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WO/2019/201126A1 |
A method and device for realizing quick movement of a carrier-based aircraft on an aircraft carrier. A deck is provided with one or more movable devices (1) for raising and moving a carrier-based aircraft. The movable device (1) is used ...
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WO/2019/202325A1 |
Methods, apparatus, systems and a vertical take-off and landing (VTOL) vehicle are provided. The VTOL vehicle includes: a fuselage having longitudinally a front section, a central section and a rear section; a first lifting surface compr...
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WO/2019/201125A1 |
A multi-level aircraft parking device for an aircraft carrier comprises a carrier-based aircraft support platform (3), a longitudinal slide rail (1) and a sliding block (2). At least one vertical slide rail (1) is fixedly installed at ea...
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WO/2019/199390A1 |
Embodiments relate to aircraft arresting systems that use a net or a cable that extends across a section of a runway. Ends of the net or cable are secured to an elongated tape, which is secured to and forms a part of an energy absorbing ...
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WO/2019/194004A1 |
The present invention suppresses adverse effects that occur in the communication of a wireless communication device on the ground when a wireless base station where an interference by a wireless communication device mounted in a flight v...
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WO/2019/194277A1 |
A flying device 11 comprises a body 13, a structural part 14, and a retroreflection member 15. The structural part 14 is provided below the body 13 in the direction of gravity. The retroreflection member 15 is provided to the structural ...
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WO/2019/194011A1 |
According to the present invention, an unmanned aerial vehicle (UAV) can be freely operated and controlled so as to smoothly and stably fly. A position and azimuth detection unit calculates, on the basis of a three-dimensional coordinate...
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WO/2019/194005A1 |
In the present invention, when there is a connection between a radio base station at which interference from a radio communication device of a flight vehicle is occurring, and a radio communication device of another flight vehicle, an ad...
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WO/2019/194003A1 |
According to the present invention, an assignment unit 53 assigns a flying object 10 having a wireless communication device 30 to each of airspaces. At this point, the assignment unit 53 limits the assignment of the flying object 10 to a...
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WO/2019/193131A1 |
Method for an aerospace structural component (19) comprising a stiffener structure (10), wherein the stiffener structure (10) comprises stiffeners (12) extending along the aerospace structural component (19), and wherein the stiffeners (...
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WO/2019/193335A1 |
A conveyor system is described for use with a scanning apparatus (49) for the scanning of objects (43), such as bottles. The system comprises a transverse conveyor having a conveyor surface (45); a plurality of object support modules(41)...
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WO/2019/184418A1 |
An apparatus and method for the continuous launching of unmanned aerial vehicles (6), relating to the technical field of aircraft launching and recovery. The apparatus consists of an unmanned aerial vehicle storage apparatus (1), an unma...
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WO/2019/190856A1 |
A system and a method for retrieving a package delivered by an Unmanned Aerial Vehicle (UAV). The system includes a receiving structure mounted to and extending from a wall of a building, the receiving structure being configured to recei...
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WO/2019/186151A1 |
A computer-implemented method for simulating liquid collection on an aerodynamic component impacting a plurality of droplets comprises: defining initial simulation parameters including a droplet distribution, size, and velocity relative ...
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WO/2019/188250A1 |
This storage facility management device comprises: a reception control unit for receiving, from a flight management device for causing a flying device to fly, instruction information that includes a time at which the flying device is to ...
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WO/2019/180574A1 |
Installation for powering and controlling a plurality of signalling lights (1), arranged in series, each comprising at least one light source (L1,L2), the installation comprising at least: - a unit (100) for remotely programming/managing...
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WO/2019/182620A1 |
Systems, methods, and non-transitory computer-readable media are disclosed for automatically generating an improved aircraft wing by modifying quantitative design variables of one or more airfoils based on joint analysis of aerodynamic a...
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WO/2019/180695A1 |
An aerial vehicle securing system for use with a base portion of an aerial vehicle, comprising: at least one substantially flat platform for supporting said base portion upon landing of the aerial vehicle thereon; at least one magnetizab...
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WO/2019/183269A1 |
Systems, computer-implemented methods and/or computer program products that facilitate aviation engine inspection are provided. In one embodiment, a computer-implemented method comprises: generating, by a system operatively coupled to a ...
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WO/2019/179999A1 |
A mobile passenger access apparatus for facilitating the boarding and disembarkation of passengers from an aircraft comprising a mobile chassis, a base stair section mounted on the chassis and including a first flight of steps, an extend...
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WO/2019/175993A1 |
[Problem] To provide a target member which accurately guides a moving body to a target location. [Solution] This target member 10, used when performing control to guide a moving body 20 to a target location, is formed using two or more d...
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WO/2019/178423A1 |
Devices for inhibiting a cable coupling drones from being entangled in the propellers of the drones, and associated systems and methods, are described herein. For example, a device can include a first weight coupled to the cable and conf...
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WO/2019/178064A1 |
A wing-to-body fairing on an aircraft having a fuselage, wing, and a wing root fairing. The wing-to-body fairing includes forward and trailing edges. The forward edge is configured for positioning adjacent a first predetermined location ...
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WO/2019/176058A1 |
According to the present invention, learning data, which is required for additionally training a learnt model of artificial intelligence to be used for identifying an aircraft, can be efficiently generated. A learning data generation met...
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WO/2019/176793A1 |
A composite material lamination device (10) laminates a composite material (22) on a lamination surface (3), which is an outer surface (1a) of a mold (1) that includes one side surface (1aa) and another side surface (1ac), or an outer su...
