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Matches 1 - 50 out of 5,378

Document Document Title
WO/2018/006439A1
An integrated power multi-axis unmanned aerial vehicle, which comprises an internal combustion engine, an electric motor, an electricity storage unit, and an electric drive unit. The internal combustion engine is employed to drive an ele...  
WO/2018/008987A1
A drone component is provided. The drone component comprises a body structure, and a plurality of wing structures mounted in the body structure and configured so as to space the body structure from the ground, wherein the plurality of wi...  
WO/2018/004325A1
The invention relates to aircraft with eight rotors, and specifically to octocopters of the micro/mini unmanned aerial vehicle class, having a weight of up to 20 kg, and which may be used for package delivery, mapping, photography and ae...  
WO/2018/004626A1
Disclosed herein is a water helicopter includes a fuselage, first and second fixed wings extending outwardly from left and right ends of the fuselage, first and second propellers disposed in a spaced apart configuration on a top surface ...  
WO/2018/000593A1
Provided in the present invention is a propeller (100), comprising a paddle (200). An attack angle of the paddle (200) is 16.89±1.5 degrees at a place where the distance from the paddle (200) to a turning center of the propeller (100) i...  
WO/2017/219201A1
An unmanned aerial vehicle (100). The unmanned aerial vehicle (100) comprises an unmanned aerial vehicle main unit (1), multiple rotors (2), and a parachute (4). The unmanned aerial vehicle main unit (1) is connected to the rotors (2). T...  
WO/2017/219200A1
An unmanned aerial vehicle (100) comprising an unmanned aerial vehicle main unit (1), multiple rotors (2), a telescoping rod (4), and a photographing device (5). The unmanned aerial vehicle main unit (1) is connected to the rotors (2) an...  
WO/2017/220803A2
A surface treatment apparatus comprising a support frame, said support frame comprising one or more lift generating portions arranged in use to cause vertical movement of the support frame and one or more biasing portions arranged in use...  
WO/2017/222152A1
The present invention relates to an electronic apparatus and a method for operating the same according to various embodiments. The electronic apparatus comprises: a moving module comprising a motor; an audio module comprising a first noi...  
WO/2017/219199A1
An unmanned aerial vehicle. The unmanned aerial vehicle comprises an unmanned aerial vehicle main unit (1), multiple rotors (2), and a photographing device (4). The unmanned aerial vehicle main unit (1) is connected to the rotors (2) and...  
WO/2017/219256A1
A flying cleaning device capable of wall-climbing comprises an aircraft main engine, a wall-climbing assembly, a start-stop assembly, a cleaning assembly and a control module; the wall-climbing assembly comprises a first suction cup (32)...  
WO/2017/219202A1
An unmanned aerial vehicle (100) comprising an unmanned aerial vehicle main unit (1), multiple rotors (2), a photographing device (4), and a parachute (6). The unmanned aerial vehicle main unit (1) is connected to the rotors (2) and to t...  
WO/2017/219255A1
Unmanned aerial vehicles with tilting propellers, and associated systems and methods are disclosed herein. A representative unmanned aerial vehicle (UAV) apparatus includes an airframe(110), a plurality of spherical motors(120) carried b...  
WO/2017/215541A1
Disclosed are a flying robot protective device and a flying robot, relating to the technical field of robots. The flying robot protective device comprises a housing (1) covering a rotor; and the housing (1) is an enclosed shell structure...  
WO/2017/217287A1
In the present invention, errors in longitude/latitude information in map data compared with actual longitude and latitude are eliminated, and an operator causes an unmanned aircraft to fly autonomously to a destination indicated in the ...  
WO/2017/215550A1
The present application relates to a safety cover of an aircraft and an aircraft with a safety cover. The safety cover of an aircraft comprises a safety cover body and a fixed arm provided in the safety cover body. A first end of the fix...  
