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Matches 1 - 50 out of 1,594

Document Document Title
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....  
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...  
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...  
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...  
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 ...  
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...  
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...  
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...  
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...  
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...  
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...  
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/2017/148199A1
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...  
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...  
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...  
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...  
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/2017/132515A2
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/2017/128050A1
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/2017/132515A3
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/2017/127746A1
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
WO/2017/087515A8
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...  
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...  
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 ...  
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...  
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...  
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...  
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/2017/031452A1
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...  
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...  
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...  
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 (...  
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...  
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...  
WO/2016/205646A1
Various embodiments of the present invention relate to a multilayered structure and a method of making the same. Various embodiments relate to a balloon including the multilayered structure. In various embodiments, the present invention ...  
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/2016/195520A1
This invention concerns a multifunctional air transport system made up of: a manoeuvrable modular hybrid airship (1) of variable length and comprising a modular transport gondola (4), and electric lifting rotors (15) embedded in two pair...  
WO/2016/163794A1
The present invention relates to an aircraft management system connected to the ground, receiving power supplied from the ground, and controlled to be maintained at a certain position. The characteristic configuration of the system compr...  
WO/2016/160628A1
An atmospheric balloon descent system includes a system housing having a drogue chamber containing a drogue chute and a parachute chamber containing a parachute. The parachute coupled with the drogue chute with a drogue tether. A riser t...  
WO/2016/153720A1
A balloon system is provided including a balloon envelope, a payload secured to the balloon envelope, a first parachute positioned within a parachute container, the parachute container secured to the payload, a first bridle line having a...  
WO/2016/141484A1
A mobile artificial cloud system comprising a mobile formation of horizontally extending panels which are elevated above the ground for providing shade. The panels can take the form of gas-filled, flattened, large balloons, or sheets of ...  
WO/2016/109677A1
Disclosed herein is a lighter-than-air (LTA) device (5000) and method of making the same. In an embodiment, the LTA device (5000) may include a membrane (E, G_in, G_out) having a flexible substrate and an active material (525) disposed t...  

Matches 1 - 50 out of 1,594