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Matches 1 - 50 out of 1,634

Document Document Title
WO/2018/163991A1
Provided is a wireless relay system with which it is possible to quickly start relaying wireless communication between a stationary base station and a user device after moving to a target position. The wireless relay system is provided w...  
WO/2018/147535A1
Provided is a wind power generation system using a jet stream, implemented by including: an aerial vehicle flying in the air without a winch so as to produce electric power through wind power generation while performing an autonomous fli...  
WO/2018/141072A1
An inflatable, amphibious landing gear comprising one or more inflated pontoons with wheels attached and with one or more air bladders below each inflated pontoon. When the air bladders are inflated, they extend below the wheels and prov...  
WO/2018/139982A1
A hybrid airship such as an unmanned drone or UAV (10, 110, 210) capable of significantly extended flight times can use one of two technologies, or both together. The first technology uses a combination of a lifting gas (such as hydrogen...  
WO/2018/138112A1
The invention relates to a flying craft (8, 98, 298, 308, 318) comprising lighter than air gas in a receptacle for creating a lifting force by means of buoyancy and a thrust force by combustion in combustion engine as a fuel together wit...  
WO/2018/135383A1
The purpose of the present invention is to provide a buoyant-type flying body with which it is possible to inhibit deformation of the outer shape or breakage of a buoyant body. A buoyant-type floating body 1, 100, 100A provided with a bu...  
WO/2018/129880A1
Provided are an aerostat nacelle, comprising a lower box body (10) and an upper box body (20), wherein the upper box body (20) covers the lower box body (10), and a side face of the upper box body (20) and a side face of the lower box bo...  
WO/2018/120744A1
Disclosed are an envelope material, an envelope, an aerostat, and a method for preparing the envelope material. The envelope material comprises a bearing layer and TPU coatings. The bearing layer is combined with the TPU coatings by mean...  
WO/2018/120742A1
A capsule body material, a capsule body, an aerostat, and a preparation method for the capsule body material. The capsule body material comprises a gas barrier layer (20), the gas barrier layer (20) being a coating or a film which are pr...  
WO/2018/113264A1
Disclosed is a centre of gravity adjustment apparatus for an airship. The centre of gravity adjustment apparatus for an airship comprises: a guide rail (30), the guide rail being provided at the bottom part of an airship gondola and exte...  
WO/2018/107733A1
A method and device for controlling an airship. The method comprises: acquiring route information and status information of the airship; determining, according to the route information and the status information, a speed and a tangential...  
WO/2018/098601A1
The invention relates to an energetically self-sustainable aerial video surveillance system and method, for controlling and monitoring large areas remotely and in real time, from any place and using any device with access to the Internet...  
WO/2018/085579A1
A vehicle body may have a skeleton formed by a plurality of overlapping layers bonded to each other. Each of the plurality of overlapping layers may be fabricated from a continuous fiber coated with a matrix material. A trajectory of the...  
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...  
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 (...  
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...  
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...  
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 (...  
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...  
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...  
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...  
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...  
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...  
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/2017/207666A3
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...  

Matches 1 - 50 out of 1,634