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Matches 1 - 50 out of 2,011

Document Document Title
WO/2019/176423A1
This flight management device manages a flying device and comprises a notification unit that sends warning information to a vehicle at a position corresponding to positional information indicating the position of the in-flight flying dev...  
WO/2019/172253A1
A flight robot, provided with: a main flight unit; a propulsion part having a plurality of propulsion units that generate a propulsion force by the driving of rotors, the plurality of propulsion units being provided to the main flight un...  
WO/2019/172060A1
[Problem] To achieve a battery which can be disabled when a phenomenon that can cause malfunction is detected, and a charger. [Solution] This battery is provided with: a battery pack 11 which has battery cells; sensors 12, 13 which detec...  
WO/2019/173831A1
The present invention relates to a method, system, and apparatus of flight system for individual users using electric ducted fans. The flight system comprises a modular unit, which comprises a plurality of electric ducted fans, means for...  
WO/2019/168044A1
[Program] To provide a highly safe drone. [Solution] A drone 100 comprising: a flight means 101-1a, 101-1b, 101-2a, 101-2b, 101-3a, 101-3b, 101-4a, 101-4b; a flight control unit 23 that operates the flight means; and an operating state d...  
WO/2019/168079A1
[Problem] To provide an agrochemical spraying drone that is highly safe. [Solution] The present invention detects a drone making contact with an obstacle by a combination of an acceleration sensor and a contact detection sensor. If conta...  
WO/2019/163173A1
This rectifying structural body 100 of a flying object is provided with a rectifying part 30, a heat input control part 20, and a vacuum heat insulated part 10. The rectifying part 30 has a rectifying surface 30a and a rear surface 30b. ...  
WO/2019/158373A1
The invention relates to a drive device (1) for an aircraft, comprising: an electric machine (2) with a stator (3) and a rotor (4) and a cooling device (10) for cooling the electric machine (2), the cooling device (10) having an encapsul...  
WO/2019/154891A1
The machine assembly comprises a plurality of electric machines (60), wherein rotors (50) and/or stators (40) of the electric machines (60) are mechanically coupled to one another. The electric machine serves, in particular, to constitut...  
WO/2019/154064A1
A gasoline-electric hybrid power vertical take-off and landing aircraft having driving rotors, said aircraft comprising at least two main rotors (1), one end of the main rotor being connected to a central coupling member, the central cou...  
WO/2019/151055A1
Provided is a wireless power transmission device which implements an efficient wireless supply of power to an aerial vehicle with high power reception efficiency. The wireless power transmission device, which wirelessly transmits power t...  
WO/2019/150637A1
The present invention comprises: a main wing 11; an engine 15 attached to the main wing 11; and a connecting structure 20 for connecting the main wing 11 and the engine 15. The connecting structure 20 has: an engine pylon 21 that is prov...  
WO/2019/148875A1
An electronic speed controller (10) and an unmanned aerial vehicle (100). The electronic speed controller (10) comprises a circuit board (11), a plurality of functional electronic components (12) and a plurality of ports comprising a sig...  
WO/2019/146271A1
This superconductive cable according to one aspect of the present disclosure is for transmitting electric power among a plurality of electric power devices mounted on an aircraft. The superconductive cable is provided with: a heat insula...  
WO/2019/146270A1
A superconductive cable system according to one aspect of the present disclosure is for transmitting electric power among a plurality of electric power devices mounted on an aircraft. This superconductive cable system is provided with: a...  
WO/2019/146578A1
When a specified flight-incapable parameter does not meet a safety standard, a flight control unit 203 controls a flight body 10 so as to perform an operation that corresponds to the reason the parameter exceeded the safety standard. It ...  
WO/2019/140642A1
The present disclosure relates to a battery safety alert system, comprising a detection device, a controller, a battery, a battery mounting portion, an engagement mechanism and a matching mechanism, wherein the detection device is used t...  
WO/2019/137791A1
The invention relates to a retaining assembly (10) of an electric motor (12) for driving an aircraft on an aircraft frame (14), said electric motor (12) being attachable to a support structure of the aircraft via said frame. The electric...  
WO/2019/140437A1
Compliant mounting systems, devices, and methods for mounting a vehicle engine to a vehicle structure or base include a top mount, a lower mount, a center trunnion mount, and an aft mount which are configured to react forces transmitted ...  
WO/2019/096358A3
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-...  
WO/2019/135271A1
An unmanned aircraft reservation 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 ...  
WO/2019/135272A1
A flight control system that has: an unmanned aircraft that has a battery; a flight management device that includes a storage part at which is stored information about the past flight record of the unmanned aircraft, that receives aircra...  
WO/2019/134406A1
Disclosed is an unmanned aerial vehicle (100). The unmanned aerial vehicle (100) comprises: a frame main body (10) and a battery (20), wherein the frame main body (10) comprises a battery accommodating cavity (11) for accommodating the b...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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....  
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 (...  
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-...  
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...  
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...  
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...  
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...  
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...  
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 ...  
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...  
WO/2017/160656A3
A system and method for conducting electronic warfare on a target site includes the use of a small unmanned aircraft system (SUAS) having a fuselage and a Prandtl wing, wherein at least two electric ducted fans are positioned on the fuse...  
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 ...  
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...  
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...  
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...  
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...  
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...  
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...  

Matches 1 - 50 out of 2,011