WO/2017/215529A1
A propeller and a fuselage, comprising a forming foam (10), at least one first fiber fabric layer (20) provided on an upper surface of the forming foam (10), and at least one second fiber fabric layer (30) provided on a lower surface of ...  
WO/2017/213936A1
A coupling is disclosed for connecting a propeller to a motor in an aircraft such as a rotary wing aircraft and the like. The coup! tag comprises a propeller hub having an inner propeller hub bore defining an axial keyway. A rotatable sh...  
WO/2017/213451A1
One embodiment discloses a drone motor and a drone comprising same, the drone motor comprising: a rotating shaft; a stator comprising a hole in which the rotating shaft is inserted; and a rotor arranged on the outer side of the stator, w...  
WO/2017/213392A1
Disclosed is a drone. The present invention includes a plurality of propellers creating a lift to prevent inclination and overturn of the drone due to a lift difference generated from uneven ground, a power driving unit providing a rotat...  
WO/2017/206003A1
An unmanned aerial vehicle comprises a motor (1), at least three sets of propeller assemblies, and a first transmission assembly for respectively transmitting movement of the motor (1) to each set of the propeller assembly, each set of t...  
WO/2017/208037A1
The present invention relates to a folding propeller-hub assembly and applicable flight modes of the assembly. In particular, the present invention provides a folding propeller-hub assembly for VTOL aircraft and for improved aerodynamic ...  
WO/2017/206070A1
Disclosed are an airframe of an unmanned aerial vehicle and an unmanned aerial vehicle (100, 200, 300) comprising a body (10, 10', 10") and an arm (20, 20', 20") connected to the body (10, 10', 10"). The arm (20, 20', 20") is provided wi...  
WO/2017/207666A2
The invention relates to an air ship having a supporting structure (12) and a shell (10) that can be filled with a gas and which is tensioned by the supporting structure (12). According to the invention, said supporting structure (12) co...  
WO/2017/209827A2
A vibration attenuation system for attenuating vibrations in a mast of an aircraft includes a weight attached to the mast but free to orbit about the mast. The weight can be comprised of one or more weight assemblies. Embodiments can inc...  
WO/2017/208754A1
An information processing device 20 is provided, for example, to a vehicle 40. A control unit of the information processing device 20 provides flight control of an unmanned aerial vehicle 50, moves the same to a destination, and acquires...  
WO/2017/205997A1
Systems and methods are provided for transformation of an arm (104) of an unmanned aerial vehicle (UAV) (100) between a flight configuration and a compact configuration. The arm (104) may have multiple foldable sections (104-11, 104-12, ...  
WO/2017/209974A1
A drone with a high-voltage trap seeks, identifies, pursues and destroys flying insects within a patrolling area. During its passive attracting mode, the drone lands on a designated ground site and attracts insects with light, sound, and...  
WO/2017/206081A1
A rubber band launching device. The rubber band launching device is mounted on an unmanned aerial vehicle and is used for launching a rubber band (30) to shoot down an enemy unmanned aerial vehicle in an air battle of unmanned aerial veh...  
WO/2017/208424A1
An attitude estimation device (30) is provided with: a data acquisition unit (32) which acquires observation data; a ranging point coordinates calculation unit (33A) which, using positioning data, ranging data, actual attitude data, and ...  
WO/2017/210595A2
Systems, devices, and methods for an aircraft having a fuselage (110); a wing (120) extending from both sides of the fuselage; a first pair of motors (132b, 133b) disposed at a first end of the wing; and a second pair of motors (142b, 14...  
WO/2017/204592A1
An unmanned aerial vehicle according to an embodiment comprises a rotary wing, a motor, and an arm body, and includes: a plurality of arm units detachably coupled to a body; the body having a plurality of receptacles to be coupled to the...  
WO/2017/202630A1
The invention relates to a modular aircraft comprising a base unit (2), formed by at least two buoyancy modules (4), at least one functional module (6), and at least one coupling device (8). At least one of the buoyancy modules (4) has a...  
