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WO/2018/165498A1 |
An unmanned aerial vehicle includes at least one rotor motor configured to drive at least one propeller to rotate; and a micro hybrid generator system configured to provide power to the at least one rotor motor. The micro hybrid generato...
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WO/2018/164241A1 |
A rotary connector (1) is provided with: an electrically conductive shaft (2); a bearing (3) which rotatably supports the shaft (2); and a housing (4) in which the bearing (3) is disposed and which includes an electrode portion (11) at a...
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WO/2018/163156A1 |
A multirotor aircraft that includes a chassis, three or more vertical rotors, one or more free wings and on ore more fixed horizontal rotor. The free wing is attached to the chassis by an axial connection so that the angle of the free wi...
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WO/2018/164683A1 |
A system comprising a computer programed to identify a connected location of a vehicle at which a user device is connected to a first network and a disconnected location of the vehicle at which the user device is disconnected from the fi...
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WO/2018/162831A1 |
An electrodynamic assembly (3) for propelling a spacecraft (1) in orbit around a star having a magnetic field, comprising at least one coaxial cable (7) comprising an electrically conductive core (8) surrounded by a first electrically in...
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WO/2018/165192A1 |
A constant tension tether management system for tethered aircraft includes a ground station for operatively coupling to an unmanned aerial vehicle. The ground station includes a spool rotatably disposed within the ground station and adap...
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WO/2018/163666A1 |
[Problem] To provide a wing system with which it is possible to simply and stably switch an aircraft between rotary-wing flight and fixed-wing flight. [Solution] The present invention is characterized in that: a rotary wing for rotary fl...
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WO/2018/164756A1 |
Various embodiments include methods of offloading user equipment communication traffic between communications drones. The methods may include receiving, at a candidate communication drone, a replacement request from a requesting communic...
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WO/2018/161406A1 |
A quick installation and removal structure for a propeller comprises a propeller (1) and a positioning assembly. The propeller comprises a propeller main body (11) and a propeller blade (12). A positioning hole (111) is arranged at the p...
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WO/2018/161646A1 |
A propeller protection apparatus (130), an arm (120), and an unmanned aerial vehicle (100). The propeller protection apparatus (130) comprises a protective rod (132), a connecting rod (134), and a holding portion (136). One end of the co...
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WO/2018/163171A1 |
A vertical takeoff and landing (VTOL) light aircraft comprising: a tilt- wing comprising port and starboard wings; a power train having: an electric motor coupled to a rotor for providing the aircraft with thrust for flight mounted to ea...
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WO/2018/162772A1 |
The invention relates to an air-transportable device (100) for projecting pressurised liquid over a surface, comprising a rotating washing head and an inspection system (11) with LED bulbs and cameras. The air-transportable device (100) ...
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WO/2018/161107A1 |
A stretcher loading assembly including a support member operatively attachable to an aircraft floor, an elongate rail member attached to the support member, an elongate traverse beam movably attached to the rail member, and a trolley ass...
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WO/2018/161144A1 |
An aircraft static test adapter assembly comprising a static test head for performing testing at an aircraft static port on an aircraft body. The static test head is biased, and optionally supported by a biasing member extending in use f...
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WO/2018/165670A1 |
A system and method for facilitating a package exchange between a AGV and an UAV is disclosed, wherein the system and method includes authenticating the package exchange between the AGV and the UAV, wherein the AGV and the UAV each trans...
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WO/2018/164426A1 |
The present invention relates to a method for detecting a porphyry copper ore body by using hyperspectral imaging of malachite, the method comprising the steps of: obtaining hyperspectral image data of an alteration zone indicated by alt...
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WO/2018/163692A1 |
This heat radiator for an aircraft cools a heat source mounted on the aircraft and is provided with a heat radiation section (3) having recesses or protrusions formed on the surface thereof which comes in contact with a main stream, the ...
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WO/2018/163991A1 |
Provided is a wireless relay system with which it is possible to quickly start relaying wireless communication between a stationary base station and a user device after moving to a target position. The wireless relay system is provided w...
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WO/2018/164170A1 |
Provided is an ornithopter that does not require additional devices such as a tail or rudder, in which each of the lead/lag angles of the left and right wings is changed nonsymmetrically, rotational moment is generated from the differenc...
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WO/2018/163159A1 |
A multirotor aircraft that includes a chassis, vertical rotors, foldable wings, and a means for deploying and folding the foldable wing. The foldable wing is attached to the chassis and the means for deploying and folding the foldable wi...
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WO/2018/165057A1 |
An aircraft can include a frame and a plurality of electrical rotors coupled to the frame. The aircraft can further include a control system physically coupled to the frame and communicatively coupled with each of the plurality of electr...
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WO/2018/161193A1 |
A four-axis aerial vehicle provided with lights comprises a control circuit (4), a wireless transceiver module (5), motors (11), a battery (9), a fuselage (10), and a top anti-collision rod (1). The control circuit (4) is connected to vo...
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WO/2018/163571A1 |
An information-processing device operating in an imaging device mounted in a mobile entity, which, when image capture by the imaging device fails, notifies the mobile entity to the effect that image capture has failed.
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WO/2018/163699A1 |
[Problem] To provide a control system for a flight vehicle that causes the flight vehicle to fly autonomously without the use of GPS and without storing flight routes, and a control device for the same. [Solution] A control system 2 for ...
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WO/2018/165093A1 |
A system and method for acquiring store comprise establishing an electronic communication between a mobile device and a unmanned vehicle; tracking in a store by the unmanned vehicle a customer having the mobile device; collecting data by...