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WO/2019/175907A1 |
Disclosed is a system for horizontal marking of air and ground transportation. The system comprises at least one sheet of a pliant mesh material that is preferably at least 30% open when in use and preferably has a ground footprint weigh...
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WO/2019/170671A1 |
This aircraft refuelling device (400) comprises a fuel circulation pipe (40) of which the downstream end (43) is equipped with a wing coupling (42) for connecting it to an inlet orifice of a fuel tank of the aircraft. This wing coupling ...
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WO/2019/171748A1 |
This aircraft platform (26) includes a base (40), a landing pad (42), a horizontal sensor (44), and at least one actuator (48R, 48L). The landing pad (42) is supported by the base (40). The horizontal sensor (44) detects the inclination ...
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WO/2019/170647A1 |
Said aircraft refuelling device comprises a deformable pipe (40) for the circulation of fuel, the downstream end (43) of which is provided with a wing fastener (42) for the connection thereof onto an intake port of the aircraft fuel tank...
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WO/2019/170997A1 |
The invention relates to a riveting machine comprising a piercing tool (52), an upper clamp (71) and a lower clamp (21), which are mounted with the ability to move relative to one another in the direction of the said clamps (71, 21) movi...
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WO/2019/170668A1 |
The invention relates to a device for refuelling an aircraft, this device comprising a fuel flow duct (40), the downstream end (43) of which is equipped with a wing coupler (42) for connecting it to an inlet orifice of a fuel tank of the...
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WO/2019/173228A1 |
An unmanned aerial vehicle including a body, a platform, a rotor, a tether cable, and an actuation system. The platform is coupled to the body such that the platform is rotatable relative to the body about a first horizontal axis of rota...
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WO/2019/163523A1 |
A flight status inspection system (10), flight status inspection method and program inspect the flight status of a flying object (12) (drone (12)) capable of flying through the air. The drone (12) has a gravitational center movement devi...
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WO/2019/162611A1 |
The invention relates to a drive unit comprising an engine such as a turbofan engine (4) and a nacelle which comprises, on the outside around an annular stream of fresh air, starting from upstream, an air inlet, front side covers (8), a ...
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WO/2019/164833A1 |
A luggage transport cart with a cabin made primarily out of a polymer. In some embodiments, the luggage cart includes an inwardly sloping floor and shelf to help contain the luggage. The floor and shelf may further include ribs and groov...
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WO/2019/164042A1 |
The present invention relates to a method for detecting a live animal in an airport common checked-baggage self-processing device by using a Doppler radar device. A method for detecting a live animal in a checked baggage according to an ...
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WO/2019/161502A1 |
A method and system for automating de-icing procedures for aircraft including the transmission of messages and illumination of guidance lights for pilots to direct their aircraft for de-icing. The system further includes apparatus for ge...
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WO/2019/162610A1 |
The invention relates to a propulsion unit comprising a nacelle and a turbofan engine, comprising a thrust reverser having gratings provided with movable thrust reversal gratings arranged around an annular duct for fresh air from the tur...
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WO/2019/160821A1 |
The invention relates to an airfield light comprising a body, a medium intensity lighting arrangement, and a high intensity lighting arrangement. The medium intensity lighting arrangement provides an omnidirectional light source, and the...
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WO/2019/160540A1 |
Example landing platform systems and methods are described. In one implementation, a landing platform includes a top plate configured to support an unmanned aerial vehicle (UAV), where the top plate has a plurality of slots therethrough....
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WO/2019/159478A1 |
The method for producing an assembly is a method for producing an assembly equipped with a member to be reinforced (20), a reinforcing member body (41), and a filler (42), wherein the reinforcing member body (41) has a pair of flanges (4...
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WO/2019/160022A1 |
[Problem] To obtain high measurement accuracy in aerial photogrammetry while reducing the cost of installing a measurement target. [Solution] According to the present invention, a launching pad 220 for an unmanned aircraft on which a UAV...
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WO/2019/155854A1 |
A multicopter system according to an aspect of the present invention is provided with: a multicopter configured to be able to aviate in a state in which the multicopter carries goods; and a mooring device installed at a location which is...
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WO/2019/156604A1 |
The present invention regards a hollow load-bearing beam structure (1) and a method for manufacturing of the structure. The structure (1) comprises fiber-reinforced composite material. The structure (1) comprises a first plurality of lam...
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WO/2019/151947A1 |
An unmanned vehicle module (700) with a landing platform (703) and deployment system with improved charging capability is provided. The unmanned vehicle module includes a landing and deployment area for receiving or deploying an unmanned...
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WO/2019/151055A1 |
Provided is a wireless power transmission device which implements an efficient wireless supply of power to an aerial vehicle with high power reception efficiency. The wireless power transmission device, which wirelessly transmits power t...
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WO/2019/152276A1 |
A system and a method for protecting a user from potentially falling unmanned aerial vehicle (UAV) or package or both are described herein. The system includes a base structure; and a roof structure attached to and extending from the bas...
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WO/2019/146517A1 |
The objective of the present invention is to provide a human-powered flight experiencing device with which a pilot can obtain the experience of flying through the air by moving his or her own arms and legs. A human-powered flight experie...
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WO/2019/144386A1 |
Provided is a method for predicting the key performance parameters of an aviation engine transition state, belonging to the technical field of aviation engine performance parameter prediction. First, an aviation engine transition-state b...
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WO/2019/146580A1 |
In the present invention, a flight plan acquisition unit 101 acquires a first flight plan that satisfies a flight condition determined in accordance with a flight purpose of a drone 20. A flight allowability determination unit 102 determ...
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