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Patent Searching and Data


Matches 1 - 50 out of 1,790

Document Document Title
WO/2021/011097A1
Aspects of the technology relate to propulsion systems for high altitude, long duration balloons, such as balloons that operate in the stratosphere for weeks, months or longer. A propeller assembly is used to provide lateral directional ...  
WO/2021/009359A1
The invention describes a three-dimensional object detection system comprising: - a transmission device (201) configured to transmit signals according to a coloured transmission method in a first plane, - a reception device comprising at...  
WO/2021/009507A1
A landing apparatus for an airship or hybrid air vehicle. The landing apparatus comprises a hollow, non-toroidal, flexible enclosure (103), having a substantially vertical axis (104), and a substantially circular cross-section centred on...  
WO/2021/007216A1
Technologies are described herein for a drag recovery scheme using a boundary layer bypass duct system. In some examples, boundary layer air is routed around the intake of one or more of the engines and reintroduced aft of the engine fan...  
WO/2020/255304A1
This barrier data collection device comprises: a unit estimation part which, on the basis of sensor data containing position information that includes height when a moving object including a flying moving object moving in the air is move...  
WO/2020/249447A1
The invention relates to a power assistance system (1) for supporting an electrically drivable aircraft (2) capable of vertical start and landing, wherein the power assistance system (1) is designed to support the aircraft (2) during asc...  
WO/2020/243573A1
A highly maneuverable craft is disclosed, having undulating fins of a light-weight material that may undulate along the horizontal axis of the craft and/or rotate 360 degrees and continuously about the central longitudinal axis of the cr...  
WO/2020/229800A1
A non-rigid airship or hybrid air vehicle has a pressure-stabilised envelope (100) that includes at least one ballonet (102, 103). A system is provided for measuring the geometry of the lifting gas enclosure (101) within the pressure-sta...  
WO/2020/226239A1
Disclosed is a low-altitude unmanned aerial vehicle surveillance system. According to an embodiment, the low-altitude unmanned aerial vehicle surveillance system comprises: a balloon body which stays in the air and is filled with gas; a ...  
WO/2020/214552A1
An airship (100) includes a ballonet (110), a ballonet tracking system (125), and a vehicle management system (140). The ballonet is disposed within the airship and includes a ballonet surface (120). The ballonet tracking system includes...  
WO/2020/206817A1
Disclosed is a large-scale semi-rigid structure airship, relating to the technical field of air floating aircrafts. The airship comprises a ship body, a vector side thrust, a vector tail thrust, an X-shaped inflatable tail fin, an air cu...  
WO/2020/202237A1
Rigid structural-frame dirigible comprising an internal framework divided in internal zones fixedly clearly separated and sealingly isolated therebetween through rigid partition means in fixed union with the internal frame itself, and su...  
WO/2020/181855A1
A dihedral trapezoidal lifting and floating integrated aircraft, comprising an aircraft body (1) and a power system. The aircraft body (1) comprises a head part provided with an equipment front compartment (2) and a tail part provided wi...  
WO/2020/128316A4
System (1) for securing an aerostat (2) to a receiving structure (3), comprising a tether (5) designed to be attached to the aerostat by one of the ends thereof, a mast (6) designed to be rotatably mounted on the receiving structure, the...  
WO/2020/175463A1
The present invention addresses the problem of providing a flying vehicle that makes it possible to fly for a long period of time by means of heated air without using any expensive lifting gases. A flying vehicle 1 according to one embod...  
WO/2020/174125A1
The invention relates to a method for controlling an elongated lighter-than-air air- craft formed of a thin shell. The method comprises providing at least one first stiffener (111, 211, 311, 411) on the outer surface of the shell of the ...  
WO/2020/166808A1
Disclosed are an air control system and method, using the air in the atmosphere. An air control system includes: a floating body (11) provided to stay in the atmosphere; an air transfer tube (15a, 15b) in cooperation with the floating bo...  
WO/2020/159402A1
Invention relates to the field of high-altitude wind energy. Aero-energystat comprises an aerostatic module in a soft gas-filled shell, a wind-power unit suspended under the shell, altemating-air-propeller electric aero-engines of the tr...  
WO/2020/153859A1
The present invention consists of a system that enhances and allows for the isolation and prevention of contamination, by diffusion, of two distinct gases separated by a membrane. The present invention is of particular use in aerostats. ...  
WO/2020/138703A1
The present invention relates to an electromagnetic exploration system based on an airship with adjustable depth of investigation, in which a transmission coil (transmitter loop) and a reception coil (receiver loop) are arranged in two i...  
WO/2020/138214A1
Provided is a flying object having a structure in which a rotating part has been removed from a portion that is touchable by a user during flight. A flying object 10 comprises: a balloon part 100; a control unit 110 provided below the ba...  
WO/2020/125824A1
The invention relates to a mobile sun shading device which comprises at least one body consisting of a cover (1) of plastic foil (2) or cellulose-based foil (2) which is in the lower part provided with at least one opening (5) and which ...  
WO/2020/128316A1
System (1) for securing an aerostat (2) to a receiving structure (3), comprising a tether (5) designed to be attached to the aerostat by one of the ends thereof, a mast (6) designed to be rotatably mounted on the receiving structure, the...  
WO/2020/132000A1
A system for an unmanned aerial vehicle can include an altitude control system 320, which further includes a compressor assembly 400, a valve assembly 500, and an electrical control assembly 600. The compressor assembly may include a dri...  
WO/2020/122315A1
The present invention relates to a wireless communication relay device using a drone and a balloon. The present invention is capable of relaying wireless communication between a drone and a manipulation device, while locating, by using a...  
