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Patent Searching and Data


Matches 701 - 750 out of 58,546

Document Document Title
WO/2017/132794A1
A rectangular unmanned aerial vehicle arm, comprising an arm body (1), the arm body being elongated and having a rectangular cross-section, and the interior being a hollow structure; the top and bottom surfaces of the arm body each have ...  
WO/2017/136568A1
An atmospheric balloon assembly includes a balloon shell extending between upper and lower apexes. The balloon shell includes a plurality of shell gores, each of the shell gores includes first and second shell edges extending between the...  
WO/2017/132990A1
A multirotor aircraft (10) comprises a body (12) comprising a main body (122) and a camera assembly (124) with a camera coupled to the main body (122); a frame (14) connected to the body (12), comprising a multirotor propulsion system (1...  
WO/2017/132982A1
A rotor unmanned aerial vehicle comprises a power device (10), a propeller assembly (20), a cradle head assembly (30), and a machine body frame (40). The propeller assembly (20) comprises a central fixed shaft (21), a mounting frame (22)...  
WO/2017/132804A1
An unmanned aerial vehicle damping device, comprising two struts (1) and a plate (2) used to mount a UAV. Each strut (1) is provided with at least two corresponding clamps (3) which clamp onto the strut (1). The device further comprises ...  
WO/2017/134459A1
The present invention aims to provide a modular jet trainer aircraft (1) which can be reconfigured to provide a plurality of different handling aircraft which will be particularly beneficial in the training of pilots. For example, the pr...  
WO/2017/136063A1
An apparatus for biological control of agricultural pests and for reducing damage to crops. The apparatus includes a container for holding biological organisms or material. The container also includes first and second ends and an opening...  
WO/2017/134901A1
The objective of the present invention is to retain an aircraft panel in an appropriate shape and ensure the shape accuracy required in a production process in combination with a holding jig, and thereby to simplify the structure of a ho...  
WO/2017/132833A1
An electronic speed control (100), a control method thereof, a control system thereof, a power assembly adopting the same, and an unmanned aerial vehicle. The control method comprises: acquiring status information of a motor (200) and/or...  
WO/2017/132807A1
An unmanned aerial vehicle pesticide tank, comprising an inverted cone-shaped tank (1) used to store pesticide liquid, a cavity (10) used to mount a pump (2) being provided on the top surface of the tank (1), the inner wall of said cavit...  
WO/2017/134902A1
The objective of the present invention is to simplify the structure of a holding jig that retains the shape of an aircraft panel and retain the aircraft panel in an appropriate shape. This holding jig (1) is provided with a plurality of ...  
WO/2017/132796A1
A multirotor aircraft (10) and a method for controlling the multirotor aircraft (10) are disclosed. The multirotor aircraft (10) comprises a body (12), a H-shaped frame (14), a first person view camera and a servo mechanism (121), wherei...  
WO/2017/133302A1
A manned aerial vehicle, comprising a cockpit (1) and a bottom cabin (2). The cockpit (1) has an accommodating cavity capable of carrying a person; the bottom cabin (2) is disposed below the cockpit (1) and is fixedly connected to the co...  
WO/2017/134659A1
There is provided an aerial platform comprising a spraying module, one or more actuators operatively coupled to the spraying module, at least a sensor for acquiring data indicative of altitude, wherein at least a controller is configured...  
WO/2017/132805A1
The present invention relates to a unmanned aerial vehicle electronic speed controller (ESC) heat dissipation device. The device comprises an arm (1), an ESC (2) being provided internally at one end of the arm (1), a rotor being provided...  
WO/2017/134223A1
The invention relates to a transport means, having an outer element (1, 31, 32, 33, 34, 63) and an inner element (3, 67) arranged within the outer contour of the outer element, wherein the inner element has a drive device having at least...  
WO/2017/136316A1
Some embodiments described herein relate to a wing that is coupled to a body of a vehicle and configured to rotate forward from a deployed configuration, in which the wing extends from the body to a retracted configuration in which a tip...  
WO/2017/135371A1
A multicopter having a radar mounted therein is provided. A multicopter includes: a plurality of motors to respectively rotate three or more rotors; and a radar system to transmit and receive a signal wave and detect a target by using th...  
WO/2017/134797A1
A moving object guidance device characterized by comprising: a detection signal generating unit 99 that generates a detection signal for detecting a moving object 200; a first antenna 3 that radiates the detection signal in a space as a ...  
WO/2017/136650A1
A new system and apparatus for detachably joining a first component to a second component is disclosed, along with a method for detachably joining two components. Embodiments of the present invention include a tensioning apparatus and sy...  
WO/2017/134338A1
The invention discloses a waitressing drone that brings drinks to people at the restaurant, and the orders are identified from the Facebook photo of the user, that the drone displays when making the delivery. The invention facilitates th...  
WO/2017/134899A1
The objective of the present invention is to provide an aircraft panel production method and aircraft panel production system with which an aircraft panel can be assembled accurately. This aircraft panel production method has: a step in ...  
WO/2017/128797A1
A fixing support (100, 300, 500), used for connecting to a head (60) or a load and a carrier carrying the head (60) or the load. The fixing support (100, 300, 500) comprises a fastening component (30, 30a, 30b) and a clamping component (...  
WO/2017/130137A1
A stratospheric drone able to operate at an altitude between 17 km and 23 km(ISA), said stratospheric drone comprising: one fuselage; at least two wings; at least one tail;at least two motors and two corresponding propellers; at least on...  
WO/2017/128113A1
Power supply control circuitry comprises: a capacitive load circuit (11), a switch circuit (12), and a time delay control circuit (13). The capacitive load circuit (11) and the time delay control circuit (13) are connected in parallel be...  
