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WO/2018/071451A1 |
A system and method for storing and sequencing a plurality of luggage items. The system includes containers with vertically stacked shelves and an automatic guided vehicle releasably attachable to the containers for transporting a contai...
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WO/2018/069802A1 |
The present invention relates to a compactor trolley for aeronautical applications, more particularly a trolley provided with a drawer having a door(s) with safety closing system which incorporates a flap for direct access to the waste s...
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WO/2018/071645A1 |
A microsatellite may include a module having a power source and a housing for containing an experiment, a drag device structurally configured to facilitate an orbit of the microsatellite when the microsatellite is deployed in space, wher...
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WO/2018/069994A1 |
The present invention suppresses, without greatly increasing the mass of a satellite, the time average peak value of a low-frequency magnetic noise or a low-frequency conduction noise generated from a power supply device which drives a h...
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WO/2018/071727A1 |
According to an aspect, a system for monitoring crops and soil conditions below a crop canopy includes a retractable boom assembly adapted to be coupled to an unmanned aerial vehicle. Further according to this aspect, the boom assembly i...
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WO/2018/071430A1 |
The exemplary embodiments herein provide a tether for use with an airborne device, where the tether contains an elongate member having a first end for attaching to a ground attachment point and an opposing second end for attaching to the...
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WO/2018/070103A1 |
Provided are a detachable unit that makes it possible to make work for calibrating the various sensors provided to an unmanned aerial vehicle more efficient and to unitize an unmanned aerial vehicle control function, and a sensor calibra...
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WO/2018/069671A1 |
A cavity system, comprising: a cavity (2) comprising a cavity opening; and an acoustically reflective structure (18, 20) located at least partially within the cavity (2), the acoustically reflective structure (18, 20) comprising one or m...
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WO/2018/071453A1 |
The use of UAV network cells may enable a wireless communication carrier to provide supplemental cellular network communication coverage to geographical areas. In some implementations, a first baseband processor of the UAV network cell m...
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WO/2018/068193A1 |
Provided are a control method, a control device, a flight control system, and a multi-rotor unmanned aerial vehicle. The control method comprises: controlling a multi-rotor unmanned aerial vehicle to fly toward a target location (210); d...
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WO/2018/071596A1 |
A contoured class divider for dividing an aircraft cabin includes a panel positioned between an aft seat and a forward seat, the panel having an aft-facing convex contour closely matching an aft-facing contour of a seatback of the forwar...
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WO/2018/071592A2 |
A hover-capable flying machine such as a drone includes a robotic arm extending from the body, and an instrumentality for balancing the machine in response to disturbances such as those caused by picking up and dropping of the payload by...
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WO/2018/069974A1 |
This image capturing device is provided with: a control unit that, by causing a lens to move in a first direction along the optical axis, causes capturing of multiple first images through the lens when the lens is positioned at multiple ...
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WO/2018/070586A1 |
The present invention relates to a drone for detecting a school of fish or submerged objects moving underwater and, more specifically, to a drone for detecting fish, landing on water while flying overwater so as to detect a school of fis...
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WO/2018/070867A1 |
An aerial vehicle (50) for vertical take-off and landing and horizontal flight comprises two wings (31, 32) extending substantially parallel to a Y-axis in spanwise direction, substantially parallel to an X-axis in chordwise direction, a...
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WO/2018/071070A1 |
An impulse momentum propulsion apparatus includes a power source and a track arranged radially relative to a vertical axis with a proximal end of the track nearest the vertical axis and a distal end of the track farthest from the vertica...
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WO/2018/068126A1 |
A seat blocking insert for an aircraft passenger seat is provided. The insert is comprised of a base and a tray. In one embodiment the base is solid having a front wall and sidewalls with grooves side for receiving an aircraft passenger ...
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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...
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WO/2018/067800A1 |
An articulated support includes a base and pitch-roll-yaw assembly having a pitch/roll subassembly and a yaw subassembly. The pitch/roll subassembly includes a central member configured for spring-loaded rotation about a pitch/roll axis,...
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WO/2018/067100A1 |
The group of inventions relates to aviation. An aeroplane comprises a fuselage which consists of a body of an upper load-bearing piloted part and a capsule in the form of a body of a lower part which is capable of automatically separatin...
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WO/2018/066744A1 |
A multidrone control system according to an embodiment of the present invention comprises: a virtual drone agent for analyzing individual information of a pilot, individual information of a drone and real-time pilot monitoring informatio...
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WO/2018/067327A1 |
A landing pad receptacle receives and stores a package delivered by an unmanned vehicle, comprising: a housing; a storage compartment in the housing; and a validation device that detects a presence of a package delivered by a unmanned ve...
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WO/2018/066753A1 |
An unmanned aerial vehicle and an automatic charging device for the unmanned aerial vehicle are disclosed. In one embodiment, the unmanned aerial vehicle comprises a main body and a connection part. The main body includes: a battery; and...
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WO/2018/064918A1 |
Disclosed are a photographic device and an unmanned aerial vehicle comprising same. The photographic device comprises: a plurality of photographic units (9); a fixing unit (7) for fixing the plurality of photographic units (9); and a pow...
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WO/2018/067982A1 |
In a preferred embodiment, a modular lavatory system for replacing a conventional lavatory monument in an aircraft cabin includes a base lavatory module including a fore sidewall, an aft sidewall, and an aisle wall that form a housing en...
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WO/2018/064900A1 |
The present invention relates to a near space aircraft pod comprising a pod body (1) and a covering piece (2), wherein a heat dissipating part (11) is provided on the pod body for dissipating heat inside the pod body; and the covering pi...
