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WO/2021/062682A1 |
A camera (100) and a movable platform (1000), the camera (100) comprising a camera body (110), a master control board (120), a functional module (130), and a flexible connecting structure (140), the flexible connecting structure (140) el...
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WO/2021/064573A1 |
The invention relates to an airport vehicle having an anti-collision system and a method for operating the vehicle, where the vehicle comprises a distance sensor, a 3D sensor system comprising two individual 3D sensors, a brake activatio...
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WO/2021/066804A1 |
Described are aircraft seats having a seat bottom coupled to a seat back and a linkage mechanism for reclining the seat. The reclining mechanism includes an actuator coupled to a recline lock linkage. The actuator is movable between posi...
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WO/2021/062455A1 |
The invention relates to a GPU (1) for the provision of electrical energy for aircraft, and to a method for maintaining and operating the GPU according to the invention. The GPU comprises a base, a cable system (4) which is formed in the...
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WO/2021/064499A1 |
A virtualized infrastructure (1200) for guiding delivery drones, a drone delivery method, and a wingless delivery drone (200) are disclosed that includes a container (210) for storing payloads; a plurality of thrust motors (230) arranged...
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WO/2021/065543A1 |
The present disclosure relates to an information processing device, an information processing method, and a program that enable more certain avoidance of collision with an obstacle. An avoidance orbit setting unit sets, on the basis of p...
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WO/2021/066583A1 |
A flight device of the present invention is a flight device having one or more wings on the left and right sides of a fuselage, respectively, to generate a buoyancy force by performing relative motion to the fuselage by means of a drivin...
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WO/2021/064819A1 |
A hybrid system for a UAV having a generator combined with a battery is suited for long-distance commodity delivery work, but often needs an engine shaft-mounted type portable engine starter which includes a starter motor for starting an...
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WO/2021/063842A1 |
The invention relates to a system for updating data for computing devices in an aircraft (10), the computing devices (1401) being likely, during the updating of the computing device data, to affect or not affect the safety of an operator...
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WO/2021/066681A1 |
A rotary-wing aircraft comprises: a fuselage including a rotatable tail boom; a front wing and a rear wing, which are fastened to the fuselage; and propulsion units, each comprising a motor and a propeller, wherein the propulsion units a...
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WO/2021/063457A1 |
The invention relates to a fluid tank for integration into a structure of an unmanned aircraft, comprising a shell having a first axial wall, a second axial wall arranged opposite thereto, an upper face, a lower face, and an enclosed int...
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WO/2021/066800A1 |
A passenger seat assembly can include a seat frame; a seat back supported by the seat frame, comprising a rearward surface, and moveable between a stowed position and a deployed position; and a monitor shroud positioned proximate to the ...
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WO/2021/066666A1 |
The present application relates to an airborne vehicle comprising a towing vehicle and a towed vehicle or person connected to and towed by the towing vehicle through a lightweight construction. The drag of towed vehicle or person creates...
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WO/2021/066792A1 |
Described are torque bearing assemblies for passenger seats. A torque bearing attachment (122, 222, 322, 422) includes an elongated body having a forward edge configured to mate with an aft end (140) of a seat bottom pan (120), and first...
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WO/2021/065734A1 |
The purpose of the present invention is to provide a notification of an appropriate intrusion warning by determining whether debris intrudes into the orbit region of a satellite constellation. A passage determination unit (110) determine...
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WO/2021/064977A1 |
[Problem] To provide a flight route generation method for a flying object, a flying object reservation method, a program, and a management server through which a user selects a suitable flight and creates a flight route only by designati...
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WO/2020/260979A8 |
An anti-torque rotor (4) is described comprising: a mast (6) rotatable about a first axis (A); a plurality of blades (8) hinged on the mast (6) and rotatable about respective second axes (B) to vary the respective angles of attack; a con...
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WO/2021/063752A1 |
The invention concerns a charger (10) for aeronautical maintenance equipment (1), the charger (10) comprising at least one so-called "high-frequency" input electrical connector (110) comprising a plurality of power supply pins capable of...
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WO/2021/063638A1 |
Disclosed is a drive device, in particular for a flying vehicle such as an aircraft or a spacecraft, comprising at least one engine (2) and a device for cooling the engine (2), the device for cooling the engine (2) comprising a cryogenic...
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WO/2021/065821A1 |
An air conditioner control system (1) for controlling an air conditioning device (30) that regulates an indoor temperature is provided with: a flying body (10) which includes a sensor (18) for measuring temperature, and which flies aroun...
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WO/2021/063907A1 |
A packaged bearing unit (12) includes an outer surface for receiving an aircraft landing gear wheel (10) and an inner surface for receiving an axle (14). The unit may comprise first and second spaced-apart sets (18a), b of tapered roller...
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WO/2021/063833A1 |
Disclosed is an aircraft controller (5), aircraft braking system (13) and method for determining braking parameters. The aircraft controller (5) is configured to determine information associated with an aircraft taxiing route associated ...
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WO/2021/064333A1 |
The invention describes a system for controlling the cyclic setting of blades (1) of a turbine engine propeller, the blades (1) being arranged in a plane normal to the axis of rotation (r) of the propeller, the system comprising: - a pla...
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WO/2021/002907A3 |
A piezoelectric ring bender servo valve assembly reduces mechanical wear by removing mechanical components used in prior art servo valves. The assembly does not use torque motor, flapper, and feedback spring. In this manner, no moving pa...
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WO/2021/064475A1 |
The three - phase vehicle, which has been changed into three climatic, terrestrial and sea modes, is applicable in every three phases. because of the special design of wings, the wing of the wing, the design and center of gravity control...
