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WO/2019/106342A1 |
A canopy (1) control system comprising: • a yoke (5), configured to be pivotably securable to a vehicle (2) and securable to a line system (6) of a canopy (1) in use, such that the yoke pivots with respect to the vehicle in a first dir...
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WO/2019/108686A1 |
Systems and methods are disclosed for implanting a dual-kite aerial vehicle including a first kite apparatus, a second kite apparatus, and a tether extending between the first and second kite apparatuses. In particular, the disclosed sys...
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WO/2019/056077A1 |
The utility model relates to the bicycle equipped with a wing and a propulsion system for flight, pertaining to the technical field of driver-propelled wheeled vehicles, more specifically those vehicles with additional propulsion means. ...
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WO/2019/044125A1 |
This flying body comprises: a fuselage; a canopy capable of adjusting the speed of a fall when falling; a brake cord having one end connected to the canopy; a winding device (20) which is provided on the fuselage and allows the other end...
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WO/2019/039062A1 |
A flight vehicle safety device (100) is equipped with a safety mechanism (10), a drive mechanism, an ejection mechanism, and a control mechanism. The safety mechanism (10) is used to ensure the safety of a flight vehicle (30) and/or an o...
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WO/2019/039063A1 |
A flight vehicle safety device (100) is equipped with a deployable body (10), an ejection mechanism, a bag-shaped member (50), and a gas generator. The deployable body (10) is wound or folded in an undeployed state, and generates dynamic...
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WO/2019/002511A1 |
The invention relates to a structure (100) of a kite (10) comprising a leading edge (110), a trailing edge (120), at least one first batten (30) extending substantially perpendicularly relative to the leading edge (110), a canopy (140) e...
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WO/2018/218370A1 |
Disclosed is an aircraft and a method of controlling an aircraft. The aircraft comprises a continuous wing assembly extending from port to starboard sides of the aircraft. The aircraft is controlled partially by flexing portions of the w...
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WO/2018/213920A1 |
A multi-layer bladder construct consisting of a non-stretchable outer covering and a stretchable inner bladder. The outer covering has an inner surface and is made from woven polymer fibers having a warp direction and a weft direction. T...
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WO/2018/193143A1 |
A flying object with an aerial advertising device can be towed from the ground or tied to a fixed point and comprises an element (1) for lifting and keeping the device in the air, which acts as an advertising medium made of lightweight a...
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WO/2018/190319A1 |
The flight vehicle (1A) is provided with: a lift-generating member (1110) disposed on an airframe (1201) in a deployable manner; manipulation mechanisms (1111, 1112), which are connected to the lift-generating member (1110) and are for m...
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WO/2018/188472A1 |
Disclosed are a high-efficiency device for generating a controllable lifting force, wherein same is able to supply a lifting force for gear lifting parachutes, and a use method. The device comprises a load frame (5), a switchable rope qu...
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WO/2018/158576A1 |
One type of kite system for the extraction of energy from the wind includes a kite connected to a base unit using a tether. The kite system comprises: an anhedral wing having wing tips and a central part located vertically higher than th...
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WO/2018/158575A1 |
A kite having multiple sections for use in a power-generation system, the kite comprising a top panel and a bottom panel, and at least one rib connection piece extending between the top panel at a first end and the bottom panel at the se...
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WO/2018/154603A1 |
The present subject matter relates to an apparatus (100) that use of a tuft of numerous wires as a drag enhancing system for spacecrafts (102). When these ultra-thin wires are used in high numbers and deployed on-board a spacecraft, they...
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WO/2018/140050A1 |
A vehicle charging system comprises a vehicle computer programmed actuate a vehicle charger to receive electricity from an aerial drone. Actuation of the vehicle charger is performed in response to determining the aerial drone has landed...
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WO/2018/102119A1 |
Offshore airborne wind turbine systems with an aerial vehicle connected to an undersea anchor via a tether arc disclosed. A floating landing platform may be coupled to the tether and be dragged along the surface of the water along with t...
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WO/2018/074948A2 |
The invention relates to aeroplanes, rockets, spacecraft and any type of flying object (FO). Side wings are mechanically fastened to the body of an FO from the outside. The wings are perpendicular to the axis of the FO when viewed from t...
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WO/2018/053813A1 |
A powered device and an aerial wing outfit with a powered device. The invention comprises a control adjuster (8), and a highly oxygenated water storage chamber (1), catalytic reduction chamber (9), and jet propulsion compartment (3) conn...
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WO/2018/050145A1 |
The invention relates to a flying or sliding element (10) with an outer skin (12), comprising a front element (14, 190) and at least one sail (24, 50, 50', 199, 212, 214, 216, 236, 238), said front element (14, 190) and/or one or more ad...
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WO/2018/046806A1 |
The invention relates to a control device for power kites. It consists of a tall Y-shaped structure (1), the base of which is connected to the center of a horizontal control bar (3) arranged perpendicular to the structure (1). An articul...
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WO/2018/028956A1 |
The present disclosure relates to a remote sensing system, comprising: an air towable housing for carrying one or more sensors, the air towable housing and/or a comprising at least a first pulley.
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WO/2018/020500A1 |
System for automated landing of an airborne body suspended on a parawing comprising a case with powered pulley driven by a controlled motor to extend and extract cables attached to a parawing. The cables are extended at the beginning of ...
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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 ...
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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 ...
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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...
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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 ...
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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...
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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...
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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 ...
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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...
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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...
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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...
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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...
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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...
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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...
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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.
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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...
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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.
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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...
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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...
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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...
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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...
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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 ...
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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...
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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...
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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...
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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...
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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...
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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...
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