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Matches 201 - 250 out of 59,481

Document Document Title
WO/2018/045575A1
A propeller assembly, a power system, and an aerial vehicle. The propeller assembly (13) comprises first propellers (131) and second propellers (132) that are disposed at intervals. Each first propeller (131) comprises a first propeller ...  
WO/2018/045578A1
A load assembly and an unmanned aerial vehicle hung with the load assembly. The load assembly comprises a cradle head and a stand (13). The cradle head comprises a second mounting portion (11) and a cradle head main body (12). The second...  
WO/2018/046990A1
Ground stations and methods for pre-flight health and safety check of PEM fuel cell powered unmanned aerial vehicles are disclosed. The ground stations are capable of reconditioning UAV fuel cell stacks and refilling the hydrogen supply....  
WO/2018/048565A1
A method for operating a propulsion system of an aircraft includes moving a plurality of forward and aft propulsors to a vertical thrust position. While in the vertical thrust positions, the method also includes providing a first forward...  
WO/2018/046124A1
The invention relates to a vehicle (101), to a system comprising such a vehicle (101), and to a method for operating an autonomously free-flying drone (103) in a system. The vehicle (101) according to the invention comprises: a platform ...  
WO/2018/048708A1
In some embodiments, methods and systems of identifying at least one pest in a crop-containing area include an unmanned vehicle including a visible light video camera configured to detect a pest in the crop-containing area and to capture...  
WO/2018/049163A1
A charging system for drones has a base structure connected to a power grid, a connector extendable from the base structure and ending in a charging interface compatible with a charging port of a drone, and a computerized controller at t...  
WO/2018/045627A1
An unmanned aerial vehicle (100) and a connecting assembly thereof. The connecting assembly comprises a column (130) and a locking member (140) and is configured to connect a first connected member (110) and a second connected member (12...  
WO/2018/048615A1
An apparatus and method for deicing a surface (66) upon which ice accumulates, on for example an aircraft wing. The apparatus and method for the deicing module include an actuating component, a casing (28), and a movable member (36). The...  
WO/2018/042676A1
The purpose of the present invention is to make the flight time of an unmanned flying body longer. This unmanned flying body comprises: a plurality of rotary blades; a plurality of control devices connected to the rotary blades; and a fl...  
WO/2018/043821A1
The present invention provides a route guiding system, using weather information, of an unmanned aerial vehicle, a method thereof, and a recording medium recorded with a computer program. That is, the present invention: calculates a plur...  
WO/2018/045116A1
An airfoil body may include a plurality of tubercles along a leading edge of the airfoil body and a plurality of crenulations along a trailing edge of the airfoil body, wherein at least one of a position, a size, and a shape of the plura...  
WO/2018/045253A1
The present invention relates to a rotor assembly where associated electric motors are configured to rotate the rotor, control the collective pitch of the rotor/assembly, and/or control the cyclic pitch of the rotor/assembly, by varying ...  
WO/2018/042106A1
A rocket engine having improved stability during its starting phase, the rocket engine (1) comprising a divergent (13) and a securing system (40) configured to retain the divergent (13) when the rocket engine (1) is started, the securing...  
WO/2018/044272A1
Described are headrests with a structural support surface and a torque hinge. The torque hinge includes a rotatable portion, a ball joint, and a plate assembly. The ball joint has a ball portion connected to a shaft. The ball portion is ...  
WO/2018/042610A1
In order to address the problem of providing an unmanned aircraft that is capable of maintaining an airframe horizontally over a water surface and capable of smoothly taking off from and landing on water, this unmanned aircraft having a ...  
WO/2018/043988A1
Disclosed are an unmanned aerial vehicle for aerial reconnaissance, which performs object detection and object hitting on the basis of image information, and an unmanned defense system and method using the same. The unmanned aerial vehic...  
WO/2018/043838A1
A virtual experience apparatus for aviation leisure sports according to the present invention comprises: a main frame having a vertical column in an inner region of which a receiving space is formed; a bottom frame connected to the main ...  
WO/2018/042117A1
The present invention relates to a nacelle for an aircraft turbojet engine, comprising: an air inlet (107), comprising a leading edge of the nacelle extended forwards by an inner wall and by an outer wall of the air inlet; a fan cowling ...  
WO/2018/044935A1
Systems and methods are disclosed for managing energy of a UAV during flight. In particular, the disclosed systems and methods assist in safely returning a UAV to ground while reducing diversionary time for providing energy to the UAV. I...  
WO/2018/042089A1
The unmanned aerial vehicle (1) comprises first control means for controlling the flight of said vehicle (1), a load-carrying means (6), movable about at least two axes (F, F1), at least one means (7) for identifying and monitoring an an...  
WO/2018/043665A1
[Problem] To provide a technology for reliably landing a flying body on a ground surface that is covered with a granular medium. [Solution] The present invention is a leg part structural body which can support a body part of a flying bod...  
WO/2018/044182A3
A method of folding and deploying the wings of an unmanned aerial vehicle with tube-launcher take-off in which the wings are folded along the fuselage, wherein the wings are folded along the fuselage (2), and then a section of the wings ...  
WO/2018/042927A1
[Problem] To provide a mechanism of radio communication for a device that flies around freely in a three-dimensional space. [Solution] A circuit provided with: an acquisition unit that acquires information relating to a flight; and a mea...  
WO/2018/043737A1
This flying mobile unit comprises a hull, a wheel, a propulsion device, and a control unit. The wheel has an axis of rotation oriented in the same direction as the direction of a thrust force to be produced by the propulsion unit. The co...  
