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Patent Searching and Data


Matches 401 - 450 out of 61,001

Document Document Title
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...  
WO/2018/110292A1
A flapping device (1A) is provided with a frame (10), an actuator installed on the frame (10), a pair of flexible wings (40) that generate lift by longitudinal oscillating movement, and cords (47) extended between the frame (10) and the ...  
WO/2018/107278A1
A capture-and-release aircraft for capturing and releasing fixed-wing aircraft is provided. The capture-and-release aircraft comprises a frame to which is secured a set of rotor units. Each rotor unit has a rotor with a rotation axis, th...  
WO/2018/112091A1
The use of UAV network cells may enable a wireless communication carrier to provide supplemental cellular network communication coverage to geographical areas. Geolocations of multiple user devices in a geographical area that is serviced...  
WO/2018/112275A1
Unmanned aerial vehicle (UAV) capture nets, netting systems, UAVs, and methods of making netting systems are disclosed. A UAV capture net may include an open-mesh material, and a plurality of streamers coupled to the open-mesh material, ...  
WO/2018/110290A1
This wing body (40) is provided with: a sheet body (70) which forms a wing surface; and a frame body (80) provided along the wing surface. The frame body (80) includes: a first frame part (81) extending along a front edge part (73) of th...  
WO/2018/109695A2
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/2018/108943A1
A control system for use in a vehicle configurable for air use or road use, the vehicle comprising moveable control surfaces for controlling operation of the vehicle in air use, wherein the system comprises: a pedal arrangement of three ...  
WO/2018/110102A1
The purpose of the present invention is to provide a transport jig which can easily transport a plurality of elongated members and which enables access to the plurality of elongated members in the same direction. This transport jig (1) i...  
WO/2018/107561A1
A method for controlling landing of an unmanned aerial vehicle (400, 500), comprising: an unmanned aerial vehicle (400, 500) measures N distances from N undercarriages (12, 13, 14, 15) to the ground when the unmanned aerial vehicle (400,...  
WO/2018/111073A1
The present invention describes a system for controlling a focussed-signal antenna for extreme-distance drone tracking, achieving an effective communication range of 10 km with said aerial vehicle. The system includes an antenna with an ...  
WO/2018/109903A1
There is a need to reduce damage to objects due to contact with a rotating rotary wing. A flight control method controls the control mode during flight of an unmanned aircraft, the method having a step for detecting abnormalities in the ...  
WO/2018/109066A1
The invention relates mainly to an arrangement (10) of individual seats intended for being installed in an aeroplane cabin (59) including a first set (11) of two seats (13.1, 13.2) and a second set (12) of two seats (13.3, 13.4), each se...  
WO/2018/108905A1
The invention relates to a method and to a device for position control of a spacecraft (1). In the method, a force is exerted on the spacecraft (1) by emitting at least one directed beam (7) of electromagnetic radiation having sufficient...  
WO/2018/110508A1
The purpose of the present invention is to attach an inner liner and a mouthpiece to each other without generating burrs. In the present invention, in a state in which a tube part 22C of an inner liner 22 is positioned inside a mouthpiec...  
WO/2018/110815A1
According to the present invention, a height adjustment device for adjusting a rotunda of a boarding bridge is provided. The rotunda height adjustment device for a boarding bridge comprises: an external column fixed to the ground and hav...  
WO/2018/112281A1
Unmanned aerial vehicle (UAV) capture devices and methods of operation are disclosed. A UAV capture device may include a netting system including a net launch device and a net, a propulsion system including a plurality of propellers coup...  
WO/2018/110598A1
The objective of the present invention is to provide a device, method, and the like that, when a failure has occurred, and in particular when a failure has occurred in the operation of part of a rotary wing, can control flight in accorda...  
WO/2018/111258A1
A computer is programmed to deploy an aerial drone to fly within a specified distance of a first vehicle. The computer is programmed to detect a second vehicle and then activate an aerial drone light.  
WO/2018/104829A1
A method of automatic roll control in a UAV includes adjusting UAV yaw, measuring UAV pitch, estimating UAV drag, and estimating UAV velocity from the drag. A system includes a processor and a memory including instructions to automatical...  
WO/2018/103457A1
An unmanned aerial vehicle (100) comprises a vehicle body (2), an arm component (4), and rotor mechanisms (6). The arm component is connected to the vehicle body. The rotor mechanisms are arranged via the arm component at the periphery o...  
WO/2018/104521A1
The invention concerns a method for gauging the liquid propellant tank (10) of a spacecraft during a phase of high-thrust along an axis (12), said tank being thermally conductive and having a known geometry. The method comprises steps of...  
WO/2018/105599A1
An objective of the present invention is to optimize actions of an unmanned device group as a whole in a state where each of the devices configuring the unmanned device group autonomously carries out action selection. The present inventi...  
WO/2018/106384A1
A magnetic spring input device is disclosed. In various embodiments, an input device as disclosed includes a manual input structure movably coupled to a base assembly; and a non-stationary magnet fixedly coupled to the manual input struc...  
WO/2018/103203A1
Disclosed is a ducted unmanned aerial vehicle, comprising: an aerial vehicle body (9), a first duct (1), a second duct (2), a third duct (3), a fourth duct (4), a front landing gear, and a rear landing gear. The first duct (1) is connect...  
WO/2018/106074A1
An unmanned aerial vehicle (UAV) may include: a flight body; a camera installed on the flight body; a sensor module mounted inside the flight body to sense nearby surroundings; a wireless communication module mounted inside the flight bo...  
WO/2018/106137A3
The present invention relates to a distributed electric propulsion system and vertical take-off and landing ("VTOL") aircraft and especially to this having hybrid or electric drive, used to transport people or goods from one point to the...  
WO/2018/103762A1
A distributed propulsion system, wherein an input end of a gas collection device of a high energy working medium collection device is connected to an output end of a core machine gas compressor of a turbine engine core machine, an output...  
WO/2018/106331A1
An electric machine is provided which includes a rotor disk extending along a radial direction and having a rotor flange attached to or formed integrally with the rotor disk and extending substantially along the axial direction. A plural...  

Matches 401 - 450 out of 61,001