Login| Sign Up| Help| Contact|

Patent Searching and Data


Matches 1 - 50 out of 64,981

Document Document Title
WO/2019/169850A1
A motor control method, a motor control device, and an unmanned aerial vehicle control system. The motor control method comprises: receiving a control signal for controlling the speed of a motor; acquiring an upper threshold of a given s...  
WO/2019/171350A1
An example system for racing aircraft systems includes: a plurality of autonomous synchronized unmanned aircraft systems configured to form a swarm at a race course through which the aircraft systems are to navigate; and a controller con...  
WO/2019/171000A1
The invention relates to an active device for attenuating acoustic emissions (8) from a turbojet of an aircraft, characterised in that the device comprises conduits (20) for the circulation of a pressurised air flow supplying rotating el...  
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/2019/172256A1
Provided is a flying robot for performing a specified operation, said flying robot comprising a body, and a propulsion part having a plurality of propulsion units that generate propulsive power by the driving of a rotor and are provided ...  
WO/2019/172606A1
The present invention relates to a system and a method for reusing pesticide for preventing liquid pesticide from falling onto the surface of the soil around crops and for collecting and reusing same. The system comprises: at least one e...  
WO/2019/170671A1
This aircraft refuelling device (400) comprises a fuel circulation pipe (40) of which the downstream end (43) is equipped with a wing coupling (42) for connecting it to an inlet orifice of a fuel tank of the aircraft. This wing coupling ...  
WO/2019/172335A1
The objective of the present invention is to enable an unmanned aerial vehicle to be operated freely and controlled to fly stably. On the basis of three-dimensional coordinates of each marker, measured by means of a position measuring se...  
WO/2019/170302A1
An integrated drain mast structure for use in draining fluids emanating from aircraft components, such as turbine engines and fuselages, for facilitating the detection of fluids leaking from said components. A self-supporting tube sectio...  
WO/2019/170974A1
The invention relates to a method for designing a plan for acquiring zones to be implemented by a space system comprising at least one satellite for several users, the method comprising the steps according to which a processor, proceedin...  
WO/2019/171748A1
This aircraft platform (26) includes a base (40), a landing pad (42), a horizontal sensor (44), and at least one actuator (48R, 48L). The landing pad (42) is supported by the base (40). The horizontal sensor (44) detects the inclination ...  
WO/2019/172744A1
The present invention relates to an apparatus (100) and method (200) of affixing display material, more particularly, display material on aircraft interior surface such as overhead stowage bin, comprising the steps of: overlaying the dis...  
WO/2019/171364A2
The present invention relates to a new micro lattice structure. The micro lattice structure comprise a set of body centred cubic structures. Each body centred cubic structure comprises a set of nodes, wherein each pair of neighbouring no...  
WO/2019/172808A1
´╗┐The invention relates to jet propulsors widely used, for example, in various transport vehicles and is intended for equipping transport vehicles moving in a three-dimensional liquid (for example, in water body) or gas (for example, in...  
WO/2019/172700A1
The present invention relates to a drone for cleaning the window glass of a high-rise building and, more specifically, to a drone for cleaning the window glass of a high-rise building, comprising: a main body having a plurality of propel...  
WO/2019/170647A1
Said aircraft refuelling device comprises a deformable pipe (40) for the circulation of fuel, the downstream end (43) of which is provided with a wing fastener (42) for the connection thereof onto an intake port of the aircraft fuel tank...  
WO/2019/172061A1
[Problem] To achieve an unmanned aerial vehicle that can be disabled when a phenomenon that can cause battery malfunction is detected. [Solution] This unmanned aerial vehicle, in which a battery 1 can be mounted, comprises sensors 23, 24...  
WO/2019/173263A1
The invention is that of a remote deployed obscuration system useful in protecting law enforcement and military personnel, for example, against attack. The remote deployed obscuration system comprises an unmanned aerial vehichle (UAV) su...  
WO/2019/170997A1
The invention relates to a riveting machine comprising a piercing tool (52), an upper clamp (71) and a lower clamp (21), which are mounted with the ability to move relative to one another in the direction of the said clamps (71, 21) movi...  
WO/2019/171749A1
A traffic control system (10) includes one or more traffic signals (16A, 16B), aircraft (12), and ground control stations (14A, 14B). The aircraft (12) includes a position sensor (52) and a wireless communication device (42). The ground ...  
WO/2019/171062A1
A spacecraft is disclosed, comprising a deployable spacecraft body (110) comprising a plurality of sub-systems (321-324) for controlling operations of the spacecraft, and a plurality of panels (101, 102) and a plurality of hinges (112-11...  
WO/2019/169469A1
The invention relates to a spacer (100') for a cylindrical conduit, comprising a first component (10) provided with a first part (11) having a plane of symmetry (PS) and a longitudinal axis (AL) pertaining to said plane, said first part ...  
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/2019/172072A1
A high-lift device 11 provided to the main wing 10 of an aircraft 1, the high-lift device 11 comprising a slat 15 and a slat moving mechanism 16 that moves the slat 15 between a deployed position and a storage position. The slat 15 has a...  
WO/2019/172805A1
The invention relates to receiving systems intended for a customer of items of merchandise deliverable by drones. A system for receiving items of merchandise comprises means for delivering an item of merchandise, which are in the form of...  
