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WO/2024/095853A1 |
In the present invention, an air conditioning control unit acquires vehicle internal environment information, vehicle external environment information, and flight information via steps S101-S103 of an air conditioning control process. Th...
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WO/2024/083876A1 |
The present invention relates to an aerostat of the type comprising a lift enclosure (1), filled with gaseous dihydrogen, electric propulsion means allowing the propulsion of the aerostat and means for supplying electricity to the propul...
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WO/2024/069215A1 |
using UAV technology can be applied to road crack detection and using image processing techniques, the captured or scanned images of the infrastructure parts can be analyzed to identify any possible defects. Apart from image processing, ...
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WO/2024/065022A1 |
The invention consists of a wind turbine that produces electrical energy when said turbine is rising through the atmosphere with the aid of a balloon filled with a gas that carries the turbine to high altitude, and that produces electric...
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WO/2024/049372A1 |
An air traffic control system for providing air traffic control of a group of balloons having at least two hot air balloons (500), each having at least one position sensing unit (141), including at least one hot air balloon (500) navigat...
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WO/2024/020096A1 |
The system can include: a vehicle 100 and a stabilizer 200. However, the system can additionally or alternatively include any other suitable set of components. The system functions to facilitate vehicular transport (e.g., via a cabin). A...
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WO/2024/020423A1 |
A hydrogen boiloff capture system. The hydrogen boiloff capture system having a cryogenic tank for storing liquid hydrogen. The hydrogen boiloff capture system also includes an intermediate tank fluidically coupled with the cryogenic tan...
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WO/2023/209319A1 |
A variable-volume aerostat, consisting of a flat gas envelope, joined to guide aerostat bodies. The flat gas envelope is typically deployed by rotation of cylindrical guide airships, or rollers suspended beneath guide aerostats. In its s...
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WO/2023/203672A1 |
This flying body system comprises a flying body (1) that can execute predetermined work, and an energy supply body (2) that can supply energy to the flying body (1).
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WO/2023/194253A1 |
Improved device and method for indoor monitoring The invention provides, amongst other aspects, an aircraft (1) for indoor monitoring, comprising a lifting means; a propulsion means (4, 4', 51, 61); a positioning means (2a, 2b); and a mo...
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WO/2023/187638A1 |
A piloting system (10) comprises an aircraft (12) disposed in the stratosphere at a first altitude (q1) and immersed in a first wind (v1), and two orientable sail towing means (14, 16), each comprising a sail (18), connected to the aircr...
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WO/2023/178456A1 |
The present invention relates to a tensegrity-type membrane structure, the aim of which is to provide a structure that levitates by means of a vacuum chamber and that can be used for the transport of cargo and/or people. The invention wo...
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WO/2023/167703A1 |
Various implementations include a low-drag smart tether system for measuring fluid speed and direction. The system includes a sleeve, a pressure sensor, and a tether. The sleeve has a longitudinal axis and an airfoil shaped cross-section...
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WO/2023/152142A1 |
A production unit (1, 1') for generating hydrogen or ammonia by electrolytic decomposition of water, with an electrolysis unit (4) supplied with electrical energy by a photovoltaic unit (8) and connected on the media side to a water stor...
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WO/2023/154380A1 |
The cabin conditioning system can include a cabin air loop, a refrigerant loop, and a set of thermal rejection components. The system can optionally include a phase-change fluid loop. However, the cabin conditioning system can additional...
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WO/2023/135521A1 |
Aerial apparatus (10) with several successive aeronautical configurations, wherein, considered in ascending flight attitude, it comprises: • - a motorized paraglider (11), including a spacecraft (11.1) and a non-pressurized sail (11.2)...
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WO/2023/133456A2 |
Solar balloons are a simple and lightweight option for aerial exploration and meteorological data collection both terrestrially and on other planets. By using lightweight materials that absorb visual light and emit low levels of thermal ...
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WO/2023/118830A1 |
A tethered aerostat (101, 201, 203, 205, 401, 601, 708) positioned at an elevated location in the atmosphere, the aerostat (101, 201, 203, 205, 401, 601, 708) having an elongate body (403) having a length extending between an upper end (...
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WO/2023/122109A1 |
An aircraft has port side and starboard side propeller blades that each have a portion of the blade hidden or overlapping with the fuselage. This hidden or overlapping blade may extend into a slot of the fuselage. The advancing or retrea...
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WO/2023/107534A1 |
The invention features an apparatus for airborne transport of cargo. Such an apparatus includes a controller and an airship having a hull, an airframe that supports the hull, and at least one ballast chamber. The controller is configured...
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WO/2023/096965A1 |
A lighter than air platform an unfinned envelope having two or more propulsion elements coupled with the unfinned envelope proximate to the center of gravity. At least one navigation sensor is configured to monitor an actual flight path ...
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WO/2023/091991A1 |
A system, method and apparatus are proposed to assist in assembling the frame, attaching the skin, and performing other tasks in manufacturing an airship and constructing other structures that are otherwise challenging, inefficient, or u...
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WO/2023/076232A1 |
Devices, such as aerodynamic kites used in kiteboarding (also known as kitesurfing), handheld aerodynamic wings used in wing foiling and wing surfing, and paddles used in paddleboarding, for generating a force for powering a user on an a...
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WO/2023/064188A1 |
The disclosed invention describes a method for determining a current state of a gas cell in an airship, particularly the lift. A computing device receives depth measurements of the interior of the gas cell using a lidar sensor positioned...
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WO/2023/064944A1 |
A lighter-than-air craft including an envelope. A mixture of helium and hydrogen disposed within the envelope. The mixture having a ratio of helium to hydrogen such that the mixture is nonflammable during operating conditions for the lig...