WO/2018/039975A1
An unmanned movable object (410) comprises a motion mechanism (426) that can be coupled between the main body (411) of an unmanned movable object (410) and the optoelectronic scanning module (450). The motion mechanism (426) can include,...  
WO/2018/039784A1
A ducted fan unmanned aerial vehicle (UAV) docking station is provided. The docking station comprises: a guide sized to receive a ducted fan UAV; and a housing communicatively coupled to the guide. The housing comprises: a storage assemb...  
WO/2018/042238A1
The purpose of the invention is to create a device and a method to allow for automated positioning of an unmanned aerial vehicle on a landing platform. The device comprises of a landing platform with a landing base and a landing surface ...  
WO/2018/043820A1
The present invention provides a route guiding system, using weather information, of an unmanned aerial vehicle, a method thereof, and a recording medium recorded with a computer program. That is, the present invention: determines whethe...  
WO/2018/039922A1
A control method and a control system for an electronic speed controller, a flight controller and an unmanned aerial vehicle, which are used to eliminate the potential safety hazards occurring in an unmanned aerial vehicle due to the ins...  
WO/2018/040426A1
An unmanned aerial vehicle, comprising a body (1) and wings (2). The body (1) comprises an upper body part (11) and a lower body part (12). The lower body part (12) is provided with a cargo compartment (121) for accommodating cargoes. A ...  
WO/2018/043116A1
To provide a small flying body in which it is possible to mitigate impact when the flying body falls and collides with the ground, etc. A small aircraft that has an airbag device and a maximum length of 2 m and that is capable of flying ...  
WO/2018/044243A1
This invention is system designed in particular to separate the plane's black box (data recording box) in case of being exposed to an accident that causes its drowning in the sea, ocean, or, elsewhere waters, yet in a following step to t...  
WO/2018/040312A1
Disclosed is an unmanned aerial vehicle of folding wing-type, comprising a fuselage (1) and arms, wherein the arm comprises a non-folding section (2), a folding mechanism (3) and a foldable section (4); the non-folding section (2) is fix...  
WO/2018/041254A1
A carrier for an air-dropped article, comprising a housing (40) for carrying an article, a floater (41) provided on an outer surface of the housing, and a retarder (42) provided on an upper part of the housing. The floater (41) comprises...  
WO/2018/041255A1
An ejecting device, comprising a cabin (30) provided on a transportation tool, and a push-out part electrically connected to an ejection triggering circuit of the transportation tool. The push-out part comprises a push rod (31). The cabi...  
WO/2018/041253A1
A black box control method comprises: acquiring current flight data of an aircraft, wherein the flight data comprises a collision signal, a loss-of-control signal, and a stall signal; determining, according to the flight data, whether th...  
WO/2018/039994A1
Disclosed is a driving device (10) used for being connected to an propeller (20), the driving device (10) comprising a main body part (12), and a driving shaft (15) arranged on the main body part (12) and capable of rotating relative to ...  
WO/2018/044074A1
The present invention relates to a method for inhibiting crack growth in a wall portion. A method for inhabiting crack growth in a wall portion according to an embodiment of the present invention comprises: an injection step for injectin...  
WO/2018/043284A1
Provided is a base station device, comprising: a wireless communication unit which wirelessly communicates with an unmanned aerial vehicle; and a control unit which, if it is determined that an emergency situation has occurred with the u...  
WO/2018/040116A1
An unmanned aerial vehicle (100, 200, 300), comprising: a rack (110, 210, 310) which comprises a body (110a, 210a, 310a) and an arm (110b, 210b, 310b); the arm (110b, 210b, 310b) is connected to the body (110a, 210a, 310a), and the arm (...  
WO/2018/040765A1
Disclosed is an aircraft with a replaceable protective cover, comprising an aircraft body (1), wherein the aircraft body (1) has a duct (2), the duct (2) is internally provided with a propeller (4), a plurality of clamping grooves (21) a...  
WO/2018/041992A1
The invention relates to a preform (3) defining two parts (21, 23) and comprising: a first group (C1) of layers of warp yarns, which is external in the first part, a second group (C2) of layers of warp yarns immediately beneath said firs...  
WO/2018/038323A1
The present invention relates to an intermeshing rotary-wing aircraft, comprising: a first rotary blade portion including a first blade and a second blade; a second rotary blade portion including a third blade and a fourth blade; a first...  
WO/2018/038493A1
Provided is a motor for a drone comprising: a rotary shaft; a stator including a hole in which the rotary shaft is disposed; a rotor disposed outside the stator; and a housing coupled to the stator, wherein the stator comprises a stator ...  
WO/2018/038822A1
A multicopter aircraft with a wide span rotor configuration is disclosed. In various embodiments, a multicopter as disclosed herein includes a fuselage and a plurality of rotors. The plurality of rotors includes inner rotors and outer ro...  
WO/2018/037268A1
Alternate manners of utilizing areas of, principally, cargo areas of commercial passenger aircraft are described. These manners of utilizing preferably occur during cruise or other non-TTL portions of flight and provide passengers with a...  
WO/2018/038438A1
Disclosed is an unmanned automated hook coupling device comprising a device coupling part, a propulsion member, a transmission member, a reception member, hook tongs, and a transmission member, wherein the propulsion member adjusts the p...  
WO/2018/038819A3
Methods, systems, computer-readable media, and apparatuses for determining a flight route for a flight of an unmanned aerial vehicle (UAV) are presented. The flight-specific route for the UAV is determined dynamically during the flight o...  
WO/2018/037796A1
This flight device is provided with a base body, thrusters, an attitude detection unit, an abnormality detection unit, and an attitude control unit. The plurality of thrusters are provided to the base body, and are provided with propelle...  

Matches 201 - 250 out of 59,481