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Patent Searching and Data


Matches 51 - 100 out of 5,019

Document Document Title
WO/2017/175223A1
An apparatus for inflating balloons and permanently maintaining them in inflated state. The apparatus comprises a connector for connecting the balloon to air or gas supply source or stream, a one-way valve for allowing air or gas within ...  
WO/2017/154474A1
This flying object (10) comprises: a plurality of rotor units (30) each including a propeller (32) and a motor (33) that drives the propeller (32); a balloon (20) that covers the lateral sides of the plurality of rotor units (30) so as t...  
WO/2017/154520A1
This flying object (10) comprises: a plurality of rotor units (30) each including a propeller (32) and a motor (33) that drives the propeller (32); and a balloon (20) that is connected to the plurality of rotor units (30), and in which a...  
WO/2017/154473A1
This flying object (10) comprises: a plurality of rotor units (30) each including a propeller (32) and a motor (33) that drives the propeller (32); a plurality of shock absorbers including a first shock absorber (20a) forming a first gas...  
WO/2017/154551A1
This flying object (100) comprises: a plurality of rotor units (20) each including a propeller (21) and a motor (22) that drives the propeller (21); a plurality of balloons (30) respectively provided to the plurality of rotor units (20);...  
WO/2017/147716A1
A balloon holder and balloon holder base for holding a balloon having a tail, including a securing element having flexible biased opposing projections bounding an elongated channel opening, an elongate member insertable into an opening i...  
WO/2017/143365A1
A simple, lightweight, strong and rigid frame of multicopter comprising a central hub, a plurality of compression and a plurality of tension members attached to one another, forming altogether a three-dimensional polytope type shape. The...  
WO/2017/140189A1
A pump container comprises: a connector (1) having an inlet provided at one end thereof, and a tube insertion cavity at the other end thereof, wherein an inner end of the tube insertion cavity is communicated with the inlet; a hollow tub...  
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/2017/132436A1
A balloon inflation system includes a staged balloon pressure regulator having an override mechanism with an off position and an override position. When the override mechanism is in the off position, the staged balloon pressure regulator...  
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/2017/131834A2
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...  
WO/2017/125923A1
A multi-rotor system for providing air thrust is disclosed comprising at least one multi-rotor assembly. The multi-rotor assembly comprising at least two rotors rotatable about a common axis wherein the outer radius of a first rotor, is ...  
WO/2017/115668A1
As one embodiment of this motor, the motor is mounted in a multicopter and is provided with: a rotating section that rotates around a rotation shaft that extends in one direction; a stationary section that is attached to a main body sect...  
WO/2017/109603A1
Described herein is a cover (2) for a mobile device, in particular a smartphone or a tablet computer, whereby it comprises an aerial device (4) provided with camera (6), which is removably housed within a cavity (C) made in said cover. T...  
WO/2017/096478A1
An aerial vehicle is disclosed which includes a body and a multicopter. The body has at least one wing. The multicopter is rotatably mounted to the body about a multicopter axis. The multicopter includes a plurality of rotors positioned ...  
WO/2017/090851A1
The present invention relates to a technology for operating one or more external devices in association with a scenario-based content executed in a main device. According to an embodiment of the present invention, a system for associatin...  
WO/2017/085417A1
Drone (10) comprising a central body (1) and a plurality of arms, preferably at least three arms (B1, B2, B3, B4), each arm comprising a first end (21) mounted on the central body, each arm comprising, in the vicinity of a second end (22...  
WO/2017/087841A1
A vectored thrust control module for an aircraft that includes a servo system that couples to the aircraft structure at an output shaft connection point. A thrust motor assembly is fully supported by the servo system and rotates a bladed...  
WO/2017/081450A1
An airframe (10) for an air vehicle comprising an outer skin layer (12) and a support layer (13) defining a fuselage of said air vehicle, wherein said outer skin layer (12) is magnetically coupled to said support layer (13).  
WO/2017/075862A1
An inflatable flying disc, comprising an annular inflatable body (2). An inflating nozzle (5) is provided on the annular inflatable body (2). The inflating nozzle (5) comprises an air nozzle seat (6) in communication with the inner cavit...  
WO/2017/079411A1
Systems, apparatuses, and methods are provided herein for stabilizing an unmanned aerial system. An apparatus for stabilizing an unmanned aerial system comprises a ring member and a pair of attachment members each having a first end and ...  
WO/2017/071678A1
The invention relates to a device for the synchronous filling of water balloons, comprising at least one filling adapter (10) and a terminating element, characterized in that the filling adapter has a first end (A) and a second end (B) a...  
WO/2017/072385A1
The invention relates to a device for preventing birds from settling in an area, simply and efficiently, which comprises a support structure to which a kite moved by the action of the wind is rotatably couplable using joining means, the ...  
WO/2017/072517A1
A rotary-wing air vehicle comprising a main body (12) and at least two rotor devices (16a, 16b) arranged and configured to generate propulsion and thrust, in use, to lift and propel said air vehicle, said rotor devices (16a, 16b) being a...  
WO/2017/074754A1
An airborne drone training track includes both a ground track and a ceiling track. The ceiling track can be disposed above and be at least essentially aligned with the ground track. Airborne drone attachment tethers movably attach an air...  