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WO/2023/057606A1 |
The invention relates to a rocket stage (1) for a multistage space launch vehicle (3, fig. 3), comprising a main engine (5) and being configured for stage separation from the remaining parts of the space launch vehicle (3, fig. 3) such t...
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WO/2023/047025A1 |
A system (1) for docking an airship (2) on a receiving structure (3) comprising at least one unmanned aerial vehicle (4) that can be controlled so as to move between the airship (2) and the receiving structure (3), carrying a first end (...
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WO/2023/047110A1 |
An airship comprising an airship body, a ballast assembly (7) comprising at least one ballast pod (7) coupled to the airship body, and a payload lifting device (4,6) coupled to the airship body and configured to lift a payload, wherein t...
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WO/2023/023828A1 |
The present invention relates to an innovative type of electric and/or hybrid digital glider drone with a steerable balloon for personal flight. The project consists of a compact ellipsoidal balloon with a self-levelling drone with rigid...
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WO/2023/002132A1 |
The invention relates to a system (100) for the thermal management of an external electric-power-generating nacelle (1) equipping an electrically powered airship and comprising electrical generation means (84.1, 84.2) and auxiliary equip...
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WO/2023/002131A1 |
The invention relates to a system (200) for the thermal management of an external electric-power-generating nacelle equipping an electrically powered airship, said nacelle comprising electrical generation means implementing at least one ...
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WO/2023/002134A1 |
The invention relates to an airship comprising a main body having a rigid structure surrounding a plurality of containers for a lighter-than-air gas, a plurality of power units mechanically connected to the rigid structure and each compr...
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WO/2023/002133A1 |
An airship comprising a main body having a rigid structure (4) surrounding a plurality of containers for a lighter-than-air gas, a plurality of propeller units mechanically connected to said rigid structure and each comprising one or mor...
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WO/2022/257586A1 |
Embodiments of the present application relate to the technical field of aviation devices, and in particular to a flying boat, comprising: an air bag (110), a cockpit (120), and a first shaft body (130). The air bag (110) is configured to...
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WO/2022/248631A1 |
A remote control system for an aircraft, comprising: - an aircraft, of the Magnus-effect type, comprising a cylinder (1) extending along a longitudinal axis (Y), the cylinder (1) being able to rotate about the longitudinal axis (Y); - a ...
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WO/2022/243614A1 |
Device for assembling secondary tubes on a main tube made of composite material, comprising a sleeve (10) mounted coaxially on the main tube and provided with two attachment regions (11, 13), the attachment regions being intended to be a...
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WO/2022/237995A1 |
A lighter-than-air aerial platform is consisting of two or more inflatable elements (100), balloons or dirigibles, a propulsion system (400), aerodynamic lifting and flight surfaces (500) which are optionally inflatable, an on-board elec...
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WO/2022/235733A1 |
A solar powered airship includes a cabin, at least one fuselage having an interior volume filled with a volume of a lighter-than-air gas such as helium, and a wing affixed to the fuselage. A plurality of solar panels are affixed to the w...
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WO/2022/232828A1 |
Various embodiments relate to a system and method of suppressing contrails emitted from an aircraft. One such system comprises a semi-closed cycle gas turbine engine of an aircraft that exhausts gases in use; a recuperator component that...
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WO/2022/223886A1 |
The present invention relates to an autonomous captive aerostat (2) of the type comprising a closed hydrogen-reservoir volume (24) providing lift, an outer membrane (40) equipped with photovoltaic cells (8) for collecting solar radiation...
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WO/2022/224261A1 |
A system and method configured for airborne processing of captured gaseous matter from the earth's atmosphere while utilizing unique high-altitude conditions in order to create a desired substance/s, wherein the operation of said system ...
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WO/2022/216264A1 |
The invention is an aerostat-type unmanned aerial vehicle system developed to reduce air pollution, comprising an unmanned aerial vehicle (5) comprising an airframe (1) filled with a lighter-than-air gas, at least one air filtration unit...
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WO/2022/217225A1 |
The invention comprises an apparatus, method for using the apparatus and system for balloon altitude control by in-situ characterization and active energy management. The invention presented enables transportation, autonomous operation a...
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WO/2022/200316A1 |
A method for manufacturing an envelope for an aerostat balloon, the finished envelope after inflation having a convex outer surface, a concave inner surface and an elongated shape which extends in an axial direction, perpendicular to a c...
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WO/2022/193156A1 |
An unmanned aerial vehicle (100), comprising: a rack (110); a buoyance apparatus (120), mechanically coupled to the rack (110), wherein the buoyance apparatus (120) can be in an open state or a closed state, and when being in the open st...
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WO/2022/182904A1 |
Pneumatically supported towers for low gravity applications are disclosed herein. In one aspect, an inflatable tower for use in vacuum environments can have a membrane configured to support a load when inflated with an inflation gas to a...
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WO/2022/182912A1 |
The technology relates to payload separation during descent of an aerial vehicle. A flight termination system (FTS) for a lighter than air (LTA) vehicle can include a first, a second, and a third mechanical actuation system. The first me...
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WO/2022/144516A1 |
The present invention relates to an aerostat (1) comprising: - an inflatable body (2) configured to be pressurised by a gas lighter than the atmosphere, - a payload support member (3) configured to support a payload, the support member b...
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WO/2022/141777A1 |
An aerostat with a phase change adjustment airbag, the aerostat comprising a main airbag (302); a load nacelle (308), which is used for containing a mission apparatus and a mission load; a phase change adjustment airbag (330), which is u...
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WO/2022/133614A1 |
A mobile towing and lifting system and associated methods, comprising a retractable tug, coupled to an aerial vehicle, wherein the tug is configured to transfer electrical power and data to and from the aerial vehicle. The aerial vehicle...
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