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WO/2018/237018A1 |
Among other things, sensor signals are received using a vehicle comprising an autonomous driving capability. A risk associated with operating the vehicle is identified based on the sensor signals. The autonomous driving capability is mod...
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WO/2018/235987A1 |
Disclosed is a system for diagnosing a solar panel. A system for diagnosing a solar panel according to an embodiment of the present invention comprises: a plurality of solar panels, each of which includes an information transmission modu...
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WO/2018/234330A1 |
The invention relates to the on-board electric power network architecture of a vehicle cabin using domestic devices, in particular of an aircraft cabin, comprising primary networks (11, 12) connected in parallel to a single domestic netw...
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WO/2018/236181A1 |
The present invention relates to a mobile platform-based AHRS flight control apparatus and, more specifically, to a mobile platform-based AHRS flight control apparatus of an unmanned flying object comprising a drone frame (10) on which a...
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WO/2018/232429A1 |
The invention relates to a protective propeller frame, in the interior of which at least one electrically driven propeller (12) is integrated and a protective device (9, 10, 16) of which surrounds the propeller to such a degree that the ...
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WO/2018/233164A1 |
The present invention reduces the influence of wind in the distribution of distributed objects by a flight body. A flight control method, which is a flight control method for controlling flying of the flight body, comprising: a step of o...
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WO/2018/233570A1 |
A gasoline-electric hybrid multiaxis rotor type unmanned aerial vehicle, which relates to the technical field of unmanned aerial vehicles. The unmanned aerial vehicle comprises an unmanned aerial vehicle frame, a lifting rotor (2) and an...
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WO/2018/234523A1 |
The invention relates to a method for detecting damage to a rotor of an aircraft, wherein the aircraft has actuators for actively reducing vibration, the method comprising the steps: determining actuator manipulated variables in a refere...
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WO/2018/233651A1 |
Provided is a device integrating a tip (3) of a rotary blade with a flight ring (2) particularly applicable to a helicopter or rotorcraft adopting an ABC-based rigid rotary blade. The device comprises an ABC-based rigid rotary blade (1) ...
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WO/2018/234705A1 |
Cryogenic propellant tank (1) for a spacecraft engine, comprising an external enclosure (10) defining an internal volume, characterized in that the internal volume of the tank comprises a primary volume (V1) and a secondary volume (V2) c...
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WO/2018/236946A1 |
When a first laser beam and a second laser beam are directed to the volume of space, an aerial drone is configured to lock onto the first laser beam using a first sensor, and to utilize the first laser beam to guide the drone to an accur...
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WO/2018/234104A1 |
A wing and flap system for an aircraft comprising: a wing; and a deployable flap connected to the wing, the flap being moveable between a first position in which a trailing edge portion of the wing substantially overlaps the flap and the...
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WO/2018/233977A1 |
System (1) for inerting at least one volume (3) in an aircraft, said system comprising at least one generator of inerting gas (2) fed with compressed air originating from a passenger cabin, and means for distributing (11) the inerting ga...
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WO/2018/234799A1 |
An aerial vehicle has a wing and a fuselage. A tether is anchored at opposing ends of the wing and/or the fuselage. The tether is arranged to prevent one or more parts of the aerial vehicle from separating from the remainder of the aeria...
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WO/2018/236903A1 |
Disclosed herein are system and method for automatically recharging a unmanned aerial vehicle (UAV) on a moving platform, comprising: a software module identifying the moving platform; a software module estimating a real-time state of th...
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WO/2018/236626A1 |
Techniques are disclosed for cooling an unmanned aerial vehicle (UAV). In some examples, a heat sink is coupled to a portion of the UAV that is to be cooled. One or more heat pipes are coupled to the shim, and extend to one or more propu...
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WO/2018/232584A1 |
An unmanned aerial vehicle and a control method therefor, and a control terminal and a control method thereof. At least two photographing apparatuses (11, 12) are provided on the unmanned aerial vehicle (10). The control method comprises...
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WO/2018/235071A1 |
A method for controlling maneuver of a refueling device, that includes: a refueling device is attached by a hose to a component of an aircraft. That component maintains a reference force on the hose. The desired position and current posi...
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WO/2018/232447A1 |
A system for monitoring a predetermined region in a water body, comprises a vessel having a control module, a plurality of drones in communication with the control module, a plurality of cameras available with the plurality of drones and...
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WO/2018/232430A1 |
The invention relates to a protective propeller frame, in the interior of which at least one electrically driven propeller (12) is integrated and a protective device (9, 10, 16) of which surrounds the propeller to such a degree that the ...
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WO/2018/234710A1 |
The disclosure relates to the field of acoustic treatment for aircraft turbojet engine nacelles. More specifically, it concerns an acoustic treatment device (6) in the form of an annular ring comprising several sections (61-66), each sec...
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WO/2018/235064A1 |
A system for slowing down the speed of flying objects by applying electrodynamic and aerodynamic braking forces. The system is comprised of plurality of stubs, where each stub is made of dielectric material surrounded by metal foil and a...
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WO/2018/234199A1 |
A metallic structure with a reinforced skin according to the invention (1), comprises at least one skin (10) and local reinforcement (3a) connected to the skin (10). Each local reinforcement (3) has a transition zone (31a) extended by a ...
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WO/2018/234670A1 |
This anti-rotation device (14) for suspending a load (12) under a machine (10) for lifting and moving this load (12), comprises a sling system (16A, 16B, 16C) provided with an element (18) for attachment to the machine (10). It further c...
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WO/2018/234798A1 |
An aircraft (1) has at least one main wing (2) and at least one boom fuselage (3). The main wing has an aerofoil section having a leading edge (20), a trailing edge (21), a chord length extending between the leading edge and the trailing...