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WO/2018/164710A1 |
A boarding guidance system includes a beacon (202A) associated with a passenger seat (400A). The beacon is configured to communicate (506) with a passenger guiding device (102) and determine a distance between the passenger guiding devic...
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WO/2018/158767A1 |
Generally, a vehicle comprising at least one hydrogen releasing element is provided. The vehicle can include at least one hydrogen releasing element coupled to a body of the vehicle. The vehicle can include a hydrogen combustion region p...
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WO/2018/158392A1 |
A method (600) for testing control logic for a propeller driven by a gas turbine engine of an aircraft includes overriding (602) a signal indicating the aircraft is operating in a ground mode. The method can further include testing (604)...
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WO/2018/159968A1 |
A body protection apparatus for use in a vehicle for carrying people according to the present invention is a seat employed in a vehicle in/on which people ride, and comprises a safety device for covering a passenger so as to protect the ...
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WO/2018/158511A1 |
The present invention relates to a redundant and dissimilar system (10) for monitoring the status of contactors (22) of an aircraft control stick (20). This monitoring system (10) comprises at least one electrical power source (2), at le...
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WO/2018/158756A1 |
A vehicle arresting system includes a base layer comprising a crushable aggregate (54) and a cover layer comprising a cementitious material having an oven-dry density of 1602 kg/m3 (100 Ib/ft3) or less. The system also may include an arr...
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WO/2018/158255A1 |
A control system (20) has both a first and second processing modules (22, 24) for controlling retraction and extension of a landing gear assembly (14) on an aircraft (10). The processing modules can operate independently of each other an...
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WO/2018/158586A1 |
An aerial delivery container is provided for release from an aircraft, the container comprising a housing comprising a hold for containing a payload; and an impact absorbing structure provided to the housing for absorbing the force of an...
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WO/2018/157633A1 |
Provided is a shock absorber (100), comprising a connecting portion (102) and buffering portions (101) respectively located on either end of the connecting portion, wherein the cross-sectional size of the shock absorber gradually decreas...
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WO/2018/160215A1 |
This invention relates to magnetic propulsion systems. Previously, motors required electronic control systems for efficiency. Embodiments of the present invention use a first axel (120) joined to a first permanent magnet (113) of a first...
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WO/2018/157393A1 |
An aerial dispensing method is disclosed. The method may comprise obtaining a wind velocity, the wind causing a drift to a substance dispensed from an unmanned aerial vehicle (UAV), and controlling one or more components of the UAV based...
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WO/2018/158757A1 |
A vehicle arresting system includes a base layer comprising a crushable aggregate and a cover layer comprising a cementitious material having an oven-dry density of 1602 kg/m3 (100 lb/ft3) or less. The system also may include an arrestor...
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WO/2018/157426A1 |
A propeller, a power assembly and an aircraft, the propeller comprising a propeller base and a blade (1) connected thereon. The blade (1) has an angle of attack of 14.05°±2.5° and a chord length of 11.94mm±5mm at a position where the...
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WO/2018/158531A1 |
The invention relates to a device and a method for the connection and linear separation of two elements (1, 2), such as the two stages of a spacecraft, consisting in using a tube (4) containing a pyrogenic-type material (5) and a glue (3...
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WO/2018/160764A1 |
A hose mounting assembly that includes a mounting member having a base and a main body portion. The main body portion includes first and second ends, a curved tie tunnel defined therethrough, and a curved mounting surface. The base inclu...
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WO/2018/158576A1 |
One type of kite system for the extraction of energy from the wind includes a kite connected to a base unit using a tether. The kite system comprises: an anhedral wing having wing tips and a central part located vertically higher than th...
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WO/2018/160740A1 |
A three-axis spacecraft including a spacecraft body including first and second opposing radiator/equipment panels, first and second opposing mounting panels, an earth deck and a zenith deck. The zenith deck faces the Earth when the space...
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WO/2018/160559A1 |
In a preferred embodiment, a retrofittable PRM lavatory complex occupies the same footprint as a preexisting outboard dual-lavatory complex. The two lavatories are separated by a common articulating wall that is typically positioned in a...
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WO/2018/158766A1 |
An airborne vehicle made of thermally non-conductive materials and method for thermal conduction in an airborne vehicle are disclosed. The airborne vehicle comprising at least one structural element made of material with high thermal con...
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WO/2018/159256A1 |
A takeoff and landing device (5) is provided with: a fixed device (55) or a communication unit (57) that can switch between a first state in which an unmanned aircraft (3) is prevented from taking off from a host device, and a second sta...
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WO/2018/157833A1 |
An unmanned aerial vehicle: arm assemblies (12, 13, 14, 15) of the unmanned aerial vehicle may be folded and unfolded relative to a casing so as to facilitate transportation and storage of the unmanned aerial vehicle. At the same time, t...
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WO/2018/157287A1 |
Provided are a method and device for controlling the landing of an unmanned aerial vehicle, and an unmanned aerial vehicle. The method for controlling the landing of an unmanned aerial vehicle comprises: receiving status information abou...
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WO/2018/158927A1 |
The present invention highly precisely estimates the shape of an object irrespective of whether there are variations in the altitude of the shape of the object, and avoids a collision between the object and a flying vehicle during flight...
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WO/2018/158686A1 |
A remote piloted aircraft (1) comprising a secondary flight assembly (4) adapted to intervene in case of failure of the aircraft (1) or in an emergency, said secondary flight assembly (4) being provided with an additional control unit (5...
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WO/2018/158549A1 |
The aircraft (10) comprises a fuselage (11) and a rhombohedral wing structure (12) comprising front wings (13, 14) mounted on a front wing-root support (17) and rear wings (15, 16) mounted on a rear wing-root support (18). One end of eac...
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