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Matches 1 - 50 out of 6,358

Document Document Title
WO/2019/073417A1
A frame assembly for an aerial system (12) includes a body (20) and a first rotor assembly (72) and a second rotor assembly (74). The first and the second rotor assemblies are coupled to the body (20) by respective hinges (86). The first...  
WO/2019/073520A1
[Problem] To provide a flying body having a new structure capable of improving flight efficiency. [Solution] The problem is addressed by a flying body capable of traveling along at least a first direction and comprising a fuselage part a...  
WO/2019/073984A1
[Problem] The purpose of the present invention is to provide a method for efficiently shading the whole of a fixed tract of land having no roofing, supports for a roof, or the like, such as schoolyard or a track and field stadium. [Solut...  
WO/2019/074393A1
The present invention relates to the field of aircraft. The proposed aircraft has the appearance of a "flying saucer" and calls to mind the astronomical phenomenon of the arrangement of the rings of Saturn, wherein the aircraft is capabl...  
WO/2019/073415A1
A frame assembly for an aerial system(12) including a fuselage body(20),a first rotor assembly(72) and a second rotor assembly(74) is described. The first and second rotor assemblies(72,74) are coupled to the fuselage body by respective ...  
WO/2018/214124A9
System, devices, and methods for a movable vehicle comprising a transformable/convertible structure are described. In some embodiments, the movable vehicle comprises a main body having a vertical axis, a first arm, and a second arm, wher...  
WO/2019/073521A1
[Problem] To provide a rotorcraft capable of improving flight efficiency. [Solution] This rotorcraft can advance along at least a first direction and comprises an arm portion, multiple motors attached to the arm portion, and a rotor atta...  
WO/2019/069498A1
A frame 10 for a multicopter 1 includes a frame body 24 having an opening 34 in a top surface thereof and having a first recessed section 36 that can accommodate a battery 12 and an electrical box 14. A flange section 66 is formed integr...  
WO/2019/069591A1
[Problem] To maximize the static thrust of a ducted fan. [Solution] This ducted fan 1 has a duct 10, a propeller 20, a motor 30, a housing 40, and a stator 50. The propeller 20 has a hub 21 disposed concentrically with respect to the duc...  
WO/2019/069740A1
The purpose of the present invention is to provide an image capturing device and an image capturing method which enable a captured image to be acquired in which the effect of reflected light is effectively suppressed in all directions of...  
WO/2019/069741A1
The purpose of the present invention is to provide an image capturing method and a program with which a plurality of captured images in which the effect of reflected light is suppressed can be acquired by way of scanning image capturing ...  
WO/2019/062257A1
A double lift force ducted vertical take-off and landing aircraft based on a tilt duct, comprising an aircraft body (10), two wings (9), N tilt ducted fans (1, 2), two lift force ducted fans (5, 7), and two duct covers (6, 13), N being a...  
WO/2019/060933A1
The invention relates to a spokeless and hubless wheel (52) inside which at least one electrically driveable propeller (44) is integrated in such a way that the risks associated with propeller rotation are kept as low as possible. The wh...  
WO/2019/062389A1
A propeller (10), a power assembly (100), and an unmanned aerial vehicle, relating to the technical field of propellers. The propeller (10) comprises: a hub (11) and at least two blades (12); the hub (11) comprises a housing (111), an up...  
WO/2019/063169A1
A rotor wing aircraft (100) provided with a propulsion apparatus (10), wherein said aircraft (100) comprises a rotating mast (50) configured to rotate said rotor wing (40), said apparatus comprising a pole (20) mechanically connectable t...  
WO/2019/062140A1
An unmanned aerial vehicle comprises a fuselage, arm assemblies, power assemblies, and photographing assemblies. The arm assemblies are installed at the fuselage. The power assemblies are installed at the arm assemblies, and are used to ...  
WO/2019/061533A1
Disclosed is an apron platform (200), comprising an apron region (210), a guide portion (220) adjacent to the apron region (210), and a positioning point (230) arranged in the apron region (210), wherein the guide portion (220) surrounds...  
WO/2019/061860A1
A flying body (100) for detecting a living body, the flying body having: a sensor portion (310) for detecting living body information related to a living body; a support component for supporting the sensor portion (310) and freely extend...  
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/2019/062256A1
A single lift force ducted vertical take-off and landing aircraft based on a tilt duct, relating to an aerial vehicle. The vertical take-off and landing aircraft comprises an aircraft body, two wings, N tilt ducted fans, a single lift fo...  
WO/2019/056053A1
A vertical take-off and landing (VTOL) aircraft (10) comprises a fuselage (24) first and second forward wings (20, 22) and first and second rearward wings (30, 32), each wing having a fixed leading edge (25, 35) and a trailing control su...  
WO/2019/057464A1
The present invention relates to a transport system (1) comprising a carrier (2) having a drive (3) for moving the carrier (2), and a load receiving element (4) which can be coupled to the carrier (2) and decoupled from the carrier (2), ...  
WO/2019/058623A1
A supply plan device 10 calculates a first route supply point on a movement route at which the supply of a chemical agent is required, a second route supply point on the movement route closer to a supply area than the first route supply ...  
WO/2019/058196A1
The present disclosure pertains to a multi-rotor unmanned aerial vehicle (UAV). Aspects of the present disclosure provide a UAV that includes at least four arms, each configured with a co-axial pair of contra rotating propellers, wherein...  
WO/2019/056756A1
A propeller (10) comprises: a first propeller fastener piece (11), a second propeller fastener piece (12), connectors (14) and at least two propeller blades (15). The first propeller fastener piece (11) and the second propeller fastener ...  
