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WO/2020/052102A1 |
A fire-fighting drone aiming method comprises: controlling a fire-fighting drone to fly to a fire-hit region; enabling the fire-fighting drone to hover around the fire-hit region; transmitting an image of the fire-hit region back via a g...
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WO/2020/054876A1 |
[Problem] To provide a work management system for easily recording and managing the progress state of a work process. [Solution] This work management system 1 is for managing work having a plurality of steps and has a terminal 407 wearab...
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WO/2020/049604A1 |
The present invention refers to a large multirotor rotary wing drone with the possibility of being connected to other drones of the same type by means of special connectors so as to increase the load capacity and flight time. It has a pr...
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WO/2020/044895A1 |
Provided is a control device for controlling a plurality of flying objects each having: a solar battery panel; a battery for storing power generated by the solar battery panel; and an antenna for forming a communication area on the groun...
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WO/2020/041218A1 |
Briefly, example methods, apparatuses, and/or articles of manufacture are disclosed that may be implemented, in whole or in part, to facilitate and/or support one or more operations and/or techniques for a system controller for a series ...
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WO/2020/039822A1 |
Provided is a control device that controls a flying object having a solar battery panel and an antenna for forming a communication area on the ground by using power generated by the solar battery panel and for providing a wireless commun...
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WO/2020/035042A1 |
A power supply method and device for an aircraft, a flight control system, and an aircraft. Said method comprises: determining the current flight phase of an aircraft (100); and controlling a battery (20), of which the discharge rate cor...
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WO/2020/034148A1 |
A power supply method and device. The power supply method is applied to a host device (100). The host device comprises a power supply circuit. The power supply circuit comprises a first power supply circuit (130) and a second power suppl...
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WO/2020/024423A1 |
An aircraft, a solar cell system (100), a wing (200), and a manufacturing method for the wing (200). the solar cell system (100) comprises a first encapsulation layer (2), a second encapsulation layer (3), and one or a plurality of photo...
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WO/2020/025886A1 |
The invention relates to a turbomachine with a longitudinal axis, comprising two, respectively upstream (122) and downstream, coaxial outer propellers (122), characterised in that at least some of the blades (148) of the upstream propell...
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WO/2020/027140A1 |
Provided is a system comprising a floodlight and a control device, the control device having: a floodlight position information acquisition unit that acquires floodlight position information indicating the position of the floodlight; an ...
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WO/2020/025332A1 |
A method for managing the propulsive power of an aircraft, the aircraft extending longitudinally along an axis X from the rear forwards and comprising at least two lateral propulsion systems (2) each comprising a fan, each lateral propul...
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WO/2020/022264A1 |
[Problem] To obtain a flying body with enhanced flight attitude stability through ingenious modification of the layout of constituent parts. [Solution] This flying body includes: a plurality of propellers 101-1a to 101-4b; a plurality of...
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WO/2020/022263A1 |
[Problem] To provide an aircraft with which it is possible to reduce vibrations of a fuselage by manipulating the arrangement position of the fuselage which is equipped with a control unit required by an aircraft. [Solution] The present ...
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WO/2020/022266A1 |
[Problem] To provide a drone that can maintain a high level of safety even during autonomous flight. [Solution] This drone includes: a battery 502 for supplying driving power; an information acquisition unit 24 for measuring the temperat...
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WO/2020/015257A1 |
A power device (100) and an unmanned aerial vehicle (1000). The power device (100) comprises a motor (20) and a propeller (10) mounted on the motor (20). The propeller (10) comprises a propeller hub (11) and at least two propeller blades...
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WO/2020/016510A1 |
A system (10, 10', 10") for propulsion and for non-propulsive electricity generation for an aircraft (7) comprising at least one turbomachine (11) and at least two pairs of rotors (1 to 6), the rotors of one same pair (1 and 6, 2 and 5, ...
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WO/2020/016941A1 |
[Problem] To provide a flying body in which a working unit can be brought into an appropriate proximity to a site on which work is to be performed. [Solution] This flying body system comprises a first rotary-wing aircraft and a second ro...
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WO/2020/016942A1 |
[Problem] To provide a flying body in which a working unit can be brought into an appropriate proximity to a site on which work is to be performed. [Solution] The power feeding method for a flying body in the present invention involves: ...
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WO/2020/016946A1 |
With conventional UAVs, it is difficult to achieve flight of adequate reliability in terms of flight distance, safety, etc. Provided is a multi-rotor helicopter (10) having: a fuselage (11); a flight motor unit (100) that has a flight mo...
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WO/2020/011380A1 |
A propulsion system for a multirotor aircraft, the propulsion system comprising: at least one power generation module configured to provide a first source of electrical power to one or more propulsion assemblies of the multirotor aircraf...
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WO/2020/011867A1 |
The invention relates to a hybrid-electrical drive system for an aircraft having two subsystems that are largely independent of each other. A stator winding of a common electrical machine is assigned to each of the subsystems such that b...
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WO/2020/012996A1 |
The present technology pertains to an unmanned aerial vehicle, driving method, and program that can easily keep the vehicle body in good balance. This unmanned aerial vehicle is provided with a plurality of motors for spinning a pluralit...
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WO/2020/008147A1 |
The invention relates to an aircraft propulsion system (100) intended for being built into the rear of an aircraft fuselage, the propulsion system comprising at least two gas generators (102a, 102b) supplying a power turbine (104) having...
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WO/2020/000658A1 |
An unmanned aerial vehicle (10) and an arm (100) thereof, the arm (100) of the unmanned aerial vehicle (10) comprising: a body (110); a foot support (120) is provided at a front end of the body (110), and an inner part of the foot suppor...
