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Patent Searching and Data


Matches 51 - 100 out of 60,447

Document Document Title
WO/2018/125942A1
Methods and systems for vertically landing space vehicles are described herein. In one embodiment, a reusable space vehicle lands in a vertical, nose-up orientation by engaging a system of cables suspended from an elevated framework duri...  
WO/2018/122413A1
The invention relates to a container for receiving, storing, and dispensing liquids and/or viscous substances, in particular fuel, propellant, or drinking water, comprising a casing (12) with a microscopic surface structure (16) that is ...  
WO/2018/119736A1
An electronic governor (100), comprising: a shell and a circuit board (130) arranged in the shell. The circuit board (130) comprises an upper surface (130a) and a lower surface (130b) arranged on the back of the upper surface (130a) and ...  
WO/2018/122371A1
There is disclosed a rotor (3, 4, 4', 4'') for an aircraft (1) capable of hovering, comprising: a stator (10, 150); a rotatable element (11, 151), which is rotatable about an axis (A, B) with respect to stator (10, 150); a blade (13; 154...  
WO/2018/120741A1
A barrier material, a polyurethane adhesive containing same, a skin and an aircraft. The barrier material comprises a povidone and an ethylene/vinyl alcohol copolymer coupled with a coupling agent. After coupling the povidone and the eth...  
WO/2018/124353A1
The present invention relates to a tilting rotor and, more specifically, to a rotor enabling bidirectionally formed rotors to be tilted such that propelling power can be generated in the same direction, and being capable of preventing a ...  
WO/2018/120155A1
Disclosed are an aerial vehicle (300), and a flying unit (100) and a lifting structure (10) thereof. The lifting structure (10) comprises a lifting main body (1), the lifting main body (1) being provided with an air channel (12), the air...  
WO/2018/119620A1
A multi-rotor unmanned aerial vehicle (1), comprising: a machine body (10) and a plurality of rotor mechanisms (20) which are provided on the machine body (2), a rotor mechanism (20) comprising a rotor (21); the multi-rotor unmanned aeri...  
WO/2018/120153A1
Disclosed is an aerial vehicle (400), a flying unit (300) and a lifting structure (100) thereof. The lifting structure (100) comprises a motion main body (1), wherein a connection portion (11) used for transmission connection with a moti...  
WO/2018/124688A1
A drone control device for collision avoidance, according to an embodiment, comprises: a driving unit for driving a rotor blade of a drone; a sensor unit including an omnidirectional camera for acquiring an omnidirectional image by photo...  
WO/2018/119555A1
Disclosed is an unmanned aerial vehicle (1), comprising an obstacle avoidance device (2). The obstacle avoidance device (2) is provided with an image sensor (21), and the axial direction (20) of the image sensor (21) can be arranged in a...  
WO/2018/120163A1
Multi-rotor aircrafts and a spreading and/or folding method of the propeller protective cover thereof. The aircraft (10, 20, 30) comprises a fuselage (110, 210,310) and a plurality of propeller protective covers (121, 221, 321) connected...  
WO/2018/122297A1
The invention relates to an electrical drive system for an aircraft. The drive system has electrical components which are operated at relatively high operating voltages. In order to compensate for negative effects of Paschen's law on the...  
WO/2018/119578A1
Transformable apparatus is provided with one or more moveable components (104, 204, 404, 604). The movement of the one or more components relative to another component (102, 202, 402, 602) of the transformable apparatus transforms the tr...  
WO/2018/124662A1
An electronic device is disclosed and includes a display, a wireless communication circuit configured to transmit or receive data, a processor, and a memory electrically connected with the processor. The memory stores instructions, which...  
WO/2018/122830A1
Overall efficiency and/or flight time of UAVs and Drones can be increased by adding elements containing lighter-than-air gasses; and/or by reducing and/or eliminating the power supplied to any combination of the motors to reduce overall ...  
WO/2018/119802A1
Provided is a gimbal frame (20) used for installing a load. The gimbal frame (20) comprises a guide rod (22), and a centre of gravity adjusting and locking mechanism (5) installed on the guide rod (22). The centre of gravity adjusting an...  