WO/2019/056052A1
A vertical take-off and landing (VTOL) aircraft (10) includes a fuselage and first and second forward wings (20, 22), each wing (20, 22) having a fixed leading edge and a trailing control surface (50) which is pivotal about a generally h...  
WO/2019/059428A1
The objective of the present invention is to provide an unmanned aerial device capable of creating great thrust without causing interference with an external obstacle, by using a single-shaft rotor having a pair of propellers. To this en...  
WO/2019/055025A1
An integrated guidance and feedback control scheme for steering an underactuated vehicle through desired waypoints in three-dimensional space. The guidance and control algorithm takes as an input the desired trajectory for the translatio...  
WO/2019/052142A1
A flying car, comprising: a vehicle body (10) having a head and a tail; a first ducted fan (20) and a second ducted fan (30) respectively provided at the head and the tail, the first ducted fan (20) having a first central axis (23) and t...  
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...  
WO/2019/054027A1
An acquiring unit of the present invention acquires a flight plan containing first flight conditions. A setting unit sets a risk level for airspace in which an aircraft is flying. A determining unit determines second flight conditions. A...  
WO/2019/052196A1
An unmanned aerial vehicle, an arm assembly, and a rotating shaft structure (10). The rotating shaft structure (10) comprises: a first fixing seat (11); a first friction plate (12) disposed on the first fixing seat (11), the first fricti...  
WO/2019/054896A1
The invention relates to the field of aeronautics, specifically to aircraft having rotors. The technical result of the claimed invention is increasing the operational efficiency of an aircraft. The essence of the invention lies in the fa...  
WO/2019/054028A1
An acquisition unit acquires, by communicating with a server device, a flight plan that states a first flight condition. A state determination unit determines the state of communication. A condition determination unit determines a second...  
WO/2019/052011A1
Provided is a propeller protection cover, comprising a latching mechanism (10) and a protection cover main body (20) connected to the latching mechanism (10), wherein the latching mechanism (10) comprises a clamping member (11) used for ...  
WO/2019/051832A1
A movable object control method, comprising: acquiring a marker (31) in an image collected by a photographing device (22); determining pose information about the photographing device (22) relative to the marker (31); and controlling a mo...  
WO/2019/053058A1
The invention relates to an autogyro (1), comprising a rotor (3), which can be set into autorotation, an instrument panel (9), which has at least one display unit (11) and/or at least one operating unit (12), the instrument panel (9) hav...  
WO/2019/051432A1
Enclosures for facilitating activities in space, and associated systems and methods, are disclosed. A representative system includes a spacecraft having an enclosed interior volume (which can be formed by an inflatable membrane) and one ...  
WO/2019/050401A1
An unmanned aerial vehicle (1) adapted to be positioned against a substantially vertical wall (2) while hovering in the air, comprising a body and rotors (21), an arm end (51), a first leg end and a second leg end (31) intersected by a f...  
WO/2019/048439A1
Unmanned aerial vehicle (UAV) (1) including an inner frame (2), an inner flight propulsion system (4) mounted on the inner frame (2), an outer frame (8), a gimbal system (6) comprising at least two rotational couplings (26, 30) coupling ...  
WO/2019/047429A1
A multi-rotor unmanned aerial vehicle-based duct propulsion system, comprising a multi-rotor unmanned aerial vehicle (10), a first cradle head interface I (20), a duct buoyancy module (30) and a second cradle head interface II (40). The ...  
WO/2019/050756A1
Various embodiments include methods, devices, and systems of transporting a payload using a robotic vehicle. The methods may determine whether a payload has separated from the robotic vehicle and take a corrective action in response to d...  
WO/2019/046911A1
An unmanned aerial vehicle (UAV) adapted for transit in and deployment from a projectile casing is provided. The UAV includes a wing assembly coupled to the projectile casing and the wing assembly moveable between a closed position and a...  
WO/2019/048916A1
The invention of interest aims to further improve the controllability of the gyro-plane design against random wind fluctuations with an improved, adjustable auto-center-gravity design. The particular design auto correctes the shift in th...  
WO/2019/040975A1
An autonomous device for servicing the outside of buildings includes a vehicle that is suspended from and tethered to a positioning system secured to the building above the vehicle. The vehicle sends positioning signals to the positionin...  
WO/2019/041174A1
Disclosed is an unmanned aerial vehicle (1), comprising a machine body (10) and a plurality of arm assemblies (201, 202) arranged on the machine body (10), wherein each of the arm assemblies (201, 202) comprises an arm (221, 222) connect...  
WO/2019/041097A1
A frame assembly of an unmanned aerial vehicle, and an unmanned aerial vehicle. The frame assembly comprises a center frame (1) and two sets of arm assemblies (2) respectively disposed on two sides of the center frame (1); each of the ar...  
WO/2019/041252A1
A power device (100) comprises a duct (1), a main rotor (2), and at least two lattice fins (3). The main rotor (2) is positioned in the duct. The main rotor (2) is used to drive a fluid to flow in the duct to generate power. The lattice ...  
WO/2019/041511A1
Provided are a motor assembly (10) of an unmanned aerial vehicle, and an unmanned aerial vehicle. The motor assembly (10) comprises a motor main body (12) and a base (11) connected and fixed to the motor main body. The base (11) is conne...  
WO/2019/043520A1
An aerial system includes a body, a propeller coupled to the body, and a motor coupled to the propeller. The motor is configured to rotate the propeller in a first direction, wherein an other portion of the aerial system rotates in an op...  

Matches 1 - 50 out of 6,358