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WO/2021/067573A1 |
An apparatus, system, and method for filtering and assaying a fluid sample are described. In an embodiment, the apparatus includes a filtration unit comprising: a filter bracket shaped to removably couple with a fluid sample cup and a va...
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WO/2021/062817A1 |
A flight control method, an unmanned aerial vehicle (100), and a flight control system. The flight control method comprises: step S201. receiving a hit signal, the hit signal being used for triggering flight of a virtual unmanned aerial ...
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WO/2021/064396A1 |
A thermal management system is provided for managing the temperature of one or more components in an aircraft nacelle. The thermal management system comprises an inlet opening into the nacelle, an outlet opening out of the nacelle, a gas...
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WO/2021/067903A1 |
An enhanced architecture for a nuclear reactor core includes several technologies: (1) nuclear fuel tiles (S-Block); and (2) a high-temperature thermal insulator and tube liners with a low-temperature solid-phase moderator (U-Mod) to imp...
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WO/2021/065180A1 |
[Problem] To provide an electric aircraft and a method for controlling the aerodynamic performance thereof with which it is possible to optimize aerodynamic performance of a blade, irrespective of the shape of the blade, in each flight p...
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WO/2021/067756A1 |
The present disclosure presents environmental sensing apparatuses and methods. In one such apparatus, an environmental sensor comprises a substrate and an array of multiple metal oxide materials on the substrate. The multiple metal oxide...
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WO/2021/064014A1 |
The invention is based on an aircraft-seat module having an enclosure unit, which at least partially delimits a passenger-seat region, and having a door unit, which is provided at least so that, at least in an operating state, it closes ...
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WO/2021/064300A1 |
Functional professional drone which is remote-controlled by a user and the electronic control unit (500) of which communicates with the electronic control unit for piloting the drone (300), characterised in that the mechanical architectu...
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WO/2021/064350A1 |
A : spacecraft attitude control system comprising • at least one attitude control device (2), the attitude control device comprising • first and second magnets (3, 4) having magnetic dipole moments Ml and M2 respectively, each magnet...
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WO/2021/062524A1 |
An overhead luggage bin includes a bucket including side walls and a belly wall defining a luggage bin interior, a door displaceable between open and closed positions, and a bullnose extending along a forward edge of the belly wall. A hi...
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WO/2021/063775A1 |
The invention relates to a device (500) for a satellite laser distance measurement, comprising a base segment (520) and an optical segment (522) which is supported by the base segment (520) and has a telescope mounting (510) with an azim...
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WO/2021/065007A1 |
It is possible to realize a passenger boarding bridge in which a floor member formed by connecting a plurality of floorboard members can be held at a fixed angle with a simple structure. This is achieved with an aisle floor for an aircra...
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WO/2021/060113A1 |
A photography system that includes: an unmanned aircraft that has a photography unit; and a control device that can communicate with the unmanned aircraft and a subject terminal. The control device comprises: a storage unit at which is r...
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WO/2021/059323A1 |
[Problem] To provide an attachment that can improve flight efficiency, and an aircraft provided therewith. [Solution] This attachment is attachable to a box body that has a groove which opens through a slit extending in the longitudinal ...
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WO/2021/056455A1 |
A pump assembly (100), a spray system (10), a mobile device (1000), and a spray method. The pump assembly (100) comprises water pump devices (110), a liquid dispenser (120), and a pressure relief mechanism (130). The liquid dispenser (12...
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WO/2021/056080A1 |
The present invention relates to an aerially distributable communications device (ACCD) including one or more gyrochutes and communications module configured for wireless communication with external communication nodes. The communication...
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WO/2021/062434A2 |
A cargo module swapping system for an electronic short take-off and landing aerial vehicle, including an autonomously driven robotic vehicle for transporting and swapping cargo modules on an autonomous electric aircraft. The robotic vehi...
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WO/2021/056139A1 |
A method for acquiring a landing position, a device for acquiring a landing position, and an unmanned aerial vehicle (12). A target landing area can be determined more effectively, so that the unmanned aerial vehicle (12) can land safely...
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WO/2021/060490A1 |
The purpose herein is to more accurately assist the avoidance of collisions of space objects such as satellites and space debris in outer space. A recorder processing unit (110) acquires, from a management business device (40) used by a ...
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WO/2021/011045A3 |
Systems, devices, and methods for a ground support system (100) for an unmanned aerial vehicle (UAV) including: at least one handling fixture (130), where each handling fixture (103) is configured to support at least one wing panel (107)...
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WO/2021/060491A1 |
To appropriately manage the disclosure of information on the orbit of a satellite constellation, an information management device (1000) is installed in at least one of a plurality of management business devices, each of which manages a ...
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WO/2021/056140A1 |
A joint assembly, a pressure type spraying system, and a movable platform, wherein the joint assembly is applied to the pressure type spraying system, comprising: a water tank joint (10), including a first end (11) for communicating with...
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WO/2021/059424A1 |
A satellite visibility assignment device (1) comprises a visibility unit setting section (21), a visibility unit selection section (22), and an optimal calculation unit (23). The visibility unit setting section (21) sets a visibility uni...
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WO/2021/062097A1 |
An aircraft airflow sensor including a vane assembly configured to sense a direction of local airflow outside an aircraft, at least one port arranged on the vane assembly, and at least one transducer arranged with the vane assembly confi...
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WO/2021/059665A1 |
Provided is a motor-integrated fluid machine having an integrally provided motor, the motor-integrated fluid machine comprising: a rotating part that rotates about a rotary axis; an outer circumferential part provided to the outer circum...
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