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Matches 201 - 250 out of 58,580

Document Document Title
WO/2017/207874A1
Connector (208) suitable for integration with a functional module (201), optionally a sensor module, to be attached as payload to an aerial vehicle (101), preferably unmanned aerial vehicle (UAV), by the connector, said connector compris...  
WO/2017/208468A1
[Problem] To provide a drone flight control system which makes it possible to improve the efficiency of pest control using a drone. [Solution] This drone flight control system 1 is provided with: a distance measurement module 101 for mea...  
WO/2017/207626A1
The invention relates to a passenger seat system (2) for a cabin (42) of a means of transportation (44) comprising: at least one passenger seat (4), which has a seat frame (6), which has a holding section (8) for holding seat devices (10...  
WO/2017/208179A1
The present disclosure describes displaying on a flight deck (12) graphical presentations indicative of performance limitations of an aircraft (10) resulting from an in-flight aircraft reconfiguration. The graphical presentations are co-...  
WO/2017/208037A1
The present invention relates to a folding propeller-hub assembly and applicable flight modes of the assembly. In particular, the present invention provides a folding propeller-hub assembly for VTOL aircraft and for improved aerodynamic ...  
WO/2017/206070A1
Disclosed are an airframe of an unmanned aerial vehicle and an unmanned aerial vehicle (100, 200, 300) comprising a body (10, 10', 10") and an arm (20, 20', 20") connected to the body (10, 10', 10"). The arm (20, 20', 20") is provided wi...  
WO/2017/208355A1
[Problem] To provide an unmanned aircraft flight control application which detects a person at low cost with high performance, and performs control so that an unmanned aircraft does not crash with the detected person. [Solution] This unm...  
WO/2017/207666A2
The invention relates to an air ship having a supporting structure (12) and a shell (10) that can be filled with a gas and which is tensioned by the supporting structure (12). According to the invention, said supporting structure (12) co...  
WO/2017/209827A2
A vibration attenuation system for attenuating vibrations in a mast of an aircraft includes a weight attached to the mast but free to orbit about the mast. The weight can be comprised of one or more weight assemblies. Embodiments can inc...  
WO/2017/207570A1
This invention relates an unmanned aerial vehicle (UAV) apparatus (20) having a frame structure (7), a plurality of primary arm structures (8) extending from the frame structure (7), a driving system (10) for driving the UAV apparatus, a...  
WO/2017/208758A1
This passenger boarding bridge is equipped with: a rotunda which is connected to a terminal building; a tunnel portion which is connected to the rotunda so as to be vertically movable; an elevation device which supports the tunnel portio...  
WO/2017/206078A1
An air combat device for an unmanned aerial vehicle, used in a scenario in which at least two unmanned aerial vehicles carries out air combats, and a victory or a defeat is determined according to the number of times of shooting down unm...  
WO/2017/207948A1
Method for forming a riblet on a component and riblet mould. This invention relates to a method for forming a riblet (3) on a component (1), characterised in that it comprises steps of: printing (106) the riblet on the component (1), com...  
WO/2017/209316A1
Provided is a method and a system for detecting a remote radiation dose rate by using a laser altimeter-based unmanned aerial vehicle. The method for detecting remote radiation, according to an embodiment of the present invention, allows...  
WO/2017/210595A3
Systems, devices, and methods for an aircraft having a fuselage (110); a wing (120) extending from both sides of the fuselage; a first pair of motors (132b, 133b) disposed at a first end of the wing; and a second pair of motors (142b, 14...  
WO/2017/208754A1
An information processing device 20 is provided, for example, to a vehicle 40. A control unit of the information processing device 20 provides flight control of an unmanned aerial vehicle 50, moves the same to a destination, and acquires...  
WO/2017/205997A1
Systems and methods are provided for transformation of an arm (104) of an unmanned aerial vehicle (UAV) (100) between a flight configuration and a compact configuration. The arm (104) may have multiple foldable sections (104-11, 104-12, ...  
WO/2017/206421A1
Provided is a pan-tilt (100) used for connecting a load (200). The pan-tilt (100) comprises a first support (11) and a second support (12) rotatably connected to the first support (11). The load (200) is connected to the first support (1...  
WO/2017/207870A1
The invention relates to a mattress (10) for an aeroplane. At the end of the mattress (10), there is a hood (15) inside the inner space (G) of which the mattress (10) may be rolled for storage. The hood (15) may be placed around a headre...  
WO/2017/210503A1
Photovoltaic (PV) device comprising an ultra-thin radiation-tolerant PV absorber mounted on a flexible film having an embedded persistent phosphor and having a plurality of interdigitated top and bottom contacts on the top of the PV abso...  
WO/2017/209974A1
A drone with a high-voltage trap seeks, identifies, pursues and destroys flying insects within a patrolling area. During its passive attracting mode, the drone lands on a designated ground site and attracts insects with light, sound, and...  
WO/2017/209796A1
Systems and methods for operating control surfaces of an aircraft. The method involves receiving, by an aircraft control system from one or more sensors, deflection information related to a shape and motion of an aircraft, and decomposin...  
WO/2017/206081A1
A rubber band launching device. The rubber band launching device is mounted on an unmanned aerial vehicle and is used for launching a rubber band (30) to shoot down an enemy unmanned aerial vehicle in an air battle of unmanned aerial veh...  
WO/2017/208157A1
An emergency exit assembly for an aircraft, including a window frame, a window assembly having an outer surface abutting the inner surface of the window frame around its perimeter, and retaining elements spaced around the perimeter of th...  
WO/2017/207968A1
A battery arrangement and a method of operating a battery arrangement for a solar powered aerial vehicle. The battery arrangement has a plurality of batteries arranged in a plurality of groups, the groups including a first battery group,...  