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WO/2018/236295A1 |
Making drones travel greater distances and stay in mid-air for longer time periods, by making them use the wings at their horizontal movements enabled by developing drones with foldable wings to consume less energy, which can depart from...
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WO/2018/232787A1 |
Disclosed is a fixed-wing unmanned aerial vehicle which takes off and lands vertically, comprising a body (1), a wing (2) fixedly arranged on the body (1) and an empennage fixedly arranged at the tail of the body (1), and further compris...
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WO/2018/234316A1 |
Method for producing a component (1) from a fibre composite material, comprising the steps of: introducing a matrix-impregnated fibre (1) onto a cylinder-like inner mould (7) of a mould space formed between the inner mould (7) and a cyli...
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WO/2018/233860A1 |
The invention concerns a drive unit (100) for an aircraft, comprising: - a pylon (102) intended to be attached under a wing (14) of the aircraft (1) and having a front face (104) and a lower face (105) and - a turbine engine (10) compris...
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WO/2018/234071A1 |
The invention relates to a cutting device (20) comprising at least one firing pin retainer (1), at least one locking element (2), a spring (6), a firing pin (7), a percussion cap (9), a charge (13), a cutting element (14), a stop (15) an...
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WO/2018/228461A1 |
An unmanned aerial vehicle (UAV) configured to be carried on a vehicle and a method and a system for holding umbrella using the UAV are disclosed. The UAV and the vehicle are communicated with each other wirelessly. The UAV can be used f...
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WO/2018/232010A1 |
A tethered drone system and method includes a tethered drone and a tether. The tether includes a conductor to communicate at least power and control signals. The tethered drone system further includes a control system configured to recei...
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WO/2018/228033A1 |
Landing gear (20) of an unmanned aerial vehicle, comprising a power assembly (200) arranged in a fuselage (10) and a landing gear body (201) connected to the power assembly (200). The power assembly (200) comprises a first connecting pie...
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WO/2018/231842A1 |
Active tethers for controlling UAV flight volumes, and associated methods and systems, are disclosed. A method in accordance with a representative embodiment includes directing a UAV upwardly from a launch site, receiving an indication o...
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WO/2018/232340A1 |
An ejector system for propelling a vehicle. The system includes a diffusing structure and a duct coupled to the diffusing structure. The duct includes a wall having openings formed therethrough and configured to introduce to the diffusin...
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WO/2018/230680A1 |
This drone coordination device comprises: an acquisition unit that acquires an action plan from an automatic driving vehicle; and a determination unit for determining a flight plan for a drone, including the area in which the drone is to...
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WO/2018/229092A1 |
The subject of the invention is an aerodynamic braking device for a payload casing intended to be ejected from a projectile on its trajectory. This braking device comprises at least one parachute connected to the casing by hangers, the p...
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WO/2018/229332A1 |
An arrangement (100), optionally comprising one or more network accessible servers, for searching for digital video material, wherein the arrangement comprises at least one processor (102) configured to receive a number of video items: s...
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WO/2018/231507A1 |
Systems and methods for extending life of an apparatus, such as a balloon, using electrolysis. A ballast liquid is carried or harvested and, when desired, is electrolyzed using an on-board electrolyzer to generate lift gas, rather than s...
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WO/2018/231738A1 |
Aircraft are configured to facilitate propeller blade pitch adjustability. According to one example, an aircraft can include a plurality of propellers, where each propeller includes plurality of blades. At least one pitch adjust mechanis...
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WO/2018/228908A1 |
The invention relates to a method (101) for charging batteries for an aircraft comprising a plurality of steps and also to a system for storing electrical energy comprising a set of batteries charged by the charging method (101) of the i...
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WO/2018/229761A1 |
According to the presently disclosed subject matter there is provided an in-flight UAV retrieval system mountable on an aircraft and configured to execute a UAV retrieval process for retrieving one or more in-flight UAVs into the aircraft.
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WO/2018/230552A1 |
An assist system (10A) comprises: a detection unit (12) mounted in an aircraft capable of hovering, the detection unit (12) being provided on the outside of the fuselage (31), and detecting objects that could be obstacles; imaging units ...
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WO/2018/229747A1 |
A system for launching an Unmanned Aerial Vehicle (UAV), comprising: a capsule comprising at least two parts; a UAV configured to be encapsulated inside the capsule in a folded configuration; and an aerial carrier comprising a release me...
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WO/2018/228939A1 |
A ground independent aerial lifting and transportation system (1), for lifting and/or transporting at least one object (2) having a weight in the range of from 100 to 2000 kg, wherein the system comprises at least one aerostat (3) and at...
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WO/2018/232343A1 |
An imaging device can be mounted on a vehicle and used to capture images. The imaging device can include a camera assembly rotatable relative to a platform of the vehicle and about two or three camera axes. The camera assembly can includ...
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WO/2018/227298A1 |
A method of adjusting an interior component to be received in a fuselage of an assembled aircraft, including determining a deformed configuration of a fuselage portion of a test rig, the fuselage portion in the deformed configuration bei...
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WO/2018/229442A1 |
A device for penetrating into a fluid, comprising at least one profile (10), a fluid injector (14), a means for measuring the separation of the flow (18) along the profile, downstream of the injector, and an injector activity controller ...
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WO/2018/230818A1 |
The present invention relates to an unmanned aerial vehicle for inspecting a high-voltage line and a control method therefor. The unmanned aerial vehicle for inspecting the high-voltage line according to the present invention comprises: ...
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WO/2018/228012A1 |
A envelope pressure regulating device, comprising: a mounting portion (10) mounted at the upper end of a envelope, the mounting portion (10) having an air-guide hole communicated with the inside of the envelope; and a pressure relief str...
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