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WO/2018/176242A1 |
An agroforestry chemical spraying system based on the mechanics-related intelligent control technology. The system comprises: an agroforestry system, an unmanned aerial vehicle system, and a system terminal. The agroforestry system compr...
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WO/2018/183996A1 |
A propulsion system for an orbiting vehicle such as a low-Earth orbit (LEO) satellite includes a set of surfaces over which a gas passes during orbital flight, and a plurality of electrodes on the surfaces. The electrodes are configured ...
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WO/2018/176152A1 |
Embodiments of emergency locating devices are described. In one embodiment, an emergency device includes a fixed part and a breakaway part, with the fixed part sized and shaped to receive the breakaway part, and wherein the breakaway par...
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WO/2018/179247A1 |
This cargo loading board comprises: a flat slideboard part with raised ribs arranged adjacently on the surface in the direction of cargo conveyance; a flat support part that is provided so as to create a height difference with the slideb...
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WO/2018/180086A1 |
The present invention is provided with a resistance generation mechanism which is provided with: a base ring 2 disposed on one space vehicle A; a one-side capturing ring 3 that comes into contact with the other-side space vehicle B; six ...
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WO/2018/178739A1 |
Invention relates to an open vertical wind tunnels for simulating a free fall sky diving. An open vertical wind tunnel comprising: a frame structure (1), a power unit (2) and a fan assembly (3); a flow straightening assembly (4) comprisi...
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WO/2018/178751A1 |
Broadcasting geolocation information of an Unmanned Aerial Vehicle (UAV) from the UAV by determining current geolocation of the UAV by communicating with a geolocation service and utilizing the geolocation service to geolocate the UAV. T...
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WO/2018/180534A1 |
In order to solve the problem in which a flight vehicle flies only in locations having poor communication quality and retained data cannot necessarily reach the ground, this device communicates with a flight vehicle, wherein the device i...
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WO/2018/183786A1 |
A support arm (12) includes: a body portion disposed between a seat end (20) and a table end (18); wherein the support arm (12) comprises a composition comprising a polymeric material, a metallic material, a thermoset material, an elasto...
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WO/2018/183535A1 |
An unmanned aerial vehicle with deployable components (UAVDC) is disclosed. The UAVDC may comprise a fuselage, at least one wing, and at least one control surface. In some embodiments, the UAVDC may further comprise a propulsion means an...
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WO/2018/182883A1 |
Methods, devices, and systems of various embodiments are disclosed for operating a propeller assembly for use with a UAV. Various embodiments include a propeller assembly including a pivotal arm, a propeller mounted on the pivotal arm, a...
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WO/2018/178589A1 |
The invention concerns an aircraft propulsion unit (1), comprising: - a turbojet engine (3); - a lateral pylon (7), connected to the fuselage of said aircraft, - a nacelle (5) mounted on said lateral pylon (7), comprising: - an upstream ...
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WO/2018/178776A1 |
The present disclosure relates to a control system for a retractable belly mounted payload in an Aerial vehicle for retraction, pan and tilt movements of the payload, comprising a first mechanism to rotate the payload about a vertically ...
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WO/2018/178750A1 |
A method and apparatus in an unmanned aircraft traffic management system are described. Flight data is received from a network device. The flight data includes data about an event related to a flight of the UAS in an airspace, a timestam...
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WO/2018/183750A1 |
A panel assembly that is configured to be secured to a frame that includes a panel having a top and a bottom, a first bracket assembly and a second bracket assembly. The first bracket assembly includes a first pivot member and a first br...
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WO/2018/178145A1 |
The invention concerns a mechanical reduction gear (156) comprising: - an input shaft (158) rotated by a motor, - an output shaft (160) coaxial with the input shaft (158), - an endless screw (250) mounted coaxially on the input shaft (15...
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WO/2018/178908A1 |
An aircraft lighting system includes a light unit configured to emit light, a portable measurement device, and a control unit. The portable measurement device is configured to measure at least one attribute of the light emitted from the ...
