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Patent Searching and Data


Matches 501 - 550 out of 61,306

Document Document Title
WO/2018/118199A1
The present disclosure relates to systems and methods for operating aerial vehicles in water-based locations. Specifically, an exemplary system may include a floating tether station and an aerial vehicle coupled to the floating tether st...  
WO/2018/117592A1
Disclosed is an electronic device comprising: a housing; a seating portion formed inside the housing such that a first external electronic device and a second external electronic device are seated thereon; at least one interface that is ...  
WO/2018/117851A4
The present document discloses method, system and device for maritime pilotage involving a pilotage control center where a request for pilotage assistance for a vessel is received. After negotiating the request and - if agreed - the foll...  
WO/2018/114659A1
A method for producing a wind turbine rotor blade (200) is disclosed. The wind turbine rotor blade (200) has at least one inner blade section (210) and an outer blade section (220) as well as a connection element (600). The inner blade s...  
WO/2018/112637A1
The present disclosure relates to a mechanism for releasably securing components of a spacecraft together during launch until such time as the mechanism is commanded to release those components. Upon command, the components are then rele...  
WO/2018/111358A1
A launching system may include a multirotor platform that includes a plurality of motors and propellers. The multirotor platform may be launched from a launch tube and actuated to transition from a storage state to a flight state where t...  
WO/2018/108148A1
An unmanned aerial vehicle, comprising a fuselage (1) and multiple arms (2) disposed at left and right sides of the fuselage (1), said unmanned aerial vehicle also comprising a sliding mechanism; open grooves (3,11) are provided on the f...  
WO/2018/109582A1
A slat (50) for an aircraft wing comprises a leading edge (51) defining a leading edge line (61), a trailing edge (52) defining a trailing edge line (62), the leading and trailing edges line defining a slat plane, the chord distance (69)...  
WO/2018/110848A1
An electronic device is provided. The electronic device includes a communication circuit configured to establish a communication channel with an aerial vehicle, a sensor configured to collect location information and orientation informat...  
WO/2018/109251A1
The invention relates to a liftable truck container (1) for supplying aeroplanes, which comprises a rolling chassis (2) with stabilising feet (3) where a structure (4) and covering (5) of the container (1) is mounted, the covering (5) ha...  
WO/2018/110382A1
Provided is a flying device having: an acquisition unit that acquires communication quality information in which position information indicating a position and the communication quality at the position indicated by the position informati...  
WO/2018/111101A8
An insect elimination system eliminates a flying insect in an airspace. The system comprises: - a camera configured to provide image data representative of at least part of the airspace; - an unmanned aerial vehicle, UAV, comprising a pr...  
WO/2018/110788A1
The present invention relates to a shooting system using a drone, and disclosed is a shooting system using a drone, which comprises a laser gun and a sensor capable of receiving laser light instead of a shotgun and a pigeon used in a con...  
WO/2018/108834A1
A propulsion system for a vehicle (10) includes a propulsor (102) for generating a thrust for the vehicle, a motor (104) operable with the propulsor for driving the propulsor, a motor mount (164) for mounting the motor in or to the vehic...  
WO/2018/110650A1
A moving body (2) is provided with a main body (21), a propulsion engine (22), and an energy supply unit (3). The propulsion engine (22) propels the main body (21). The energy supply unit (3) supplies energy to the propulsion engine (22)...  
WO/2018/111059A1
The invention relates to the field of transport by air and water and to power engineering, in particular to designs of bladed propellers. A rotating-blade propeller comprises a plurality of blades which are independently connected to spi...  
WO/2018/112161A2
Systems and methods for reducing switching losses in an electrical system in an aircraft are provided. In one example implementation, a method can include receiving DC power at an inverter of an electrical power system of an aircraft. Th...  
WO/2018/107972A1
An arm and an unmanned aerial vehicle, the arm comprising a first arm segment (11) and a second arm segment (12), the first arm segment (11) being provided with a locking part (112) and the second arm segment (12) being provided with a l...  
WO/2018/108616A1
The invention relates to a longitudinal adjustment device (50) for a seat, particularly an aircraft passenger seat, said longitudinal adjustment device (50) comprising at least one rail arrangement (100), said rail arrangement (100) comp...  
WO/2018/110088A1
An unmanned aircraft 1 according to one embodiment of the present invention is able to properly make an emergency landing in case of an abnormality. The unmanned aircraft 1 is configured as a multicopter which flies with the lift and thr...  
WO/2018/109695A3
The present disclosure relates to a launch system and method. The launch system and method can include at least a preliminary accelerator tube system (PAT) that can be combined with a main accelerator tube system (MAT). The PAT alone or ...  
WO/2018/109255A1
The invention relates to a method for producing reinforced monocoque structures and to the structure obtained, the method comprising: using base components (1) made from a partially cured composite material and joining the base component...  
WO/2018/111101A1
An insect elimination system eliminates a flying insect in an airspace. The system comprises: - a camera configured to provide image data representative of at least part of the airspace; - an unmanned aerial vehicle, UAV, comprising a pr...  
WO/2018/107564A1
Disclosed is an unmanned aerial vehicle, comprising a fixed-wing fuselage (10), a fixed-wing power assembly (20) and multiple rotor power assemblies (30). The fixed-wing power assembly is provided on the fixed-wing fuselage. The multiple...  
WO/2018/111360A1
Unmanned aerial vehicles and flight planning methods and apparatus are disclosed. An example apparatus includes an unmanned vehicle including a body and a propulsion source to propel the unmanned vehicle during flight; and a route planne...  