WO/2017/067352A1
The invention relates to the field of data transmission. Provided are an information processing system, method and device. The system comprises: a first control apparatus (110); a first combat apparatus (120); a second combat apparatus (...  
WO/2017/065106A1
The purpose of the present invention is to provide a remote-control type unmanned aircraft and a control handover method for the remote-control type unmanned aircraft such that the control thereof can be smoothly handed over among multip...  
WO/2017/059275A1
A kite includes a frame including a leading edge support and a plurality of struts extending rearward from the leading edge support, a flexible main canopy attached to the frame and at least one flexible kite sizing section adjustably at...  
WO/2017/047546A1
The present invention is a method for controlling a multicopter by transmitting a first control signal and a second control signal from a controller operated by the operator toward a multicopter that performs an unmanned flight with a pl...  
WO/2017/043519A1
This balloon 1 is formed by joining two plastic films 10 and 12 together. The balloon 1 includes: a gas supply valve 6 which is sandwiched between and is joined to the first film 10 and the second film 12; a first chamber 14 which expand...  
WO/2017/035628A1
A toy projectile, a method of launching a toy projectile, and a kit for a toy projectile are described. A toy projectile comprising a projectile body having the general form of a rocket and a propulsion device defined within and extendin...  
WO/2017/035391A1
A ganged servo flight control system for an unmanned aerial vehicle is provided. The flight control system may include a swashplate having first, second, and third connection portions; a first control assembly connected to the first conn...  
WO/2017/032106A1
A method for beautifying an Ochroma model aircraft with a thermally-contracted skin comprises: printing a colored ink on a white skin using a UV flatbed printer to obtain a skin printed with a pattern; placing a wooden-structure frame of...  
WO/2017/028501A1
A propeller connection structure and an unmanned aerial vehicle. The connection structure comprises a motor rotor shell (1) and a propeller (2). The motor rotor shell (1) is provided with a connection part (11) for connecting the propell...  
WO/2017/030883A1
Reusable balloon multi-fill system. At least some of the illustrative embodiments are balloon multi-fill systems including a hose-end adapter, a plurality of hoses coupled to the hose-end adapter, and a plurality of balloon nipples coupl...  
WO/2017/027952A1
There is disclosed a balloon holder for holding a balloon having a tail and a tapered self-closing bladder. The balloon holder comprises a main body having a tail locking mechanism, an elongated member protruding from a bottom extremity ...  
WO/2017/026729A1
The present invention relates to an airplane formed by folding a plate-shaped base material, the airplane having a fuselage portion formed at the center thereof and having wings extending from both sides of the upper portion of the fusel...  
WO/2017/013840A1
This unmanned flight vehicle (10) comprises: a time measurement unit (101) that acquires the current time instant; a flyable range changing unit (112) that determines a flyable range of the unmanned flight vehicle (10) in accordance with...  
WO/2017/012515A1
Disclosed is an aerial vehicle, comprising an airframe (1), a propeller (2), shrouds (121, 31) and a drive mechanism (8), wherein the shrouds (121, 31) are arranged on the airframe (1) and are used to increase the lifting force of the ae...  
WO/2017/008107A1
A safety rotor system for an aircraft including a flight rotor that is rotationally driven by a drive, the system including: a safety rotor that is rotationally driven during rotation of the flight rotor, the safety rotor including one o...  
WO/2016/111715A3
Embodiments of a hand-launched solar-powered aircraft are disclosed. In addition, embodiments of kits are disclosed for the construction of a hand-launched solar-powered aircraft. Further, embodiments of methods of making a hand-launched...  
WO/2017/010019A1
[Problem] To configure the frame supporting an unmanned aerial vehicle so as to be lightweight and strong. [Solution] An unmanned aerial vehicle (1) is equipped with: an upper frame (10) that is formed by connecting, at intersection poin...  
WO/2017/000156A1
A double-blade tandem helicopter comprises a helicopter body (10), a power system, a control system, and two groups of rotors (30, 50). The two groups of rotors are vertically disposed relative to the helicopter body. Each group of rotor...  
WO/2017/000908A1
A remote control device for an aircraft and an aircraft system. The aircraft system comprises an aircraft (3) and a remote control device. The remote control device includes a first GPS chip (4), a magnetometer (5), a gyroscope chip (6),...  
WO/2016/204829A1
An apparatus for filling a plurality of containers with a fluid-additive mixture. The apparatus including a connector configured to removably couple the apparatus to a fluid source, a plurality of coupling elements, each coupling element...  
WO/2016/204828A1
An apparatus for filling a plurality of containers with a fluid. The apparatus including a connector having a coupling mechanism proximate to a first end of the connector, the coupling mechanism being configured to removably couple the a...  
WO/2016/197964A1
Provided are a rotor control device and a rotorcraft. The rotor control device comprises a servo apparatus (10) provided with a power main shaft (120), a power transmission assembly (20), a fixing frame (30), a first propeller (40) and a...  
WO/2016/198555A1
The present invention relates to a balloon (100) which can be internally illuminated, can be filled with propellant gas and is able to climb, comprising a lower (103) and upper (102) region during generic use, and having an interior spac...  
WO/2016/192249A1
A method and apparatus for manipulating an aerial vehicle. The method comprises the steps of: step I, perceiving a flight instruction input by a user via an input device of an intelligent terminal, wherein the flight instruction comprise...  

Matches 51 - 100 out of 5,019