO/2023/280457A1 |
An electronic device comprises a sensor arrangement, a control system operable to obtain sensor data from the sensor arrangement, and a microphone configured to provide an audio signal representing sound waves received by the microphone....
|
|
WO/2023/279630A1 |
An automatic recovery charger nest for a vertical take-off and landing fixed-wing unmanned aerial vehicle, comprising a cabin body (1) and a top cover (2) which can open and close and which is mounted at the top part of the cabin body (1...
|
|
WO/2023/276031A1 |
[Problem] To provide a new technology for utilizing formation flight of a plurality of artificial satellites having light sources in the entertainment field. [Solution] The present invention is an artificial satellite control device whic...
|
|
WO/2023/276030A1 |
[Problem] To provide a novel technology that uses flight by a plurality of satellites that each have a light source for entertainment. [Solution] The present invention is an artificial satellite control device that controls the plurality...
|
|
WO/2023/278005A1 |
Methods, devices, and systems are described for a mounting flange and bracket for a space habitat. The bracket system couples a bladder of a space habitat to a cylindrical core. The bracket system includes a soft goods layer configured t...
|
|
WO/2023/277720A1 |
A nuclear-powered ground-effect aircraft carrier is capable of travelling above the surface of water at a maximum speed of up to 550-600 km/h and has a twin-hulled catamaran design. Disposed between the hulls is a large wing, the aircraf...
|
|
WO/2023/274721A1 |
The invention relates to a method for protecting an object (2), in particular a land vehicle or watercraft, in particular a ship, from a radar-guided missile (4), by deploying and using an active offboard reflector (8), which is arranged...
|
|
WO/2023/275516A1 |
According to the present disclosure there is provided a duct arrangement for influencing fluid flow, the duct arrangement comprising: a duct section arranged to receive a fluid flow therethrough, the duct section defining a first directi...
|
|
WO/2023/276029A1 |
[Problem] To provide a new technology for utilizing formation flight of a plurality of artificial satellites having light sources in the entertainment field. [Solution] The present invention provides a content provision device which prov...
|
|
WO/2023/275686A1 |
An aircraft loader (100) comprises a chassis (124), a cab (128), a loading floor (144) and a load lifting apparatus (110). The load lifting apparatus (110) includes a frame (112), a first horizontal platform (114) and a second horizontal...
|
|
WO/2023/272489A1 |
A propeller and an unmanned aerial vehicle. The propeller comprises: a hub (10); blades (20) connected to the hub (10), the blades (20) each comprising a connecting end connected to the hub (10), and a tail end distant from the hub (10);...
|
|
WO/2023/275970A1 |
[Problem] To provide a novel and improved information processing device, an information processing method, and a program, which are capable of improving robustness of a camera with regard to rotation, when identifying stars corresponding...
|
|
WO/2023/275535A1 |
A passenger cubical assembly comprising: a door; a door support assembly having a sliding mechanism, the sliding mechanism arranged to support the door such that the door is translatable relative to the door support assembly along a firs...
|
|
WO/2023/275808A1 |
A compact directed energy system is disclosed that is configured to generate directed energy beams. The compact directed energy system includes a radio frequency system configured to provide a directed energy beam in a frequency range be...
|
|
WO/2023/275474A1 |
The invention relates to a locking system (801) for an aircraft nacelle comprising a first portion (803), intended to be mounted on a first part (703) of an aircraft nacelle, and a second portion (809), intended to be mounted on a second...
|
|
WO/2023/277847A1 |
The present invention relates to a console (C) provided in air vehicles; at least one control stick (2) located on the console (C), providing mission input to the air vehicle by the user; at least one bracket (3) allowing the control sti...
|
|
WO/2023/272367A1 |
The present invention consists of a device that adds thrust to the blades of rotary-wing aircraft such as helicopters, comprising an air inlet (8) located approximately in the middle of the span of each blade (4), a duct (9) extending fr...
|
|
WO/2023/275836A1 |
Method for manufacturing a core (10) for an aircraft panel (100) with the steps of: arranging first sheet-shaped partitioning elements (12), each with vertical slits (16), extending transversely from a first edge (12a), and transverse sl...
|
|
WO/2023/278001A1 |
A navigation processing system includes at least one processor configured to execute operational instructions that cause the at least one processor to perform operations that include generating navigation data. A data stream is generated...
|
|
WO/2023/275470A1 |
The invention relates to a sealing device (12) composed of a lip seal (20) and a spring (21) or another resilient seal which radially and axially compresses the first seal, forming two sealing lines (25, 25) closed over substantially pla...
|
|
WO/2023/272601A1 |
A damping structure (2), a movable platform, and a load (4) damping method. The damping structure (2) comprises: a first support member (100); a second support member (101), which is spaced apart from the first support member (100); a da...