WO/2018/107956A1
Provided in the present invention is an unmanned aerial vehicle and a power assembly thereof, a propeller and a propeller base assembly. The power assembly comprises a drive device, a propeller, and a propeller base assembly. The propell...  
WO/2018/110308A1
This flapping device (1A) is provided with: a power source (20); a power transmission mechanism (30); wing bodies (40R, 40L) driven by the power transmission mechanism (30); a first biasing part (60A); and a second biasing part (60B). Th...  
WO/2018/107416A1
A manually operable mechanism for mechanically and electrically connecting parts of an unmanned aerial vehicle (UAV) comprises a first engaging means (20) associated with a first part of the UAV including at least one first electrical co...  
WO/2018/107330A1
The systems, methods, and devices related to the control and operation of a carrier for supporting a payload. In one aspect, a carrier may comprise: a stator configured to be coupled to a base support, said stator comprising a spherical ...  
WO/2018/112404A1
Systems and methods are provided for autonomous airborne vehicle control using a millimeter-wave (MMW) radar. Embodiments of the present disclosure enable a MMW radar system to support an unmanned aerial vehicle (UAV) in accomplishing mi...  
WO/2018/111488A1
An aircraft including a wing system, a plurality of control surfaces, a camera mounted on a camera pod, and a control system. The camera pod is configured to vary the orientation of the camera field of view only in yaw, relative to the a...  
WO/2018/110291A1
This wing body (40) is used in a flapping device and generates a buoyancy force by performing a swing motion. The wing body (40) is provided with: a nonwoven fabric (70) which forms a wing surface; a frame body (80) which is overlapped o...  
WO/2018/107503A1
A visual simulation system is disclosed. The system may comprise a non-transitory computer-readable memory that stores computer-executable instructions. The system may further comprise one or more processors, individually or collectively...  
WO/2018/107964A1
The present application provides an unmanned aerial vehicle and a power assembly, a propeller, and a propeller base assembly thereof. The power assembly comprises a propeller and a propeller base assembly. The propeller comprises a seat ...  
WO/2018/112161A3
Systems and methods for reducing switching losses in an electrical system in an aircraft are provided. In one example implementation, a method can include receiving DC power at an inverter of an electrical power system of an aircraft. Th...  
WO/2018/110987A1
A fan-in-wing aerial vehicle according to an embodiment may comprise: a fuselage; main wings extending from both sides of the fuselage in the span direction; rotors rotatably mounted inside the main wings, respectively; and opening/closi...  
WO/2018/107337A1
A pan-tilt (100), comprising a driving mechanism (40). The driving mechanism (40) comprises a rotor assembly (43) and a stator (41); the rotor assembly (43) comprises an installing member (431) used for bearing an external load, and a dr...  
WO/2018/110306A1
This flapping device (1A) is provided with: a power source (20); a power transmission mechanism (30); wing bodies (40R, 40L) driven by the power transmission mechanism (30); and an engaged body position adjustment mechanism (50). The pow...  
WO/2018/111924A1
Aerial launch and/or recovery for unmanned aircraft, and associated systems and methods. A representative system includes a first, carrier aircraft having an airframe a propulsion system carried by the airframe and positioned to support ...  
WO/2018/110634A1
A problem to be addressed by the present invention is to provide a flight management system and flight management method for actively managing the flight of an unmanned aerial vehicle. Provided is a flight management system, etc., of an ...  
WO/2018/110883A1
A drone takeoff and landing system according to an embodiment comprises: a drone including a through-hole; and a landing pad including an extension member which can pass through the through-hole, wherein, when the extension member of the...  
WO/2018/110509A1
In the present invention, a tube part of an inner liner is thermally deformed along an inner peripheral section of a tubular part and an inner peripheral section of a dome part of the inner liner is attached to a skirt part using an adhe...  
WO/2018/109532A1
The present invention relates to a secure terminal (1) for the aerial transport of passengers whose technical and operational infrastructure makes it possible to ensure the physical security of the building, of the aircraft, of the goods...  
WO/2018/107434A1
A propeller protection cover, comprising an annular main body (10) and an installing support base (30), wherein an upper end face of the annular main body (10) is provided with a top layer net (20), and the installing support base (30) i...  
WO/2018/111346A1
A device is provided for controlling fluid flow over a window of a movable optical instrument housing. The device includes a generally annular body having an inner peripheral edge configured to correspond to a peripheral edge of the wind...  
WO/2018/108949A1
A vehicle having a first configuration for road use and a second configuration for air use, comprising: road wheels; a traction drive propulsion unit for driving road wheels when in contact with the ground; a thrust propulsion unit for d...  
WO/2018/110307A1
This flapping device (1A) is provided with: a skeletal body (10); a power source (20); a power transmission mechanism (30); and wing bodies (40R, 40L) driven by the power transmission mechanism (30). The power transmission mechanism (30)...  
WO/2018/111075A1
The present invention describes a system for a platform for automatically landing a drone at high descent speed, with magnetic attachment on contact, comprising a landing surface with a quickly recognisable visual pattern which, once pos...  
WO/2018/108227A1
Drone pipe for securely conveying goods unloaded from a drone, the drone pipe comprising : a dockingstation (1), a transport system in the pipe comprising chain, rubber, roll or using pressure.  
WO/2018/107733A1
A method and device for controlling an airship. The method comprises: acquiring route information and status information of the airship; determining, according to the route information and the status information, a speed and a tangential...  

Matches 501 - 550 out of 61,306