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WO/2018/081904A1 |
An aircraft comprising a hydrogen-containing envelope, a water-collection system for collecting water from the envelope, an electrolyser to convert the water collected using the water-collection system into hydrogen, and a hydrogen-reple...
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WO/2018/081879A1 |
The present invention relates to a tethered aerial system comprising its own means for generating electrical energy, preferably a fuel cell, for powering on-board electronics. In addition, the present invention describes a tether cable (...
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WO/2018/077806A1 |
A lighter than air vehicle with a hull, a laminate for such hull and a method of production of such laminate A lighter-than-air vehicle comprising a hull of a laminate material with a reinforcing fibre layer, for example Zylon®, and a f...
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WO/2018/076779A1 |
An adhesive comprises an adhesive body and graphene. The weight percentage of graphene in the adhesive is 0.2-1%. Graphene is added in the adhesive body so that graphene is dispersed in the adhesive body. Graphene has a good helium block...
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WO/2018/077805A1 |
A lighter than air airship (1) comprising a gas-filled flexible hull (2) which is elongate with a longitudinal axis (1') and with a front end (4) and a rear end (5), wherein a harness-structure (3) is abutting an outer side of the hull (...
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WO/2018/075632A1 |
Embodiments disclosed herein enable routine autonomous execution of at least some major phases of aerostat operation in response to commands from human or automated external operators, a built-in decision-making capacity, or both. Variou...
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WO/2018/072479A1 |
The present invention relates to an anchoring system for a tethered balloon, comprising: an anchoring frame having a first support arm (41) and a second support arm (42), the two support arms being used for supporting the anchoring frame...
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WO/2018/070067A1 |
A projection system (100) according to the present disclosure is provided with: a flying object (1); a projection device (10); and a control unit (30). The flying object (1) has: an exterior body; a flying device (3) that causes the exte...
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WO/2018/059058A1 |
Disclosed is a landing control method for an aerostat, comprising sending a landing signal to the aerostat by means of a controller; a capsule body of the aerostat starting to discharge air to make the aerostat start to land until the la...
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WO/2018/057034A1 |
A UAV includes a fork lift system and a length component. The forklift system includes one or more elongated members extending at least partially in a horizontal direction. The forklift system also includes an extension mechanism configu...
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WO/2018/009101A1 |
The invention relates to search and rescue means for indicating the location of an aircraft. A signalling device for indicating the site of an aviation accident comprises a balloon adapted for filling with a gas that is lighter than air....
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WO/2017/213308A1 |
The present invention provides a flight vehicle operating method comprising the steps of: (a) flying a flight vehicle in the direction toward a mooring portion located under the flight vehicle; (b) mooring the flight vehicle at the moori...
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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...
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WO/2017/202146A1 |
A valve assembly for an aerostat and an aerostat. The assembly comprises a valve (1) with a valve opening (7), and a valve disc (2). The valve disc can move relative to the valve (1) to cover or open the valve opening (7). At least one o...
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WO/2017/197996A1 |
A covering. The covering comprises a protective layer (1) and a load bearing layer (3) that are disposed in a stacked manner, and comprises a smart unit (21). The smart unit (21) is disposed between the protective layer (1) and the load ...
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WO/2017/198001A1 |
A method for flying a large balloon comprises the following steps: S1, flatten a balloon capsule (10) on a flying site (20), connect one end of the balloon capsule (10) to one end of a thread (30), and fix the other end of the thread (30...
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WO/2017/200803A1 |
An energy efficient and lighter-than-air high altitude platform (HAP) is disclosed that allows for sustained station keeping at high altitudes of about 50,000-80,000 feet for prolonged periods of time. The HAP includes an aerodynamically...
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WO/2017/185958A1 |
An aerostat launching system, comprising: an auxiliary balloon connected to an aerostat (60) to be launched to hang the aerostat (60); and a support (30) used for suspending a nacelle (62) of the aerostat (60). The aerostat launching sys...
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WO/2017/185139A1 |
The present invention relates to a wireless communication system for controlling one or more remote automated mining assets. The system includes a high-altitude platform including at least one high altitude communication apparatus, and f...
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WO/2017/164736A1 |
A balloon (1) has a gas-filled bag (3), as well as a number of displays (5) which are present on the outside of the bag. The balloon (1) further has a frame (9) which is present on the outside of the bag and which defines a holding volum...
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WO/2017/154010A1 |
An airborne device for surveillance of an enclosed area, comprising a platform having illuminating imaging devices, and an attached lighter than air balloon. A vertically aligned rotor provides additional lift, a rotor directed along the...
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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...
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WO/2017/148199A1 |
The present invention provides a graphene-modified polyurethane composite, a polyurethane adhesive prepared from same, a method for preparing the polyurethane adhesive, and an aerostat having the polyurethane adhesive. The composite comp...
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WO/2017/139283A1 |
Described herein are features for a high altitude lighter-than-air (LTA) system and associated methods. A zero-pressure balloon (ZPB) is attached in tandem with one or more variable ballast air super-pressure balloons (SPB). The ZPB prov...