|
|
WO/2023/275839A1 |
A method for manufacturing a core (10) for a panel (100) for an aircraft comprises the steps of: arranging first sheet-shaped partitioning elements (12), each having a plurality of vertical slits (16) extending transversely from a first ...
|
|
WO/2023/274914A1 |
In order to reduce maintenance work and to improve long-time reliability, the invention provides a health monitoring method for checking a functionality of a flight control surface driving apparatus (104) using at least one load sensor (...
|
|
WO/2023/278690A1 |
An example of a deflected slip stream wing system with coflow jet flow control includes a wingbox, a flap, a compressor, and a propulsor. The wingbox has a root and a tip. The flap is moveably attached to the wingbox and has a leading ed...
|
|
WO/2023/272526A1 |
Disclosed in the embodiments of the present application are a charging base station, a flight vehicle, and a flight vehicle system. The charging base station is used for charging a battery of a flight vehicle, and comprises: a flight-veh...
|
|
WO/2023/272600A1 |
Provided are a take-off and landing platform, an unmanned aerial vehicle, a take-off and landing system, an accommodating device, and a take-off and landing control method. The take-off and landing platform specifically comprises: a supp...
|
|
WO/2023/278262A1 |
Systems and methods are disclosed that address the problem of large-scale optical manufacturing of microstructures. The systems and methods utilize one or more optical processing systems to generate a first set of alignment marks in a fi...
|
|
WO/2023/279032A1 |
Exemplary embodiments include systems and method for making a membrane surface having an axis of revolution using first and second mandrel having precise and accurate working surfaces. The systems and methods may also use gore material t...
|
|
WO/2023/277657A1 |
Disclosed is a transmission line construction method using wire pulling and wire tensioning, by which, after measuring a coordinate point of a power line connection hole of a transmission line tower by using a drone, a power line is cut ...
|
|
WO/2023/275739A1 |
A cover (10) for an opening on the exterior of an aircraft that contains a fire-resistant, high-temperature tolerant foam (14) encased in a cover (11) made of an aramid fabric (12). The cover is friction-fitted to the interior of the ori...
|
|
WO/2023/274337A1 |
Disclosed in the present utility model is a photographing support, comprising a fixing portion, a mounting portion and a photographing device, wherein the fixing portion is used for fixing the photographing support to another object; the...
|
|
WO/2023/277723A1 |
The claimed invention relates to aviation and concerns command posts for manually controlling an aircraft, in particular a single-rotor helicopter. In one of the possible design embodiments, the invention is envisaged as follows. A yoke ...
|
|
WO/2023/276033A1 |
[Problem] To provide a novel technology which utilizes, in the entertainment field, flight control by a plurality of artificial satellites having a light source. [Solution] The present invention is an artificial satellite control system ...
|
|
WO/2023/274913A1 |
In order to reduce maintenance work and to improve long-time reliability, the invention provides a health monitoring method for checking a functionality of a flight control surface driving apparatus (104) using at least one load sensor (...
|
|
WO/2023/276032A1 |
[Problem] To provide a novel technology that utilizes formation flights by a plurality of satellites with light sources in the entertainment field. [Solution] The present invention is a satellite control device that controls a plurality ...
|
|
WO/2023/276028A1 |
[Problem] To provide a novel entertainment application for flight control of a plurality of artificial satellites that have a light source. [Solution] The present invention is an artificial satellite control device that controls a plural...
|
|
WO/2023/276640A1 |
Provided is a flying object control system comprising an area-forming part that forms a prescribed area relative to a grip, a detection unit that detects a displacement of the prescribed area formed by the area-forming part, and a contro...
|
|
WO/2023/275454A1 |
The invention relates to a method (200) for controlling a system for generating and controlling power in an aircraft comprising: - a hybrid propulsion system comprising an electrical network and a propulsion-energy source; - at least one...
|
|
WO/2023/275838A1 |
A method for manufacturing a core (10) for a panel (100) for an aircraft comprises the steps of: arranging a plurality of first sheet- shaped partitioning elements (12), each having a plurality of vertical slits (16) extending transverse...
|
|
WO/2023/275466A1 |
The present invention relates to an assembly (10) for a propeller of a turbine engine of an aircraft, the assembly comprising: - a variable-pitch vane (2) comprising a blade connected to a root, the vane (2) comprising a longitudinal axi...
|
|
WO/2023/274917A1 |
An aircraft landing gear assembly (50, 80) comprising: a first landing gear element (60) movably coupled relative to a second landing gear element (62) to pivot about a pivot axis (PA) between a first condition and a second condition; a ...
|
