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Patent Searching and Data


Matches 1 - 50 out of 702

Document Document Title
WO/2018/009229A1
An air and land multimodal vehicle comprises a frame, a propeller engine attached to a first location of the frame supplying power and torque to a propeller, a ground engine attached to a second location of the frame supplying power and ...  
WO/2018/000083A1
A control bar stopper includes a stopper body having a sleeved line receiving slip groove that allows sleeved line slippage. The stopper body has an underlying control bar bumper. A brake body is provided having a sleeved line receiving ...  
WO/2017/181260A1
A kite control bar having a tensioning member anchored to the bar end float and secured to the trim line. The tensioning member is capable of expanding and contracting. The tensioning member has a default state which is either an expande...  
WO/2017/184806A1
The airborne vehicle recovery method and apparatus enables radiosonde users to reliably recover launched radiosondes and provides new and unique opportunities for research and data acquisition with balloon launched radiosondes. Airborne ...  
WO/2017/165442A1
An apparatus comprising: a traveler connected to an elongate track; a stator comprising an elongate conductor spaced from the elongate track, a first ferromagnetic unit, and a second ferromagnetic spaced from the first ferromagnetic unit...  
WO/2017/147641A1
The present invention relates to a kiteboarding spreader. The sue spreader includes a base and a slide member extending from the base. A sliding fastener is provided for slidably fastening to the slide member and fastening to a kite. Adv...  
WO/2017/127413A1
A parafoil system having an adjustable trim angle during flight to control glide slope and descent speed of a parafoil is provided. The parafoil system may include a pulley cluster comprising first and second variable trim pulleys, each ...  
WO/2017/093618A1
The present invention relates to a single skin wing of the controllable type that is held by at least two lines at its ends. More particularly, it relates to a single skin wing, the leading edge (2) of which is provided with diagonals (8...  
WO/2017/046637A1
Tailed parachute-paraglider (10) comprising a first portion (A) of a substantially squared/rectangular shape with sides (11, 13) two by two substantially parallel and opposed, and a second portion (B) with trapezoidal shape, comprising a...  
WO/2017/042685A1
A device is disclosed; said device is capable of floating in the sky by means of the interaction of its surface with the wind, as in the case of a kite. The device features a plurality of cylinders linked together, with valves at their f...  
WO/2017/036587A1
The invention relates to a profile for a canopy, steered kite, kite or sail, consisting of a top sail and a bottom sail as well as of profile-forming profile ribs, the bottom sail of the profile not extending up to the profile trailing e...  
WO/2017/031945A1
Provided is a multi-shaft manned aircraft, comprising a machine frame (1), and a powered apparatus (4), transmission apparatus (42), rotor apparatuses (2), variable-pitch apparatus, seat (5), and control apparatus (6) mounted on the mach...  
WO/2017/021001A1
The invention relates to a canopy for a paraglider, parachute, flexkite, or surfkite canopy, consisting of an upper sail (12) and a lower sail (14), and of profile ribs forming a profile, characterised in that at least two separate press...  
WO/2016/200457A3
A rotary aerial vehicle (AV) includes an engine configured to rotate at least one rotor at a variable rotor speed, a full authority electronic microcontroller (FAEM) in electrical communication with the engine. The FAEM is configured to ...  
WO/2016/200407A1
A system enabling safe manned and unmanned operations at extremely high altitudes (above 70,000 feet). The system utilizes a balloon launch system and parachute and/or parafoil recovery.  
WO/2016/196831A1
A hardpoint relief pad (300) is described and includes a base surface (310), a hardpoint overlay (320), and a first stress relief area (330A). The base surface is configured to conform to and be fixedly attached to an interior surface (3...  
WO/2016/168918A1
A composite kite line for kite boarding which includes a high tensile strength inner load-bearing line encapsulated in a sheath which increases die composite kite line buoyancy.  
WO/2016/166256A1
The invention relates to an aircraft comprising a cockpit having at least two seats arranged laterally one next to the other and transversely to the direction of flight, a upwardly-pivotable cockpit hood which, when pivoted upwards, rele...  
WO/2016/128584A1
The invention relates to a paraglider (10) comprising a canopy (12) having a top sail (14) and a bottom sail (16), wherein the canopy (12) is subdivided into several elongated chambers (18) having a longitudinal axis. Each chamber (18) h...  
WO/2016/076727A1
There is disclosed a sail for producing propulsive power or lift in a fluid, where the sail comprises a first layer and a second layer where the first layer and the second layer are connected along at least one corresponding side, and th...  
WO/2016/075461A1
A kite for use in a system for extracting energy from the wind comprises: a wing (1) having a roll neutral point or zone when the kite is in flight; a tether (4) coupled directly or indirectly to the wing; a rigid spar arrangement (2); t...  
WO/2016/055784A1
A kite (100) comprises: a wing (101); upper (102B) and lower flaps (102A) located along at least a portion of an edge of the wing that forms the trailing edge of the wing when the wing is active; a controller (200) configured to generate...  
WO/2016/012695A1
The invention concerns an airborne device (10) comprising at least three supporting wings (12) and a linking device (18), the wings being linked to each other by first flexible cables (16), each wing being further linked to the linking d...  
WO/2015/198141A9
The present invention relates to a flight-capable wing construction which may be driven by wind and which comprises: a tethering line which is designed to connect the wing construction to a base station during operation, wherein one end ...  
WO/2015/198141A1
The present invention relates to a flight-capable wing construction which may be driven by wind and which comprises: a tethering line which is designed to connect the wing construction to a base station during operation, wherein one end ...  