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WO/2018/183428A1 |
In some embodiments, systems, apparatuses and methods are provided herein that enable delivery of retail products. Some embodiments provide delivery systems comprising: a package support frame comprising first and second package supports...
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WO/2018/177449A1 |
The invention relates to a cabin lining element (18') for an aircraft cabin arranged in the interior of an aircraft fuselage structure (12), having a fuselage structure side (30) and a cabin side (32). On the fuselage structure side (30)...
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WO/2018/182797A1 |
This document describes a system and method through which unmanned aerial vehicles (UAVs) and other vehicles (e.g., unmanned underwater vehicles (UUVs), also known as autonomous underwater vehicles (AUVs), unmanned water-surface vehicles...
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WO/2018/177873A1 |
The invention relates to an automation system (10), comprising: a control device (20) for controlling at least one machine, at least one unmanned aircraft (40, 40a, 40b, 40c, 40d), the control device (20) being designed to control the un...
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WO/2018/176291A1 |
Hollow motor apparatuses and associated systems and methods for manufacturing the same are disclosed herein. In representative embodiment, a hollow motor apparatus includes a rotor assembly rotatable about a rotation axis, a stator assem...
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WO/2018/183040A1 |
An load adaptive lift assist for a pivoting stowage bin includes an assembly housing having an interior and a pair of opposing end fittings. A piston rod is disposed within the assembly housing and operatively coupled to one of the end f...
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WO/2018/178729A1 |
The present disclosure relates to seating apparatus. In particular, the present application relates to an aircraft seat (1). The aircraft seat (1) includes a seat chassis (4) and a seat assembly (5). The seat assembly (5) has a seat pan ...
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WO/2018/182576A1 |
A system that includes a vehicle fuel-receiver comprising a port located on a vehicle surface; and an onboard computer programmed to: send a fuel delivery request to an unmanned aerial vehicle (UAV); actuate the port to permit the UAV to...
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WO/2018/183731A1 |
A solid state liquid-chilled bar unit for an aircraft galley includes a multilevel frame dimensioned to fit the galley and including stacked slots, each slot configured to fit a compartment. Warmer compartments include a liquid thermoele...
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WO/2018/182564A1 |
A drone pod includes a pod shell, a door, a motor and a computer. The pod shell includes a base, a top, and a wall. The top has an opening sized to receive a drone. The wall connects the base and the top. The door is disposed in the open...
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WO/2018/177474A1 |
The invention relates to a receiving apparatus (200, 300, 400, 500) for packages (1) or packets delivered by air, having an enclosure (201, 301) that protects against weathering and has an opening (202) for inserting a package (1) or a p...
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WO/2018/182944A1 |
An autonomous drone integrated with wide bandwidth, high energy acoustic wave generators sent to evict and eradicate agricultural pests within a patrolling area. The drone hovering close to a plant bombards its leaves and fruits with hig...
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WO/2018/178187A1 |
The invention relates to a dynamic force generator (100) comprising - a supporting shaft (110); - a first rotor (120) comprising: an internal bore (121) housing said supporting shaft (110) and bearings (R1, R2) arranged between the suppo...
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WO/2018/178276A1 |
The present invention essentially relates to an arrangement of individual seats intended to be installed in a cabin of an aeroplane (59) comprising at least one module (M1) of two seats (13.1, 13.3) arranged facing each other, said modul...
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WO/2018/182496A1 |
A device configured to deploy a retractable landing gear having a main landing gear (110) and a secondary landing gear (120) is provided. The device comprises an electrical motor (130) in driving connection with a drive shaft (140) conne...
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WO/2018/182448A1 |
The invention relates to methods for rescuing the crew of a light helicopter in the event of an emergency involving loss of control in uncontrolled freefall. The technical result of the invention is a more effective method for rescuing t...
