Login| Sign Up| Help| Contact|

Patent Searching and Data


Matches 551 - 600 out of 61,001

Document Document Title
WO/2018/091899A1
An LED lighting assembly(1)is provided comprising a cassette (2), a lens, a printed circuit board (6) having at least one LED light source mounted thereon wherein the lighting assembly comprises a collimator (12) provided between the LED...  
WO/2018/090808A1
A cradle head motor, a cradle head and an aircraft. The cradle head motor comprises: a rotor (2), a stator (1) and a magnetic ring (3); a first wire threading hole (11) is provided in a middle portion of the stator (1); a second wire thr...  
WO/2018/091097A1
A conveyor assembly comprises an item conveyor and a connector unit for loading of luggage or parcel items to the item conveyor or unloading of luggage or parcel items from the item conveyor. The conveyor assembly comprises an anchoring ...  
WO/2018/093825A1
Passenger seats having improved comfort emergency egress solutions for mini suites or other types of passenger seats that have a privacy screen, wall, or sliding door that divides the passenger seat from the aisle area or other common ar...  
WO/2018/090325A1
Disclosed are a survival item dropping device (100) and an unmanned aerial vehicle. The survival item dropping device (100) comprises a hook unit (1) and at least two rope assemblies (2) used for connecting to different survival items to...  
WO/2018/093382A1
A latch system that includes a paddle button assembly having a button that is movable between a home position and an actuation position, a latch assembly that includes a striker assembly and a hook assembly, and a cable that extends betw...  
WO/2018/090646A1
Disclosed are a boosting method and boosting device (100) for a tethering aircraft, and a tethering aircraft system. In the process of controlling a tethering aircraft executing a flight mission, determining, according to current locatio...  
WO/2018/090281A1
A manually detachable locking mechanism for connecting parts of an unmanned aerial vehicle (UAV) comprises: a first engaging means (25) associated with a first part of the UAV, a second engaging means (35) associated with a second part o...  
WO/2018/091901A1
An LED lighting assembly (1) is disclosed which is arranged to produce a predetermined non-circular light pattern the LED lighting assembly comprising a cassette (2), a lens, a printed circuit board (6) having at least one LED light sour...  
WO/2018/091475A1
The invention relates to an electrohydraulic module (1) for driving at least one component of an aircraft, in particular an airplane, wherein the electrohydraulic module (1) comprises at least one electric motor (2) and at least one comp...  
WO/2018/091900A1
An LED lighting assembly (1) comprising a cassette (2), a lens, a printed circuit board, PCB, (6) having at least one LED light source mounted thereon, the lighting assembly comprising an LED driver circuit arranged to maintain conductio...  
WO/2018/093607A1
A cinched parachute is disclosed. In various embodiments, a cinched parachute as disclosed herein includes a canopy comprising one or more sections of canopy material, and a device integrated with the canopy that controls dimensions of t...  
WO/2018/086128A1
A rotor assembly (30) and an unmanned aerial vehicle (100). The rotor assembly (30) comprises a motor (31), a propeller (32), and a connection assembly (33) for connecting the propeller (32) to the motor (31). The motor (31) comprises a ...  
WO/2018/089531A1
An autonomous or semi-autonomous device or vehicle, such as a drone, and method for controlling the same, the method including sensing a physical manipulation or an aspect of a physical manipulation of the autonomous or semi-autonomous d...  
WO/2018/087671A1
The present disclosure provides an aircraft (10), as well as systems and methods for reducing current flow to electrical systems onboard an aircraft (10). A signal return network (220) is spaced from a composite structure (210) and first...  
WO/2018/089205A1
Embodiments relate generally to flush plates (14) having noncircular openings. In a specific example, the flush plate has a shark-fin shaped opening with an extending fin along a tail portion.  
WO/2018/086202A1
An unmanned aerial vehicle battery compartment (100), and unmanned aerial vehicle (200) having the unmanned aerial vehicle battery compartment (100). The unmanned aerial vehicle battery compartment (100) is used to accommodate an unmanne...  
WO/2018/087353A1
The invention relates to a device (1) for encoding information between a plurality of normally closed switches (P1...Pn) arranged on an operating lever (2) and a control device (9), said switches being connected in series between a volta...  
WO/2018/087440A1
The invention relates to a control method implemented by a communication device (2), comprising: acquiring a current location (P1) and current capacities of a drone (4); selecting a destination point (P2) that can be reached by the drone...  
WO/2018/086483A1
An impact damper device comprises at least one rubber and air-based shock absorber set (1) arranged in a support frame comprising a fixed plate (6) and a blocking plate (5) arranged in parallel and aligned with each other, and connected ...  
WO/2018/087057A1
The invention relates to a movable base (2) for transporting equipment by land, in particular aeronautical equipment. The movable base (2) comprises a frame (120) including two side arms (122) designed to move parallel to one another and...  
WO/2018/089588A1
Described is a layaway system for a retail store that includes a layaway processing utility, a detector, and a drone. The layaway processing utility electronically stores information about the layaway account and communicates with custom...  
WO/2018/089236A1
A container for aerial drone transport includes a main body; a lid; a plurality of aerial drone grip elements organized in an aerial drone grip configuration; a plurality of visual aerial drone orientation markers carried by at least one...  
WO/2018/086132A1
A detection device (100) and an unmanned aerial vehicle (200). The detection device (100) comprises a battery (10), a battery mounting base (20), a circuit (70), and a sliding member (30). The battery (10) is provided with at least one g...  
WO/2018/088149A1
The purpose of the present invention is to facilitate the attachment of a second member to a sheet-like first member, while supporting the first member in a state of being capable of being deformed by gravity. This component production m...  
