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WO/2019/135273A1 |
A flight control system that has: an unmanned aircraft that has a battery; power supply devices that supply power to the unmanned aircraft; a flight management device that receives aircraft information about the unmanned aircraft, batter...
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WO/2019/119210A1 |
A battery, a battery control system, and an unmanned aerial vehicle. The battery (20) comprises: multiple cells (21) connected in series and multiple wires (22); one end of each wire (22) is electrically connected to the cathode or anode...
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WO/2019/122333A1 |
The invention relates to a drive system for an aircraft, comprising: a propeller P (101) having propeller blades; an electric motor E (102); a transmission system (103) for mechanically transmitting a positive torque T+ from the electric...
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WO/2019/124479A1 |
Provided is an energy system provided with: a first mounting unit whereon transportable energy storage equipment that can store energy or an energy source is detachably mounted; a second mounting unit whereon transportable energy storage...
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WO/2019/123419A1 |
An anti-torque system (10) for a helicopter (1) is described that comprises: an electric power supply unit (15); at least one first rotor (17), operatively connected to an electric power supply unit (15) and operable by the electric powe...
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WO/2019/122680A1 |
The invention relates to the field of propulsion assembly suspensions for aircraft, and more specifically, a load-bearing structure (30) configured to be mounted on a gas generator (11) of a dual-flow turbojet engine (7). The load-bearin...
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WO/2019/122684A1 |
The invention relates to the field of aircraft propulsion unit fairings and, more particularly, to an assembly comprising a longitudinal spar (31) configured to be mounted on a lateral member of a bypass turbojet engine (7) gas generator...
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WO/2019/122634A1 |
The invention relates to a suspension device (4) for a turbomachine comprising a body (15) intended to be secured to a stationary portion of an aircraft, extending along a longitudinal axis (A) that is designed to be parallel to an engin...
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WO/2019/125789A1 |
A buoyant aerial vehicle includes: a balloon configured to store a gas; a pay load coupled to the balloon; and a propulsion unit coupled to the payload by a tether. The propulsion unit includes: a fuselage having a substantially longitud...
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WO/2019/105219A1 |
Disclosed are an aircraft engine suspension and a suspension box section (100) thereof. The suspension box section (100) comprises: a body; and a suspension-engine connection part and a suspension-wing connection part formed in the body....
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WO/2019/105412A1 |
A battery (1), an unmanned aerial vehicle (3), an automatic terminal, and a transfer centre, the battery (1) comprising a battery body and a clamping mechanism connected to the battery body and used for clamping and releasing a package (...
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WO/2019/096358A2 |
The invention relates to an autogyro having a fuselage comprising a rotor on its upper face, the rotor having rotor blades and being made to autorotate by an airflow, wherein the rotor has a rotor drive such that said rotor can be motor-...
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WO/2019/092371A1 |
The invention concerns a method and a device for manufacturing a structural and/or acoustic panel for a nacelle of an aircraft propulsion assembly. The invention involves heating, by means of a heating means (3) producing electromagnetic...
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WO/2019/094804A1 |
Exhaust redirecting devices are described that are suitable for use in tilt rotor aircraft. Such devices are constructed of light weight material and permit redirection of exhaust gases from turbojet engines of tilt rotor aircraft as nac...
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WO/2019/090191A1 |
A vertical landing and take-off aircraft VTOL transitions from a vertical takeoff state to a cruise state where the vertical takeoff state uses propellers to generate lift and the cruise state uses wings to generate lift. The aircraft ha...
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WO/2019/086742A1 |
The present invention relates to an assembly of three wings joined with or without marginal plates, for aerial, water, land or space vehicles, to reduce induced drag and interference drag and provide greater manoeuvrability, independence...
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WO/2019/083490A1 |
The claimed technical solution belongs to systems intended for setting a body in motion and can be applied in air and water carriers. The drive has a piston with the blades which are used to repulsion the body from environment. Among the...
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WO/2019/083638A1 |
Features for a tail-sitter aircraft having efficiently designed propulsive elements are disclosed. The aircraft may have a tail with landing mounts to support the aircraft in a vertical position for takeoff and landing. The aircraft may ...
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WO/2019/075555A1 |
An assembly comprises a wing and a pylon fairing extending from the wing at a pylon location. The pylon fairing has an aerodynamic profile defining a fairing trailing edge. The pylon fairing has an upper section extending from the wing a...
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WO/2019/073601A1 |
The present invention meets flying distance and flying time requirements while effecting safe flight for an unmanned flying body. This unmanned flying body comprises: a thrust generating device; a flight control device that controls the ...
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WO/2019/063682A1 |
The invention relates to a method for propelling an aircraft. In order to obtain electric energy, fuel is combusted and an electric machine is used, wherein the fuel is used to cool at least one part of the electric machine, and the fuel...
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WO/2019/063942A1 |
Drone for dispersing capsules which contain biological active agents for combatting pests, the dispersion aircraft comprising: - a propulsion means which ensures the movement of the aircraft in a horizontal direction parallel with the gr...
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WO/2019/061782A1 |
Disclosed are a battery module and an unmanned aerial vehicle. The battery module comprises a battery body (200) detachably mounted in a battery compartment (100); the battery body (200) is provided with at least one locking assembly (21...
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WO/2019/065848A1 |
Provided is an autonomous flying device in which a large payload and long continuous flying time are ensured, and the position and orientation during flight can be reliably adjusted. This autonomous flying device 10 is equipped with: a m...
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WO/2019/058647A1 |
The present invention addresses the problem of providing a highly durable all-weather motor capable of maintaining motor performance in such a way that the degradation of the motor performance is prevented by enhancing a heat dissipation...
