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Patent Searching and Data


Matches 151 - 200 out of 61,378

Document Document Title
WO/2018/172754A1
A propeller assembly (200) comprising a propeller hub (201) which can be driven about an axis and at least two propeller blades (203) each mounted to the hub at a point distal from the axis by pivoting means (203, 211, 212) alloying the ...  
WO/2018/174905A1
Some methods and configurations are disclosed for high bandwidth acquisition of magnetometer data with increased sensitivity. Some embodiments provide for increased bandwidth and sensitivity of the magnetometer by eliminating a reference...  
WO/2018/173158A1
A data acquisition device (1) comprises a balloon body (10), a first rope (21), a second rope (22), a first holding member (31), a second holding member (32), a first rail (41), and a second rail (42). The first rope (21) is connected to...  
WO/2018/171089A1
Disclosed is an aircraft (100) with a super high aspect ratio based on self-unfolding folding wing technology, the aircraft comprising: an aircraft body (10); a fixed wing (20); and a movable wing assembly comprising a first movable wing...  
WO/2018/172316A1
The invention relates to a positioning device (10) for positioning a manipulator (11) on an outer wall (101) of an aircraft (100), said device comprising at least one yoke (30) with a first yoke arm (58) and a second yoke arm (59), and a...  
WO/2018/173765A1
This control device (C) controls a linear actuator (1) that raises and lowers a landing gear (L) on the basis of the stroke displacement of the linear actuator (1) as detected by a stroke sensor (10). When the landing gear (L) is to be s...  
WO/2018/173040A1
The present invention provides a method for decelerating and redirecting an airborne platform, comprising the steps of retaining a flexible airfoil in non-deployed form in controllably releasable secured relation with each corresponding ...  
WO/2018/173994A1
The present invention addresses the problem of providing an unmanned aerial vehicle and an airbag device thereof capable of preventing damage to a payload even in the event of difficulties such as a mid-air collision or uncontrolled desc...  
WO/2018/172960A1
Embodiments of the present disclosure relate generally to galley trolley compartment doors that replace traditional trolley retainer latches used to secure trolleys when positioned in galley compartments. The galley trolley compartment d...  
WO/2018/172659A1
The invention relates to a heat transfer device (2) capable of transferring heat, comprising a housing (5) having a first main wall (12) and a second main wall (14), said housing (5) comprising an internal cavity (6) closed in a sealed m...  
WO/2018/172045A1
A passenger seat (10) comprises a backrest (14) and a seat element (16) that includes a first portion (16a) adjoining the backrest (14) and a second portion (16b) that can pivot between a rest position and an operational position. In the...  
WO/2018/175545A1
A passenger seat assembly includes a riser attached to an upper surface of a floor of the vehicle, a seat attached to an upper surface of the riser, and at least one shell portion attached to the upper surface of the riser. The riser inc...  
WO/2018/167473A1
The present subject matter relates to a system and a method for galactic transportation (100). The galactic transportation system (100) may comprise multiple rails (102) arranged in a first direction (103), a platform (108) for supportin...  
WO/2018/168565A1
[Problem] To provide a drone (unmanned flying body) capable of appropriately capturing images of root position portions and side surfaces of field crops in a field. [Solution] When a camera capable of capturing images in the rearward dir...  
WO/2018/167472A1
The present subject matter relates to an aircraft stabilization system (200). The aircraft stabilization system (200), amongst other components, may include multiple sensors (202), a processing unit (206), and multiple stabilization unit...  
WO/2018/170158A1
Embodiments of systems, devices, and methods are described that relate to module structures for use in forming a cabin interior of an aircraft (102). Many embodiments relate to a support structure (105) including a lattice (174) configur...  
WO/2018/165728A1
The present invention relates to an anchoring platform for captive aircraft that addresses one of the main problems when handling captive aerostats, which is the excessive workload required to switch same between flying and anchored stat...  
WO/2018/165916A1
Disclosed is a propulsion system for an unmanned aerial vehicle, the system comprising a propulsion motor (121) and a locking device (203). The propulsion motor (121) is used to drive a propeller (122) of the unmanned aerial vehicle (100...  
WO/2018/167840A1
The present invention is configured such that, for each RSO(n), in each combination of observation-possible time periods OT(h) for a number R(n) of requested observations, an evaluation value E(m,n,h) is integrated that was calculated by...  