WO/2018/086511A1
A ventilating and lighting apparatus (100) for an individual cabin can improve a contact area between air and a photocatalyst and ensure sufficient light irradiation on the surface of the photocatalyst, and implements rational utilizatio...  
WO/2018/085902A1
The present invention provides an inflation system (12) for use in a buoyancy system (14). The buoyancy system is adapted to be fitted to an aircraft (15) for recovering and retaining the aircraft (15) at the surface of a body of water (...  
WO/2018/088140A1
The purpose of the present invention is to facilitate the riveting of a second member to a first member when superposing and assembling the two members. This component production method is provided with: a step (S2) in which an attaching...  
WO/2018/089072A3
A system and method for flight planning for a first vehicle. The method includes generating, based on an entry indicator, a first flight plan for the first vehicle, wherein the entry indicator indicates entrance of a second vehicle into ...  
WO/2018/087492A1
Disclosed is an aircraft engine installation/removal and transfer device (20) in the form of a carriage (100) comprising, on the one hand, a chassis (110) mounted on castor wheels (111, 112, 113, 114) and, on the other hand, a cradle (15...  
WO/2018/089069A1
A passenger seat, such as an aircraft passenger seat, includes a seat base and an entertainment system. The seat base includes a cushioning member and a cover covering the cushioning member. The entertainment system is positioned between...  
WO/2018/087541A1
A deployable wrapped rib assembly is disclosed, comprising a hub, a plurality of ribs each being connected to the hub at a fixed angle such that each rib is inclined with respect to a perimeter of the hub, each one of the plurality of ri...  
WO/2018/088028A1
Provided are: a vibration control device for exerting an excellent vibration-damping effect on a small, light-weight imaging device mounted in an unmanned aircraft; and an unmanned aircraft provided with the vibration control device. A v...  
WO/2018/087273A1
The invention relates to a spacecraft (100) comprising a main body (110) and an attitude control system, said attitude control system including active attitude control means (150). In addition, the attitude control system also comprises ...  
WO/2018/086227A1
An unmanned aerial vehicle (100), comprising a fuselage (1) and a powered component (7). The fuselage (1) is provided with a battery compartment (22) configured to accommodate a battery (2). The battery compartment (22) is provided with ...  
WO/2018/087213A1
The present invention relates to an aircraft (100) comprising: a fuselage (101) comprising a plurality of panels (105) adapted to define an aerodynamic shape for a cockpit or a cargo hold of the aircraft (100);at least one wing (103) str...  
WO/2018/089859A1
The present invention relates to systems and methods for powering and controlling flight of an unmanned aerial vehicle. The unmanned aerial vehicles can be used in a networked cellular communication system. A tether management system can...  
WO/2018/086496A1
A telescopic propeller arm assembly (12) and an unmanned aerial vehicle (10). One end of the telescopic propeller arm assembly (12) is connected to a body (11) of the unmanned aerial vehicle (10), and the other end is connected to a powe...  
WO/2018/086663A1
A folding propeller (1) with an adjustable rake angle has a hub (10) and at least three propeller blades (11) which are pivotally mounted in the hub (10) about pivot axes (25a) extending radially outwards from a central area in the hub (...  
WO/2018/088915A1
The purpose of the present invention is to cool the brakes of the landing gear of an aircraft. For this purpose, the air of the air-conditioning system of the aeroplane is used. Pre-conditioned air from the outside can be supplied to the...  
WO/2018/087582A1
Described herein is a portable external battery module. The module is characterized in that it comprises an aerial device (4) provided with camera (6), which is removably housed within a cavity (C) made in the casing (2) of the module, a...  
WO/2018/089056A1
There is provided a seat base frame (10) comprising one or more base frame tubes (16) having noncircular cross-sections. In a specific example, the tubes (16) have elliptical cross-sections. Further embodiments provide base frame tubes (...  
WO/2018/086204A1
A propeller, comprising: a propeller hub (10), and propeller blades (20). The propeller blades (20) are connected to the propeller hub (10). At a distance of 47.37% of the radius of the propeller from the center of the propeller hub (10)...  
WO/2018/088873A1
The present invention relates to a positioning control device and a method therefor. The positioning control device of the present invention can be applied to various objects, for example, unmanned air vehicles, buildings, and virtual re...  
WO/2018/086225A1
A power device, comprising a motor (1), a control panel (2) electrically connected to the motor (1), and a propeller (3) provided on the motor (1). A first connection structure (14) is provided at one end of the motor (1). The control pa...  
WO/2018/088331A1
The clamp attaching device is provided with: a robot arm base (20) having a rotary table; a robot arm disposed on the rotary table of the robot arm base (20) and having multiple arms (21, 22, 23, 24, 25) and multiple joints; a robot hand...  
WO/2018/089735A1
The Glider Guideway System (also referred to as Terreplane Transportation System) is a ground-based transportation comprised of flying vehicles pulled by a propulsion line. An important design feature of the most preferred system is that...  
WO/2018/089583A1
Systems, devices, and methods for an extruded wing protection and control surface (126) comprising: a channel (206) proximate a leading edge (202) of the control surface, a knuckle (210) disposed about the channel, a leading void (212), ...  
WO/2018/089934A1
Commercial supersonic aircraft and associated systems and methods. A representative commercial supersonic aircraft includes a fuselage configured to carry a crew and between 20 and 60 passengers, a delta wing mounted to the fuselage, and...  
WO/2018/087934A1
Provided is a control system for an aircraft that increases diagnostic precision of an oil pressure system (1). An oil pressure system (1) of this control system is provided with: a drive device (11) for driving a landing member (2); a c...  

Matches 551 - 600 out of 61,001