WO/2017/208424A1
An attitude estimation device (30) is provided with: a data acquisition unit (32) which acquires observation data; a ranging point coordinates calculation unit (33A) which, using positioning data, ranging data, actual attitude data, and ...  
WO/2017/210595A2
Systems, devices, and methods for an aircraft having a fuselage (110); a wing (120) extending from both sides of the fuselage; a first pair of motors (132b, 133b) disposed at a first end of the wing; and a second pair of motors (142b, 14...  
WO/2017/208272A1
Drones have reached technological maturity and very affordable costs, but their direct use in firefighting applications is still largely limited by problems concerning their range, their limited load capacity and their flight autonomy. S...  
WO/2017/203139A1
Support system (16) for a structural casing (10) of a turbomachine, which comprises: – a handling fitting (17) comprising a front edge (19) provided with one or more holes (26) for receiving one or more screws (24) for attachment to a ...  
WO/2017/202952A1
A solar panel (12) that comprise at least one photovoltaic cell (14) fixed on a support (16) comprising a frame (18). The support (16) comprises guiding means and a continuous wire (20), the wire (20) being strung on the frame (18) by be...  
WO/2017/203910A1
A method for designing the cross-sectional shape of the fuselage of a flying body having the fuselage extending in the roll axial direction, the section being taken on a plane perpendicular to the roll axial direction. This method is pro...  
WO/2017/201880A1
A delivery method utilized by an unmanned aerial vehicle, a control method, a control device, and a data storage medium. The delivery method comprises: an unmanned aerial vehicle transmits, to a wireless terminal, request information (S0...  
WO/2017/204592A1
An unmanned aerial vehicle according to an embodiment comprises a rotary wing, a motor, and an arm body, and includes: a plurality of arm units detachably coupled to a body; the body having a plurality of receptacles to be coupled to the...  
WO/2017/202630A1
The invention relates to a modular aircraft comprising a base unit (2), formed by at least two buoyancy modules (4), at least one functional module (6), and at least one coupling device (8). At least one of the buoyancy modules (4) has a...  
WO/2017/203126A1
The present application describes a casing (10), in particular an exhaust casing, for a turbomachine, comprising an inner hub (14) having an axis (A) of rotation and an outer annular ferrule (16) extending around the hub (14), said ferru...  
WO/2017/204998A2
Systems and methods include UAVs that serve to assist carrier personnel by reducing the physical demands of the transportation and delivery process. A UAV generally includes a UAV chassis including an upper portion, a plurality of propul...  
WO/2017/202222A1
An aerial vehicle and a foldable landing gear thereof, comprising: a first support frame provided with a first gear; a second support frame arranged below the first support frame and pivotally connected to the first support frame, the se...  
WO/2017/204892A1
Described herein are apparatuses that provided various features related to unmanned aerial vehicles. An example apparatus may include, (i) a support structure, (ii) at least one shaft coupled to the support structure via at least one swi...  
WO/2017/205255A1
A stoppable rotor, which includes a first and second blade and rotates about a substantially vertical axis, is stopped with the first blade pointing forward and the second blade pointing backward while the aircraft is mid- flight. Anti-t...  
WO/2017/201713A1
A mounting device for mounting a motion sensor comprises a mounting frame (1000) used to carry a motion sensor (3000); and a plurality of shock absorbing mechanisms (2000) connected to the mounting frame (1000), disposed at an interval, ...  
WO/2017/204320A1
Provided is a means and a method that can improve capturing performance of a space device in space by a capturing device provided with an adhesive part constituted by an adhesive. One embodiment of the present invention is a capture plat...  
WO/2017/201759A1
Disclosed are an optical housing (100), and a photographing apparatus (200) and an unmanned aerial vehicle using the optical housing (100). The optical housing (100) comprises: a mounting member (10) used for connecting to the unmanned a...  
WO/2017/203151A1
The present application concerns a method for manufacturing a casing (10'), in particular an exhaust casing, for a turbomachine, comprising the steps consisting of: a) producing casing sectors (30a), each casing sector (30a) comprising a...  
WO/2017/203552A1
In order to provide an unmanned aircraft with which it is possible to minimize damage due to crashes caused by malfunction during flight, etc., a flight route is set on map information including a fall avoidance region, a control is perf...  
WO/2017/204050A1
The objective of the present invention is to make it possible for an inspection operator to carry out a hammering sound inspection without it being necessary for the inspection operator to perform an operation to move an inspection devic...  
WO/2017/202146A1
A valve assembly for an aerostat and an aerostat. The assembly comprises a valve (1) with a valve opening (7), and a valve disc (2). The valve disc can move relative to the valve (1) to cover or open the valve opening (7). At least one o...  
WO/2017/203793A1
According to the present invention, a body part is provided with: a plurality of motors; and a plurality of rotors corresponding to the motors. The rotors are driven by output from the corresponding motors. The rotational speed of each o...  
WO/2017/203164A1
The invention concerns a spacecraft (2) comprising a body (4) having a face (6, 16, 18), a radiator (22) carried by said face and a thermal insulation device (28) capable of thermally insulating the body (4) from the space environment. T...  
WO/2017/203423A1
A safety device (D) for controlling a remotely piloted aircraft (RPA) comprises a first module (A) suitable to be installed on said aircraft (RPA) and a second module (B) suitable to be installed on a land base and connected by means of ...  
WO/2017/203590A1
A flight vehicle 3 is provided with a power reception device 20 that receives power by contactless charging through magnetic resonance, and a propulsion generation mechanism (motive-power motor 255, motor control device 254) that provide...  

Matches 201 - 250 out of 58,580