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WO/2020/002822A1 |
The invention relates to a fire resistance device (50) that is designed to be placed between a mounting strut (9) of a double-flow aircraft turbomachine and a connecting cowling (30) with which said turbomachine is equipped, the connecti...
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WO/2020/002504A1 |
The invention relates to a supplementary function module (1) for vehicles, more particularly airliners, and to an aircraft with a corresponding supplementary function module (1). The purpose of the supplementary function module (1) is to...
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WO/2020/002503A1 |
The invention relates to a functional enhancement module (1) for aircraft, more particularly commercial aircraft, to enhance a functional module (30) supplied with electric power via a power supply bus (20), and to an aircraft having a c...
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WO/2020/003181A1 |
The application provides a pod for moving a vehicle and also provides a network of interchangeable pods. The pod includes an energy storage and powering machine and a nacelle. Refer-ring to the nacelle, it includes an enclosure for surro...
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WO/2020/003239A2 |
A tail sitter (1, 1', 1'', 1''', 1'''') comprising a wing (4) with a closed front section (C) is described.
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WO/2020/004366A1 |
[Problem] To provide a drone, that is, an unmanned aircraft, which is capable of maintaining a high level of safety, even in autonomous flight. [Solution] This drone system 500, in which a controller 401 and a drone 100 operate in cooper...
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WO/2020/003240A1 |
A tail sitter aircraft (1') is described that comprises: a fuselage (2) arranged vertically in a take-off/landing position and transversely to a vertical direction in a cruising position of the aircraft; a single wing (4); at least two f...
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WO/2019/243119A1 |
The invention relates to a rear propulsion system (4) for an aircraft configured to ingest a boundary layer of said aircraft, the rear propulsion system (4) extending longitudinally along an X-axis, the rear propulsion system (4) compris...
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WO/2019/243767A1 |
An electric engine comprises: an inner casing; an outer casing which is positioned around the inner casing; a rotor comprising a plurality of rotor blades, the rotor being located between the inner and outer casings and being rotatable a...
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WO/2019/243117A1 |
The invention relates to a rear propulsion system (4) for an aircraft configured to ingest a boundary layer of said aircraft, the rear propulsion system (4) extending longitudinally along an X-axis, the rear propulsion system (4) compris...
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WO/2019/244462A1 |
[Problem] To provide a multicopter with low energy consumption and having a high degree of freedom for miniaturization design. [Solution] The present invention has: a fuselage 12; N number of first lift generators 30 which are located on...
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WO/2019/241357A1 |
The present disclosure pertains to electric machines such as electric propulsion systems for aircraft that integrated cooling systems, and methods of cooling such an electric machine. Exemplary electric machines include an electric motor...
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WO/2019/241725A1 |
A hover-capable aircraft includes a body including a tubular strut, a first rotor assembly rotatably coupled to the body and positioned about the strut, wherein the first rotor assembly includes a first plurality of circumferentially-spa...
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WO/2019/241581A1 |
An aircraft has a frame, at least one electrically-powered propulsion unit providing motive power for levitation and translation of the aircraft, at least one pod comprising a battery, mounted by a physical interface to the frame, the ph...
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WO/2019/233060A1 |
Disclosed are a control system and a control method for an oil-electric hybrid multi-rotor unmanned aerial vehicle, the control system comprising a fuselage (1) and a plurality of rotors (2) evenly arranged on side faces of the fuselage ...
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WO/2019/232472A1 |
A power system with a reliability enhancing battery architecture for electric motors adapted for use in an aerial vehicle. Individual batteries may be used to power a subset two or more motors in systems with six or more motors, for exam...
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WO/2019/227610A1 |
The present invention relates to the field of unmanned aerial vehicle and the invention provides a high-low voltage switching device, an unmanned aerial vehicle and a switching method therefor. The switching device is applied to a multip...
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WO/2019/225607A1 |
[Problem] To provide an aircraft wherein the need for additional components for heat radiation is eliminated by making the structure of the aircraft itself suitable for heat radiation, and a frame for the aircraft. [Solution] This aircra...
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WO/2019/222603A1 |
An aircraft-based power system includes a charger system that includes a charger controller and a charger circuit. The charger system is further configured to connect to a ground-based power source and the charger system is further confi...
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WO/2019/220038A1 |
The invention relates to an aircraft power architecture comprising a power transmission gearbox (12), located in a first compartment (30), a gas turbine (14), located in a second compartment (32) comprising a gas generator (18) and a fre...
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WO/2019/214944A1 |
The invention specifies an arrangement having at least one electrical module (2) which is arranged on a heat sink (3). The arrangement has: - first deflection elements (4) which are formed in or on the electrical module (2), - second def...
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WO/2019/216189A1 |
[Problem] To provide a drone group that can measure, in an established three-dimensional measurement formation, the three-dimensional atmospheric environment of an arbitrary space to be measured in the sky. [Solution] In a drone group 10...
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WO/2019/211549A1 |
The invention relates to a propulsion system (7) for a helicopter (1), comprising a linked turbine engine (10) that is able to drive a main rotor (4) intended to be coupled to a rotary wing, characterized in that the propulsion system (7...
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WO/2019/210501A1 |
Provided are a propeller mounting structure (100), a propeller (200) matched with the same, a power set (300) comprising the propeller mounting structure (100) and the propeller (200), and an unmanned aerial vehicle. The propeller mounti...
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WO/2019/210639A1 |
Disclosed are a throttle control method and apparatus, and an unmanned aerial vehicle. The method comprises: receiving a throttle control signal, and acquiring the final throttle given by the throttle control signal (101); acquiring the ...
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