WO/2020/122316A1
The present invention relates to a mobile meteorological observation device using a drone and a balloon, wherein the mobile meteorological observation device uses a balloon unit to lift a measuring instrument capable of measuring weather...  
WO/2020/116925A1
A drone takes off and lands vertically in the same way that an existing drone takes off and lands. The drone has a foldable wing portion to which a solar cell panel is attached, and when reaching a predetermined height, the drone unfolds...  
WO/2020/109050A1
The present invention relates to a robot arrangement having at least one buoyancy body (01) for filling with a gas lighter than air. The robot assembly comprises two stabilisation rods (02), which extend through the buoyancy body (01) an...  
WO/2020/109247A1
In a method for producing a PBO fiber with increased resistance against UV-caused degradation, a coating is provided on the PBO fibers, wherein the coating comprises graphene oxide cross-linked by polymerization with glutaraldehyde and r...  
WO/2020/091796A1
A ground-, sea- or aircraft-based laser transmission system can be implemented to remotely and wirelessly transmit power to an airship to be stored in an energy storage device, such as a battery. The airship can include an energy collect...  
WO/2020/076353A1
An airship dynamic adaptive harness is provided to stabilize airships and particularly a tethered aerostat in high winds and atmospheric changes. A novel adaptive device accommodates the supply of a lift gas and simultaneously controls o...  
WO/2020/018148A4
Systems, devices, and methods for receiving, by a processor (1424) having addressable memory (1427), data representing a geographical area for imaging by one or more sensors of an aerial vehicle (1302); determining one or more straight-l...  
WO/2020/051247A1
A towed atmospheric balloon system includes an atmospheric balloon including a quantity of lift gas and a neutral buoyancy towing system coupled with the atmospheric balloon. The neutral buoyancy towing system includes one or more towing...  
WO/2020/027140A1
Provided is a system comprising a floodlight and a control device, the control device having: a floodlight position information acquisition unit that acquires floodlight position information indicating the position of the floodlight; an ...  
WO/2020/018148A1
Systems, devices, and methods for receiving, by a processor (1424) having addressable memory (1427), data representing a geographical area for imaging by one or more sensors of an aerial vehicle (1302); determining one or more straight-l...  
WO/2019/245963A1
A valve assembly (50) for use with an unmanned aerial vehicle is provided and includes an inlet tube (52), a shuttle (70), a base plate (56), a screw assembly (60), and a spacer block (54). The shuttle is partially disposed within the in...  
WO/2019/246087A1
A system for an unmanned aerial vehicle can include an altitude control system 320, which further includes a compressor assembly 400, a valve assembly 500, and an electronics control assembly 600. The compressor assembly may include a co...  
WO/2019/200199A1
Disclosed in some examples are methods, systems, devices, and machine-readable mediums for providing a PNT system provided by stratospheric balloons. This stratospheric PNT system (SPNTS) replaces the space-segment of a standard PNTS wit...  
WO/2019/190222A1
The present invention relates to an atmosphere purification apparatus using a flying object, and an atmosphere purification and treatment method and, more specifically, to: an atmosphere purification apparatus using a flying object, the ...  
WO/2019/170158A1
Provided is a transformable stratospheric airship, comprising: an upper hull (1), a lower hull (2), a folded ballonet (3), and wire arrangement mechanisms (4) arranged on the upper hull and the lower hull, wherein the folded ballonet com...  
WO/2019/173443A1
An aircraft apparatus may include an outer membrane and an inner flexible bladder. The flexible bladder may include a lighter-than-air lifting gas therein, and an interstitial space between the outer membrane and the inner flexible bladd...  
WO/2019/162737A1
The present invention relates to a field of transport system and more particularly relates to system enabled to transport passengers by a hybrid balloon air-ship followed by guide-ways. The static enclosure may further comprise a gas lig...  
WO/2019/157577A1
A fault-resistant aerostat system is discussed, for structural support and network interconnection, which can be applied to numerous systems based on lighter-than-air lift. The invention describes a system with an optimized reinforcement...  
WO/2019/135802A1
A flight vehicle includes a drone (28) with a pair of shaped protrusions (22, 24) mechanically coupled to the drone. One of the shapes is a hollow lift-producing shape (22), such as being a balloon filed with a lighter-than-air gas, and ...  
WO/2019/127987A1
A cable winding device, comprising: a bottom plate (10); a cable storage device (20); the cable storage device (20) is disposed on the bottom plate (10) and has a cable storage space; a cable spooling device (30); an outlet end of the ca...  
WO/2019/127986A1
A mooring rope guiding device, comprising a mounting support (10) connected to a truss; a winding wheel (20), the winding wheel (20) being pivotally connected to the mounting support (10), and a winding groove (21) being circumferentiall...  
WO/2019/127985A1
A connecting structure and an aerostat comprising the same. The connecting structure (100) is used for mounting an external device and comprises: a capsule connecting portion (10) which is a solid structure; one end of the capsule connec...  
WO/2019/127984A1
Provided is a buoyancy measurement device (10) for a captive balloon. The buoyancy measurement device (10) comprises: a cable connector (22), multiple mooring cables (24) of the captive balloon being connected to the cable connector (22)...  
WO/2019/119690A1
An aerostat positioning system and method, a storage medium, and a processor. The system comprises: an altitude sensor (10), provided in an aerostat and used for measuring the altitude of the aerostat relative to a plane in which an anch...  
WO/2019/125789A1
A buoyant aerial vehicle includes: a balloon configured to store a gas; a pay load coupled to the balloon; and a propulsion unit coupled to the payload by a tether. The propulsion unit includes: a fuselage having a substantially longitud...  

Matches 1 - 50 out of 1,790