WO/2017/205255A1
A stoppable rotor, which includes a first and second blade and rotates about a substantially vertical axis, is stopped with the first blade pointing forward and the second blade pointing backward while the aircraft is mid- flight. Anti-t...  
WO/2017/203793A1
According to the present invention, a body part is provided with: a plurality of motors; and a plurality of rotors corresponding to the motors. The rotors are driven by output from the corresponding motors. The rotational speed of each o...  
WO/2017/202223A1
Provided in the present application are an aircraft, a power unit and a power assembly thereof, wherein a power unit comprises a driving member, a propeller driven by the driving member, and an electric adjusting module connected to the ...  
WO/2017/197603A1
A multi-rotor unmanned aerial vehicle (100), comprising a main housing (10), a first rotor group (11), a second rotor group (12), and a third rotor group (13). The main housing comprises two end-face reference surfaces arranged oppositel...  
WO/2017/200609A1
The present disclosure pertains to self-piloted, electric vertical takeoff and landing (VTOL) aircraft that are safe, low-noise, and cost-effective to operate for cargo-carrying and passenger-carrying applications over relatively long ra...  
WO/2017/197602A1
A multi-rotor aircraft (100), comprising: a main aircraft assembly (10) comprising a first magnetic medium (13), a main housing (11), and a control motherboard accommodated in the main housing (11), the first magnetic medium (13) being p...  
WO/2017/200610A1
The present disclosure pertains to self-piloted, electric vertical takeoff and landing (VTOL) aircraft that are safe, low-noise, and cost-effective to operate for cargo-carrying and passenger-carrying applications over relatively long ra...  
WO/2017/199724A1
A propeller 16 includes: a hub 42; a plurality of blades 44 radially extending from the hub 42; and a guard 46 connected to the respective outer ends 58 of the plurality of blades 44. The guard 46 includes: a first member 60 consisting o...  
WO/2017/198082A1
Disclosed is an aerial vehicle, comprising an aerial vehicle body, mechanical arm components provided on the aerial vehicle body, and power apparatus provided on the mechanical arms. The power apparatus comprise corresponding driving ele...  
WO/2017/197601A1
An unmanned aerial vehicle capable of walking on the ground, comprising a main housing (11), a first rotor group (12), and a second rotor group (13). The first rotor group (12) and the second rotor group (13) are mounted on edge surfaces...  
WO/2017/198084A1
Disclosed is an aerial vehicle, comprising an aerial vehicle body, mechanical arm components provided on the aerial vehicle body, and power apparatus provided on the mechanical arm components. The power apparatus each comprise a mount ba...  
WO/2017/198248A1
Vehicle (1) comprising at least one rotor (3) which is driven by a driving device (2) and which includes at least two cylindrical rotor blades (4) that are mounted so as to be rotatable about the longitudinal cylinder axes (5) thereof by...  
WO/2017/197232A1
Aircraft isolator devices, systems, and methods for isolating a structural component within an aircraft can include an engine interface, airframe, and one or more (e.g., a plurality of) isolator devices attached to the engine interface a...  
WO/2017/197325A1
An unmanned aerial vehicle includes at least one rotor motor configured to drive at least one propeller to rotate. The unmanned aerial vehicle includes a data center including a processor; a data storage component; and a wireless communi...  
WO/2017/197316A1
An unmanned aerial vehicle includes at least one rotor motor configured to drive at least one propeller to rotate; a passenger compartment sized to contain a human or animal passenger; and a hybrid generator system configured to provide ...  
WO/2017/197239A1
An unmanned aerial vehicle includes multiple rotor arms; a rotor disposed at an end of each of the multiple rotor arms; and an adjustment component configured to enable a first rotor arm to move relative to a second rotor arm.  
WO/2017/197245A1
A solar power system comprising a solar panel, a load, and a battery pack group. The load comprising an electric motor operatively coupled with a propeller. The battery pack group comprises one or more voltage controllable battery packs,...  

Matches 1 - 50 out of 5,378