WO/2015/160697A1
A vehicle-based airborne wind turbine system having an aerial wing, a plurality of rotors each having a plurality of rotatable blades positioned on the aerial wing, an electrically conductive tether secured to the aerial wing and secured...  
WO/2015/150470A1
The invention relates to a tethered aircraft and the control of such tethered aircrafts, for example for use in Airborne Wind Energy (AWE) applications. Tethered aircrafts can use bridles (15) distributed along the span-direction to impr...  
WO/2015/113148A1
A method for monitoring air pressure in a kite when kite boarding is described. The method involves a first step of connecting an air pressure sensor to one or more bladders of the kite. The method involves a second step of positioning a...  
WO/2015/116015A1
An inflatable vertical takeoff and landing aircraft intended for individual use, in which lift is generated by a rotor, wherein deflectors which deflect the airflow from said rotor compensate for the reaction torque arising from the rota...  
WO/2015/107556A1
An arc-type wing (1) is described, connected to at least one pair of power ropes (2) through at least two pairs of control bridles, each one of such pairs being composed of at least one front bridle (21) and of at least one rear bridle (...  
WO/2015/094851A1
An example method may include determining a drag force of an apparent wind on an aircraft that is coupled to a ground station via a tether. The method also includes determining a trajectory of the aircraft to a point downwind of the grou...  
WO/2015/083189A1
An arc-shaped wing (1) with differentiated wing profiles is described, composed of a section of central arc (11) and two lateral shoulders (12), wherein such central arc (11) is composed of a first wing profile (2) and each one of such s...  
WO/2015/039056A1
A method may involve operating an aerial vehicle in a hover-flight orientation. The aerial vehicle may be connected to a tether that defines a tether sphere having a radius based on a length of the tether, and the tether may be connected...  
WO/2015/037026A1
An arc-type wing (1) with high aerodynamic efficiency is described, composed of a central arc section (13) connected to pairs of bridles (11, 12) through a pair of shoulders (14, 15); each shoulder (14, 15) supports a panel (2) equipped ...  
WO/2015/037025A1
A method is described for real-time determining the shape of an arc-type wing (1) with high aerodynamic efficiency, wherein the wing (1) is composed of a central arc section (13) connected to pairs of bridles (11,12) through a pair of sh...  
WO/2015/032652A1
The method according to the invention for controlling a flying object (2, 20) having a stiff airfoil ( 21 ) and being controllable by means of a roll movement for carrying out lateral turns, with which the flying object (2, 20) is connec...  
WO/2015/025990A1
Aeropedalplane (2), of the present invention is a cycling Aircraft, which uses a double cycling system. The essential segments of the installation include, the double cycling system, twin arm gearbox (12), transmission gearbox (14), tran...  
WO/2015/012762A1
A flying boat 10 comprises a flying part 1 1 adapted to float on a body of water 12 and fly through air, and a propulsion unit 13 which is separate from the flying part 1 1. The propulsion unit 13 being adapted to float on the body of wa...  
WO/2014/118413A1
The invention relates to an improved kite of the type commonly used for kitesurfing, comprising a laminar surface (1) defined by a leading edge (2) and a trailing edge (3), and a frame (4) equipped with a leading profile (4a) and a plura...  
WO/2014/055044A1
Paramotor with dynamic torque compensation comprises of frame (1), harness or seat (2), engine and propeller (3) rotating in a cage (4) characterized by one or more surfaces placed on said frame and/or said cage in such a way that when a...  
WO/2014/020596A1
An unmanned aerial vehicle having a task to be fulfilled, the unmanned aerial vehicle comprising: a rechargeable energy storage unit; a propulsion arrangement configured to operate in at least two operative modes; a direction control arr...  
WO/2014/016901A1
The purpose of the present invention is to provide a double-layered flexible wing that allows a wing of a paraglider, etc. to be prevented from being unexpectedly deformed and further allows the wing to quickly recover and to be easily o...  
WO/2014/009931A1
A parachute device is provided with a bag containing a main parachute and a reserve parachute and with a propulsion assembly (14) having a frame (15) to which two arms (16) are coupled; the two arms can be opened laterally by operating a...  
WO/2013/186009A1
The invention relates to a hybrid aircraft (F). According to the invention, a suitable position for mounting an energy generation unit (14) in the aircraft is identified, said energy generation unit comprising an internal combustion engi...  
WO/2013/166596A1
A safety system for a traction kite comprises a central load bearing line and sliding control bar arrangement comprising a connection loop for connection to a harness hook, a system hub connecting the loop to the central load bearing lin...  
WO/2013/142949A1
A massive de-powering system for a kite wing used in kite boarding comprises a deflation control line that connects to a valve on the kite wing's leading edge bladder. In the preferred embodiment, disengaging the tether line from the har...  
WO/2013/140329A3
A hollow kite control bar is provided with means for sliding access to the bar for one or multiple lines or groups of lines. Each line has one end towards the kite and the other towards the bar. The length of each line between the kite a...  
WO/2013/140329A4
A hollow kite control bar is provided with means for sliding access to the bar for one or multiple lines or groups of lines. Each line has one end towards the kite and the other towards the bar. The length of each line between the kite a...  
WO/2013/140329A2
A hollow kite control bar is provided with means for sliding access to the bar for one or multiple lines or groups of lines. Each line has one end towards the kite and the other towards the bar. The length of each line between the kite a...  
WO/2013/114342A1
A system for reducing interference drag on an aircraft 40 during flight comprises an air intake opening 42 defined in the aircraft in a region of a wing-root 28 of the aircraft. The air intake opening is preferably provided in the fusela...  

Matches 1 - 50 out of 702