WO/2018/165937A1
Disclosed is a distance-measuring sensor (1) and a plant protection unmanned aerial vehicle having the distance-measuring sensor (1), the distance-measuring sensor (1) comprising a housing (10), a distance-measuring module (20) arranged ...  
WO/2018/170427A1
Systems and methods are described herein for automatically monitoring a status or position of a vehicle component. Both powered and non-powered (or passive) systems are contemplated. The systems and methods utilize a sensor that signals ...  
WO/2018/169652A1
The present approach relates to the inspection of assets, such as assets having parts that move during operation. As discussed herein, operational data for the asset may be incorporated into planning or adapting the flight plan and/or op...  
WO/2018/167013A1
The invention relates to a device (1) for connecting an end of a first shaft to an end of a second shaft, the end of the first shaft having a radial groove, the device comprising: -a body (2) having a bore (21) into which the end of the ...  
WO/2018/170383A1
In an embodiment of the invention there is a cyclotronic actuator. The actuator is defined by having a high-voltage plasma driver connected to a first electrode. The first electrode is surrounded by a dielectric material. A second electr...  
WO/2018/165882A1
A propulsion system includes a propulsion motor (121) configured to drive a propeller (122) and an apparatus (203) for releasably coupling the propeller (122) to the propulsion motor (121). The apparatus (203) includes an engagement memb...  
WO/2018/169154A1
The present invention relates to a personal imaging system using a flying object and, in particular, to a personal imaging system which can acquire an image while following a user by using a balloon-type flying object. In the present inv...  
WO/2018/169066A1
Provided are a method for manufacturing a resin sheet 10 capable of substantially transmitting heat, the resin sheet 10, a method for manufacturing a structural body using the resin sheet 10, the structural body, and an airframe of an ai...  
WO/2018/166436A1
Disclosed is an unmanned aerial vehicle sliding-type mechanical arm device comprising a mechanical arm (1), a mechanical arm seat (2), and an electric motor impeller assembly (3) mounted on the mechanical arm (1), wherein the mechanical ...  
WO/2018/167471A1
The present subject matter relates to an aerial vehicle (100). The aerial vehicle (100) comprises a main body (102) having at least one suction motor (104) to suck-in atmospheric air, to amplify the sucked air and to eject the amplified ...  
WO/2018/169403A1
An airfoil-shaped body having a variable outer shape, comprising: a first skin, defining a suction surface, a second skin, defining a pressure surface and connected to the first skin at least at a leading edge and/or a trailing edge of t...  
WO/2018/168564A1
[Problem] To provide a simple method and a simple device capable of accurately measuring the water depth of a field, in particular, the entirety of a rice field. [Solution] By flying, in the air above a field, a drone (unmanned flying bo...  
WO/2018/167161A1
The invention relates to a method for determining, by reanalysis, a vibratory environment of a coupled vehicle/passenger system, the vehicle being subjected to external forces Fext and being coupled to a new passenger comprising x=l, ......  
WO/2018/165699A1
Disclosed is a water scoop for attachment to an aircraft having an associated water storage hopper. The water scoop is used for scooping water from a body of water. The water scoop has a boom pivotably attached and depending from the und...  
WO/2018/169454A2
´╗┐The invention relates to aeronautical engineering, and specifically to the construction of aviation engines and aeroplane braking devices, and can be used in a cascade-type thrust reverser rotating cascade made of polymer composite ma...  
WO/2018/165915A1
A method for planning a waypoint of an unmanned aerial vehicle (200) for an electronic device (100). The method comprises: in a case in a which an electronic device (100) does not establish a communication connection (300) with an unmann...  
WO/2018/169575A1
A passenger seat having improved backrest comfort features. The passenger seat has a backrest with a movable portion. In one example, the movable portion is defined by an upper backrest portion that can slide up and away from a lower bac...  
WO/2018/163298A1
A control device may comprise a control unit that controls a heating unit that heats an optical member provided forward of an image sensor. The control unit may cause the heating unit to heat the optical member when an imaging device is ...  
WO/2018/165313A1
An aerodynamic device for enhancing lift and reducing drag of an airfoil, comprising a central portion oriented in a substantially chordwise direction on the airfoil, and a first outer portion and a second outer portion arranged substant...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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) ...  

Matches 151 - 200 out of 61,378