WO/2017/128052A1
An unmanned aerial vehicle and an electrical motor control chip and an electronic governor thereof. The electrical motor control chip comprises: an encapsulation case (11), an analogue peripheral circuit (21) encapsulated in the encapsul...  
WO/2017/129536A1
The invention relates to an aircraft wing. The wing comprises a movable flap which is able to move in rotation relative to a fixed central body, flexible piping (40) and a rail (30) for guiding the movable flap and the flexible piping (4...  
WO/2017/128742A1
A propeller (9), a power component and a flight vehicle, wherein the propeller (9) comprises a hub and a blade connected to the hub; at the distance of a second threshold from the propeller disk center (1), the blade has an angle of atta...  
WO/2017/129137A1
Provided are a gimbal of an unmanned aerial vehicle and a bearing support thereof. The bearing support (5) comprises: a fixed base (50) and a pressing plate (51). The fixed base (50) comprises a base (501), a first rotating support (502)...  
WO/2017/127931A1
An inlet guide assembly for a turbine receiving a pulsed flow, including a duct having an internal volume, and an inlet port, first outlet nozzle and second outlet nozzle each communicating with the internal volume. The inlet port is con...  
WO/2017/131284A1
The present invention relates to a joined-wing type unmanned aerial vehicle. More specifically, the present invention relates to a joined-wing type unmanned aerial vehicle comprising: a fuselage; main wings formed on opposite sides of th...  
WO/2017/129223A1
The invention relates to a free fall simulator comprising a closed air circuit, an air duct (10) that includes a flight chamber (11) in which persons can remain suspended in the air as a result of an upward vertical air flow, a lower ope...  
WO/2017/128744A1
A propeller, power assembly, and aircraft. The propeller comprises a blade fastener (1) and a blade (2) connected to the blade fastener (1). At a location having a distance of 55% of a radius of a propeller disc defined by the propeller ...  
WO/2017/132305A1
An aeronautical car comprises a ground-travel system including at least one traction device, an air-travel system including at least one flight mechanism configured to be selectively moved between a first position when the aeronautical c...  
WO/2017/132515A2
Some embodiments described herein relate to an aircraft that includes a support frame, at least one gas compartment, and multiple propulsion units. The gas compartment(s) can be coupled to the support frame and configured to contain a ga...  
WO/2017/132304A1
A weather modification system that includes both systems and vehicles capable of modifying the weather. The systems may include devices capable of utilizing compositions to create dispersants that can modify weather. The system is capabl...  
WO/2017/128050A1
Provided is an unmanned aerial vehicle (100, 200, 300, 400), comprising a body (10) and a multi-lens camera module (20). The multi-lens camera module comprises at least two camera units (21, 21', 21'', 21'''). The camera units (21, 21', ...  
WO/2017/130181A1
A landing platform for a hovering vehicle comprises an erectable and retractable boundary element which, when in erected position, defines a substantially closed volume.  
WO/2017/132515A3
Some embodiments described herein relate to an aircraft that includes a support frame, at least one gas compartment, and multiple propulsion units. The gas compartment(s) can be coupled to the support frame and configured to contain a ga...  
WO/2017/128313A1
An arm structure (20) for an unmanned aerial vehicle (1). The arm structure (20) comprises an arm upper cover (21) and an arm lower cover (22). The arm upper cover (21) has a distal end portion that is provided with a motor mounting port...  
WO/2017/131427A1
An electronic device and a method for displaying an image transmitted by a robot and remotely controlling a movement of the robot are provided. The electronic device includes a communicator, an inputter, a display, and a controller. The ...  
WO/2017/128782A1
Disclosed are a gimbal and an unmanned aerial vehicle. A free end of a first connecting arm (11) of the gimbal is connected to a Yaw shaft (21), and a gripping end is close to a second connecting arm (12). Parts of the first connecting a...  
WO/2017/129661A1
The invention relates to a curable resin that represents an excellent substitute for phenolic resins and is therefore able to replace phenolic resins in all applications in which they are used. Said resin is characterised in that it comp...  
WO/2017/129960A1
A method and apparatus are provided for detecting defects in a solar panel array (20), using an unmanned aerial vehicle (UAV) (10). The UAV (10) has mounted thereon a pyranometer (12), a GPS receiver (13), a thermographic camera (14), a ...  
WO/2017/129930A1
A moving wing aerial vehicle is rendered collision tolerant by a cage (8) of generally spherical shape, which envelopes the lift assembly. The cage (8) is formed including an annular equatorial track (14). Spokes (2,3) extend from the li...  
WO/2017/131834A3
A pivoting wing system, capable of vertical take-off and landing, having a hub connected to one or more wings provided on a spanwise axis. The wings are further provided with one or more thrust producing devices mounted to the top and bo...  
WO/2017/129692A1
The invention relates principally to a stop (30) for an aircraft seat, which stop is designed to be installed on a rail (16), said rail (16) having, in alternation, bearing regions, in which two lips that are oriented toward one another ...  
WO/2017/130653A1
A mobile unmanned mobile body (8) for inspecting an object to be inspected, the unmanned mobile body (8) being provided with: an inspection device (14) for inspecting the object to be inspected; a wire (16) extending toward the object to...  
WO/2017/128062A1
Methods and systems for reducing a delay in adjusting an attitude of a multidimensional gimbal in response to state information of a payload are provided. At least one ESC unit may be provided together with the IMU to reduce a time requi...  
WO/2017/131834A2
A pivoting wing system, capable of vertical take-off and landing, having a hub connected to one or more wings provided on a spanwise axis. The wings are further provided with one or more thrust producing devices mounted to the top and bo...  

Matches 701 - 750 out of 58,546