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WO/2018/178566A1 |
A method for controlling a multi-engine bay (10), according to which the following steps are carried out: a) the bay is controlled so that it ensures a desired thrust and so that each engine is used in accordance with a set of operating ...
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WO/2018/178948A1 |
An air intake unit (3) for an engine of an aircraft (1); the intake unit (3) has: a tubular housing (4); a first inlet opening (7) which is obtained through an outer wall (6) of the tubular housing (4) and through which external air can ...
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WO/2018/178565A1 |
A device for temporarily increasing power (13) for increasing the power of at least one first turbomachine (5A) and at least one second turbomachine (5B), said device comprising a coolant reservoir (14), a first injection circuit (16A), ...
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WO/2018/175037A1 |
Electrically operated propellant thrust assist supplements an airplane's takeoff, landing or inflight maneuvers. Unlike conventional SRM propellants, the burn rate of the electrically operated propellant can be varied via an electrical i...
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WO/2018/172815A1 |
The invention relates to multicopter frames. The multicopter frame according to the present invention comprising: (i) a first housing (1) and a second housing (2), both the first housing and the second housing are substantially centrally...
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WO/2018/173072A2 |
System for precision irrigation is disclosed, the system comprises a main line. A plurality of sub main lines, wherein the plurality of sub main lines are configured to receive fluid from the main line. Further the system comprises a plu...
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WO/2018/174943A1 |
An air inlet for a flight vehicle engine includes at least one fin, at least partially upstream of a throat of the engine. The fin protrudes into a flow channel, extending beyond a boundary layer into the main airstream in the inlet. The...
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WO/2018/172252A1 |
The invention relates to a cabin air inlet module (16). The cabin air inlet module (16) has a flow channel body (8). The flow channel body (8) has at least one wall which delimits a flow channel in which feed air (5) is supplied to a zon...
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WO/2018/172812A1 |
The invention relates to an aircraft braking landing device and to the emergency landing of an aeroplane. The device comprises a shock-absorbing platform consisting of elastic cells fastened to each other and filled with a gaseous mixtur...
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WO/2018/172737A1 |
A vehicle comprising: a fuel store (104) configured to store a fuel, the fuel comprising a hydrocarbon; a fuel reformer (108) coupled to the fuel store (104) and configured to: receive an input comprising the hydrocarbon; and process the...
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WO/2018/175606A1 |
An aircraft for use in fixed wing flight mode and rotor flight mode while maintaining a horizontal fuselage is provided. The aircraft can include a fuselage, wings, rotor, and a plurality of engines. The rotor can comprise a wing attachm...
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WO/2018/172666A1 |
The invention concerns a method for monitoring at least one engine (2) of an aircraft (1), the aircraft comprising a passenger cabin (4), the method comprising the following steps: - a step of acquiring (110) a signal that is at least in...
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WO/2018/172046A1 |
A passenger seat (10) comprises a backrest (14), a seat element (16) and a size increasing mechanism (30) which is designed to convert a weight (FG) acting on the seat element (16) when a user sits in the passenger seat (10) into an incr...
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WO/2018/171239A1 |
A negative pressure low dead oil anti-bubble aeroplane fuel tank apparatus, comprising a fuel tank outer shell, an oil suction hose (3) arranged inside the fuel tank outer shell, a fueling port (9) arranged on the fuel tank outer shell, ...
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WO/2018/173348A1 |
This low-temperature tank is provided with a container main body (10). The container main body (10) includes: a metal liner (13) that forms a storage space; and a wall member (14) wound on an outer peripheral surface (13a) of the metal l...
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WO/2018/175694A1 |
Disclosed herein is a modular aerial vehicle system having a fuselage module configured to couple with a plurality of lift generation modules. The modular aerial vehicle system may comprise a fuselage module and a lift generation module....
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WO/2018/175931A1 |
Display systems for a vehicle are contemplated that comprise a seat display unit coupled with a display screen, where the display screen is affixed to a seat back and the seat display unit is disposed within the seat back. The display sc...
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