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WO/2018/065737A1 |
The invention relates to a system for measuring the distance of an obstacle (14), in which an optical flow is radially measured in rotation around a circle (12) in a plane intersecting the obstacle; and the distance of the obstacle is de...
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WO/2018/067296A1 |
Systems, devices and methods are disclosed for detecting, characterizing and engaging unmanned vehicles. In one aspect, a method includes detecting an object, such as an unmanned aerial, land or aquatic vehicle that communicates using a ...
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WO/2018/067029A1 |
The invention relates to aviation engineering. Each variant of an aircraft canopy comprises a glazed housing having a front portion, an upper portion and convex lateral portions which protrude beyond the upper portion. The housing has tr...
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WO/2018/065704A1 |
The invention relates to a device for mechanical locking/separation by rotation, comprising a main body (1) secured to a first system, provided with an actuator (2) for rotatably actuating a rotatable rod (3) inserted into the main body;...
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WO/2018/066043A1 |
Provided is a delivery rotary-wing aircraft capable of stably landing on a destination free of influence from an updraft occurring in a region, such as tall buildings. This rotary-wing aircraft comprising a plurality of rotary wings, a c...
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WO/2018/067028A1 |
The claimed invention relates to rotary wing aircraft and, in particular, helicopters having a single-rotor configuration. In one of its possible embodiments, the claimed helicopter comprises a fuselage, a tail boom, a tail rotor secured...
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WO/2018/065159A1 |
The invention relates to a method for replacing an aircraft part; in particular an aircraft turbine engine; the method comprising the following steps: (a) deciding (100) to replace a part, in particular a faulty part; (b) landing (102) t...
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WO/2018/066819A1 |
An unmanned aerial vehicle (UAV) according to various embodiments may comprise: a housing; a motor arranged in the inner space of the housing; a rotor which is rotated by the motor, and which comprises at least one cam structure; and at ...
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WO/2018/064831A1 |
Provided is a tripod head (100), comprising: a bracket (10), a roll axis motor assembly (21), a pitch axis motor assembly (22), a first camera (31) and a second camera (32); the first camera (31) and the second camera (32) are provided o...
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WO/2018/065703A1 |
The invention is directed to an attachment device (1) for attaching a booster (200) along a main body (100) of a space launch vehicle, comprising a combination of two pivots (2, 3) and of an annular linear connection (4), and to a space ...
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WO/2018/067499A1 |
In some embodiments, systems and methods are provided that limit the change in temperature and/or control a temperature of a product during delivery. Some embodiments provide systems comprising an unmanned delivery vehicle (UDV) comprisi...
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WO/2018/065336A1 |
An aircraft having a longitudinal axis determining a fore-aft direction, comprising at least two floats (111, 121)) configured to support the aircraft on a ground medium located below the floats with a ground-facing side of the floats, w...
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WO/2018/065274A1 |
Air start unit for starting and servicing jet engines in aircraft and other flying machines, wherein at least one compressor (1) is provided for generating air and a power supply (10) for supplying electrical power consumers. The propose...
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WO/2018/065882A1 |
The present discloses a system for washing and de-icing of aircrafts. The preset invention provides a hangar comprising three gantries to ensure different steps of the washing or the de-icing process. The structure of the gantries is ess...
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WO/2018/067310A1 |
An air intake assembly for an aircraft includes an auxiliary power unit intake that is defined by a skin of the aircraft. The auxiliary power unit intake is in fluid communication with an auxiliary power unit. The air intake assembly als...
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WO/2018/065731A1 |
The invention relates to a method for locating defects in an electrical line of an aircraft, said line comprising a plurality of electrical harnesses, said method comprising the following steps: determining a distance of a defect on the ...
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WO/2018/067329A1 |
A method of supersonic thrust generation includes generating a thrust supersonic exhaust plume (522) having a first average velocity from an engine (500), and expelling a bypass exhaust plume (532) having a second average velocity from t...
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WO/2018/067370A1 |
An air duct includes a first chamber and a second chamber, the first chamber being defined between an air handling device and the second chamber, and the second chamber being defined between the first chamber and an environment exterior ...
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WO/2018/065857A1 |
This disclosure relates to systems and methods for determining predicted risk for a flight path of an unmanned aerial vehicle. A previously stored three-dimensional representation of a user-selected location may be obtained. The three-di...
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WO/2018/066918A2 |
A flapping flight device according to the present invention is a flight device having at least one wing on each of the left and right sides of a fuselage so as to make a relative movement with regard to the fuselage by means of a driving...
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WO/2018/065977A1 |
A method for determining a route for a drone to deliver a package from an origin to a destination using vehicles that are not actively participating in a delivery of the package; a method for delivering the package from the origin to the...
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WO/2018/060970A2 |
An oblique rotor-wing aircraft may be capable of vertical take-off and landing, subsonic cruise, transonic cruise, and/or supersonic cruise. The oblique rotor-wing aircraft may comprise one or more of a fuselage, a rotor-wing, a thrust-v...
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WO/2018/058314A1 |
A control method, a control device (110), and an electronic device (100). The control method is used for controlling the electronic device (100). The electronic device (100) comprises a display (101) and a communication module (102). The...
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WO/2018/060392A1 |
Aircraft comprising a fuselage (1) divided by a floor (2) into an o upper volume (3) and a lower volume (4) through which joists (5) extend that support the floor and delimit, along with the fuselage and the floor, two side chambers (6),...
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