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WO/2019/058991A1 |
Provided is a communication relay device with which it is possible to stably achieve a three-dimensional network, such as 5G mobile communication, across a wide area, and to reduce energy consumption. The communication relay device compr...
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WO/2019/052530A1 |
Disclosed is a hybrid electric unmanned aerial vehicle, comprising a primary frame (1) and two secondary frames (2), two primary rotors (3) respectively arranged at two ends of the primary frame (1), four secondary rotors (4) respectivel...
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WO/2019/051993A1 |
Provided is a foldable propeller, comprising a propeller assembly (100) and a rotary driving assembly (200), wherein the propeller assembly (100) comprises a first blade (1), a propeller upper bracket (2), a second blade (3) and a propel...
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WO/2019/049313A1 |
[Problem] To provide an aerial vehicle having improved responsiveness during transportation. [Solution] An aerial vehicle 1 includes: a fixed rotor 20b (20) that supports a first rotary wing 50b so as to allow rotation thereof; a movable...
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WO/2019/042095A1 |
A given rotational speed calculating method, a device, an electronic speed controller, a power system, and an unmanned aerial vehicle. The given rotational speed calculating method comprises: acquiring a maximum rotational speed, a minim...
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WO/2019/044866A1 |
Provided are a container with a battery, and a delivery system using the container with the battery, capable of continuous operation for a long time. The gist of the invention is to provide a container that includes a case body for conta...
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WO/2019/044842A1 |
This battery pack (2000) comprises a secondary battery (2020), a sensor (2040), and a control device (2060). The secondary battery (2020) supplies electric power to a flying object (10). The sensor (2040) outputs a measurement value rela...
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WO/2019/034765A1 |
The invention relates to a vertical takeoff aircraft (1), preferably an unmanned aerial vehicle (UAV), drone and/or unmanned aerial system (UAS), comprising: a rigid wing (5) which is oriented substantially horizontally both when hoverin...
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WO/2019/035080A1 |
A system and method for distributing power to racing aircraft systems is provided. The system includes a race course, a power transmitter directed towards a power delivery section of the race course, the power transmitter configured to r...
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WO/2019/030832A1 |
The present invention achieves a mechanism for an unmanned aerial body to receive power via contactless charging, while mitigating adverse effects on the performance of the unmanned aerial body. This unmanned aerial body comprises: a pla...
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WO/2019/020684A1 |
The invention relates to an electric motor having an integrated cooling device, which particularly uses bleed air as the primary coolant for cooling components of the stator and/or of the rotor. According to the invention, the environmen...
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WO/2019/016509A1 |
An aerodynamically shaped pod for an aircraft, particularly a solar powered high altitude long endurance unmanned aircraft. The pod is removable and contains an inner removable unit (AIB) which holds systems required to operate the aircr...
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WO/2019/016510A1 |
The present invention provides a pod (100) for an aircraft (1000), comprising: a housing (1); a unit (2) comprising a propulsion system, the unit comprising at least one attachment point (5) for coupling the unit to the housing (1), wher...
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WO/2019/010993A1 |
Disclosed are a stator seat (100), an electric motor (200), and an aircraft (300). The stator seat comprises: a fixing seat (10) and a bearing bush (20), wherein the bearing bush is fixed to the fixing seat, the bearing bush comprises at...
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WO/2019/009940A1 |
Various embodiments include methods for operating a photovoltaic-powered drone (101) having a photovoltaic surface (110) on one side of at least one of wing or fuselage body of the drone (101). The method may include determining a flight...
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WO/2019/009944A1 |
Various embodiments include methods for operating a photovoltaic- powered drone (101) having a photovoltaic surface (110) on one side of at least one of wing (106) and/or body (102) of the drone (101). Various embodiments may include fly...
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WO/2019/009424A1 |
Provided are: an aircraft that can fly stably even when water is discharged from a hose installed on the airframe thereof; and an aircraft system that uses the aircraft. This aircraft system comprises: a master aircraft 10; three slave a...
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WO/2019/006469A1 |
An electric aircraft has a fault-tolerant electrical system designed to optimize competing concerns related to cost, performance, and safety. An electrical system in accordance with some embodiments of the present disclosure has a plural...
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WO/2019/001998A1 |
The invention relates to an engine device, in particular based on a gas turbine, which preferably can be used for a hybrid-electrically driven aircraft. A drive section of the engine device produces an accelerated gas flow, which is furt...
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WO/2018/233570A1 |
A gasoline-electric hybrid multiaxis rotor type unmanned aerial vehicle, which relates to the technical field of unmanned aerial vehicles. The unmanned aerial vehicle comprises an unmanned aerial vehicle frame, a lifting rotor (2) and an...
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WO/2018/233860A1 |
The invention concerns a drive unit (100) for an aircraft, comprising: - a pylon (102) intended to be attached under a wing (14) of the aircraft (1) and having a front face (104) and a lower face (105) and - a turbine engine (10) compris...
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WO/2018/227270A1 |
A system for providing both driving and charging functionality by using a plurality of traction inverters and a plurality of energy storage devices coupled to one another across the electric motor; an AC/DC converter front-end circuit in...
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WO/2018/225757A1 |
This unmanned aerial vehicle is provided with a main body unit, a propulsion unit which has a rotor blade and a motor for rotating the rotor blade about a rotation shaft and which is attached to the main body unit, a rechargeable battery...
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WO/2018/224808A1 |
A method of producing an aircraft battery system, the method comprising: identifying a volume of free space on an aircraft (100); arranging a plurality of electrical power cells (112, 114) such that the plurality of cells (112, 114) are ...
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WO/2018/225769A1 |
This unmanned aerial vehicle is provided with a main body unit, a propulsion unit which has a rotor blade and a motor for rotating the rotor blade about a rotation shaft and which is attached to the main body unit, a rechargeable battery...
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