WO/2019/170158A1
Provided is a transformable stratospheric airship, comprising: an upper hull (1), a lower hull (2), a folded ballonet (3), and wire arrangement mechanisms (4) arranged on the upper hull and the lower hull, wherein the folded ballonet com...  
WO/2019/172804A1
The invention relates to the field of aviation, particularly to designs for vertical take-off and landing aircraft. A convertiplane comprises a fuselage, a pair of wings (a fore wing and an aft wing), propulsion systems comprising engine...  
WO/2019/170668A1
The invention relates to a device for refuelling an aircraft, this device comprising a fuel flow duct (40), the downstream end (43) of which is equipped with a wing coupler (42) for connecting it to an inlet orifice of a fuel tank of the...  
WO/2019/173228A1
An unmanned aerial vehicle including a body, a platform, a rotor, a tether cable, and an actuation system. The platform is coupled to the body such that the platform is rotatable relative to the body about a first horizontal axis of rota...  
WO/2019/171231A1
A system, a method, and/or a computer program for mounting a cable device on an electric cable of an electric grid, and dismounting therefrom, the mounting device including a first coupling part arranged to attach the mounting device to ...  
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/2019/169491A1
A headrest for a seat having a backrest frame and a base. The headrest includes a displacement member mountable to the backrest frame to position a lower end of the displacement member in front of the backrest frame and above the base. T...  
WO/2019/173443A1
An aircraft apparatus may include an outer membrane and an inner flexible bladder. The flexible bladder may include a lighter-than-air lifting gas therein, and an interstitial space between the outer membrane and the inner flexible bladd...  
WO/2019/165611A1
A method for detecting a water ripple of an image, comprising: obtaining an image (301) obtained by photographing an image calibration device (20), wherein the image calibration device (20) comprises a plurality of calibration objects (3...  
WO/2019/168047A1
[Problem] To provide a drone that is safe. [Solution] This drone is provided with a flight means 101-1a, 101-1b, 101-2a, 101-2b, 101-3a, 101-3b, 101-4a, 101-4b, a flight control unit 23 which operates the flight means, and an approach de...  
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/2019/166280A1
The invention relates to a housing for an ejectable flight recorder of an airplane, comprising: an inner housing (110) with at least one inner edge (112) and a deformable outer region (120) with at least one rounded outer edge (122). The...  
WO/2019/168287A1
Disclosed are a system and a method for providing golf course services by using a fuel cell drone, the system and the method providing various services during rounds of golf through a fuel cell drone using a hydrogen fuel cell as a power...  
WO/2019/168045A1
[Problem] To provide a drone that is safe. [Solution] This drone 100 is provided with a flight means 101-1a, 101-1b, 101-2a, 101-2b, 101-3a, 101-3b, 101-4a, 101-4b, a flight control unit 23 which operates the flight means, and a strong w...  
WO/2019/168854A1
An autonomous wagon for receiving a package and transporting it to a storage unit for storage until retrieval by the recipient is described. The storage unit may include a heating or cooling mechanism for controlling the temperature in t...  
WO/2019/166281A1
The invention relates to a universal flight recorder (100) comprising securing means (110) in order to secure the flight recorder (100) in an airplane (50) recess (55) provided for this purpose and comprising connection means (150) for s...  
WO/2019/167846A1
A high-lift device (1) is provided with: a flap (2) disposed at a front edge (50a) of a main wing (50), and configured to be stored in the lower surface of the front edge (50a) and to be extended forward of the front edge (50a); a first ...  
WO/2018/111449A8
Various embodiments of a user-wearable device can comprise a frame configured to mount on a user. The device can include a display attached to the frame and configured to direct virtual images to an eye of the user. The device can also i...  
WO/2019/168643A1
A rail launch mechanism and method for launching a payload is configured to release payload lugs (52,54) of a payload from a platform (36). A rack for launching a payload includes multiple rails that separately engage lugs in the respect...  
WO/2018/098031A3
An unmanned autonomous vehicle is configured to delivery packages in a product delivery network. The vehicle includes an outer housing, a conversion circuit, a battery, and a control circuit. The outer housing includes a first layer that...  
WO/2019/167302A1
Provided is an industrial unmanned helicopter in which a wide load space can be ensured, in which the energy efficiency of coaxial contra-rotating rotors can be enhanced, and which provides a high degree of freedom in designing of the he...  
WO/2019/166040A1
Disclosed is a method for reducing contrails during operation of an aircraft (100, 100') having a heat engine (10). The method comprises: bringing about condensation of the moisture contained in the exhaust gas (A) of the heat engine by ...  
WO/2019/167333A1
This wireless communication system is provided with a shield chamber forming part, a leakage waveguide, a first antenna, a first device, a second antenna, and a second device. In the shield chamber forming part, an internal space serving...  
WO/2019/168316A1
A paradrone is disclosed. A paradrone according to an embodiment of the present invention comprises a canopy and a servomotor portion. The canopy comprises: a parafoil; a transverse canopy frame coupled to the parafoil so as to support t...  
WO/2019/168052A1
[Problem] To provide a drone having high safety. [Solution] A drone comprising: flight means 101-1a, 101-1b, 101-2a, 101-2b, 101-3a, 101-3b, 101-4a, 101-4b; a flight control unit 23 for operating the flight means; a crash determination u...  

Matches 1 - 50 out of 64,981