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WO/2017/136906A1 |
This invention patent is aimed at innovating personal locomotion by free uni-steerable flight with new technologies using clean propulsion energies. The invention is characterised by a new concept of individual aerial locomotion, innovat...
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WO/2017/135485A1 |
The present invention provides an unmanned aerial vehicle comprising: a body part having an inner space filled with a particular gas; and a plurality of wing parts mounted on the body part and providing a propelling force, wherein each o...
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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...
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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...
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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', ...
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WO/2017/127746A1 |
Described herein are features for high altitude lighter-than-air (LTA) balloon antenna systems and associated methods. One or more long wire communications antennas may be built into the balloon skin. The antenna may extend under, in, on...
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WO/2017/125820A1 |
A system for elevation control. The system comprises a substantially gastight envelope containing lifting gas wherein the envelope further comprises a plurality of envelope segments in fluid communication with one another. At least one t...
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WO/2017/114370A1 |
Provided is a hydrogen ion gas-filled aircraft composed of a multi-stage telescopic cylinder, a sealed container, a light source, an electric field and a propeller. The cylinder is made of plastic, and is connected to the sealed containe...
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WO/2017/107781A1 |
A multi-rotor air vehicle comprises an airbag and a multi-rotor system. The airbag comprises an airbag body (300) and an internal space surrounded by the airbag body. The airbag is of a shape of a flat plate where the center is thicker t...
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WO/2017/105657A1 |
Techniques are disclosed relating lighter-than-air aircraft. Such aircraft may be used for various purposes, such as providing network connectivity to areas that would otherwise lack such connectivity. For example, in some embodiments, a...
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WO/2017/101735A1 |
An exhaust assembly for an aerostat, and an aerostat provided with said exhaust assembly, the exhaust assembly comprising a valve base (2) having a valve port (1), and a valve cover (3) able to selectively cover the valve port (1), and a...
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WO/2017/100055A1 |
An example computer-implemented method involves determining that an aerostat is located within a first atmospheric layer. A first wind-velocity measure is indicative of wind velocity in the first atmospheric layer. The method also involv...
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WO/2017/095505A1 |
An aerostat system including an aerostat and a tether. One end of the tether is attached to the aerostat and the other end of the tether is configured to be attached to ground handling equipment, such as a reel apparatus. The aerostat sy...
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WO/2017/087515A1 |
A control system for a tethered aerostat is provided, where at least one rotational and at least one translational degree of freedom are controlled to setpoints through the variation of tether lengths by an actuator system. The term teth...
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WO/2017/081406A1 |
The invention relates to an aircraft (10) which comprises: a balloon (100) extending between two side ends (101, 101') of said balloon, said two side ends of the balloon defining an axis R of said balloon; connection means (110) comprisi...
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WO/2017/075678A1 |
An unmanned and remotely controlled aircraft is formed by a multirotor system combined with an inflatable casing. The aircraft can lift or be powered by a power system comprising comprising three or more rotors. In some embodiments, the ...
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WO/2017/067412A1 |
A multi-rotor aircraft comprises: an airbag, comprising a bag body (510); a multi-rotor system, comprising a main support (520) located in an internal space of the airbag, a plurality of motors (550) and a plurality of propellers (560) w...
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WO/2017/069331A1 |
The present invention relates to a hydrogen recycling flight system and flight method and comprises: a flight fuselage having at least one pair of wings at both sides of the fuselage; a hydrogen gas balloon air-tightly connected to the f...
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WO/2017/059545A1 |
A geostationary platform is held afloat by a superpressure balloon. A suitable altitude is 25 km. The craft carries electrohydrodynamic thrusters, to overcome winds, held within a scaffold. Sensors determine position, velocity, accelerat...
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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/2017/031452A1 |
An atmospheric balloon includes an upper apex and a lower apex and a balloon membrane. The balloon membrane includes a plurality of balloon gores. The balloon gores extend between the upper and lower apexes. One or more of the balloon go...
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WO/2017/027939A1 |
The present invention relates to a process of using an aerostat, more specifically an airship with air staff and with an air framework to solve the current problems in electric energy transmission system. Such problems are related to the...
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WO/2017/022209A1 |
A flying body equipped with: a plurality of rotor units (30) which each have a propeller (32) and a motor (33) driving the propeller (32); a cushioning body which extends across the vertical height of the plurality of rotor units (30) an...
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WO/2017/017411A1 |
Disclosed in a lighter than air vehicle comprising a first envelope (34), a second envelope (36) located inside the first envelope (34), and a tube (40) connecting the first envelope (34) to the second envelope (36). The first envelope (...
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WO/2017/017410A1 |
Disclosed is a lighter than air vehicle comprising: an envelope (34) containing a lighter than air gas (22), at least part of the envelope (34) admitting the passage of light (28) through the at least part of the envelope (34); and means...
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WO/2016/204180A1 |
[Problem] To provide a buoyant flying body such that the risk of crashing can be reduced in order to ensure a high level of safety, and motion control can be facilitated by reducing the influence of wind in order to exert a high level of...
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