WO/2018/120890A1
An unmanned aerial vehicle (100), comprising a body (10) and an undercarriage (20); the undercarriage (20) is entirely received in the body (10) in a folding state; the undercarriage (20) is entirely received in the body (10) when folded...  
WO/2018/120044A1
An unmanned aerial vehicle and a landing gear system thereof. The landing gear system (1) comprises: a drive mechanism (2), a transmission mechanism (31) and a plurality of landing gear mechanisms (3); the drive mechanism (2) comprises a...  
WO/2018/120742A1
A capsule body material, a capsule body, an aerostat, and a preparation method for the capsule body material. The capsule body material comprises a gas barrier layer (20), the gas barrier layer (20) being a coating or a film which are pr...  
WO/2018/120001A1
A power device, comprising a motor (1) and a propeller (2); the motor (1) is used for driving the propeller (2) to rotate; the motor (1) has a hollow cavity (11) that is open at two ends; the hollow cavity (11) extends from the top of th...  
WO/2018/119727A1
A control method for an electronic speed controller. A first communication interface used for single-line communication is provided on the electronic speed controller. The method comprises: acquiring voltage information of the first comm...  
WO/2018/122239A1
The invention relates to a driving device comprising: a screw-nut system (17) comprising a threaded stem (18) and a first nut (20; 21) linked to the threaded stem (18) by means of a helical link; a gear (30) allowing a rotational movemen...  
WO/2018/125622A1
An aerial vehicle is provided including rotor units connected to the aerial vehicle, and a control system configured to operate at least one of the rotor units. The rotor unit includes rotor blades, wherein each rotor blade includes a su...  
WO/2018/125445A1
Systems and methods may use a drone swarm to increase cargo capacity. A drone swarm may include a networked drone system or two or more drones, such as a parent drone and a child drone. A method may include receiving support component ba...  
WO/2018/122769A1
Working with the traditional soda lime float glass, there is a limit on how thin an automotive laminate can be while still meeting all of the functional and safety requirements. By using alternate glass compositions and chemical temperin...  
WO/2018/122536A1
A seat (100) comprising a seat portion (20), a backrest (10), and a headrest (12) attached to a structure of the backrest. The headrest comprises a head cushion (13) attached to the backrest by at least one headrest arm (16); the arm is ...  
WO/2018/116490A1
A first deployment mechanism (30) deploys a first radiator panel (20) from a state in which the first radiator panel (20) faces the south surface or north surface (10) of a satellite body structure. With the first radiator panel (20) fac...  
WO/2018/117264A1
The present invention relates to a double-sided adhesive tape provided with a layered structure having an adhesive layer (I), a base material, and an adhesive layer (II) in that order. The ratio (Y/X) of the thickness (Y) of adhesive lay...  
WO/2018/117199A1
[Problem] To provide an airbag device for an aircraft that has sufficient battery protection performance. [Solution] An airbag device 1 for an aircraft comprising an upper covering material 19 and a lower covering material 20 which serve...  
WO/2018/114544A1
A movable flight surface for an aircraft, comprising: – an envelope (20) mounted so as to pivot on an articulation axis (21) having at least one end projecting from the envelope, – at least one electric motor (51) which is mounted in...  
WO/2018/115712A1
The present invention relates to a system (1) for generating gaseous dihydrogen, comprising at least: a load (3) of a hydrogen storage material configured to release the gaseous dihydrogen by decomposition of said load; a heating member ...  
WO/2018/117851A1
The present document discloses method, system and device for maritime pilotage involving a pilotage control center where a request for pilotage assistance for a vessel is received. After negotiating the request and - if agreed - the foll...  
WO/2018/116984A1
This movement guide device is equipped with a track unit (33) which sandwiches from the inside and outside and holds a longitudinally oriented cylindrical floor rail (20) having a slit (21) formed in the upper section thereof in the leng...  
WO/2018/118042A1
Provided herein are various improvements to satellite or payload deployment systems and equipment. In one example, a satellite deployment apparatus is provided. The satellite deployment apparatus includes opposing retention members confi...  
WO/2018/117776A1
Various embodiments of the present invention provide a drone comprising a communication module for wirelessly communicating with an external drone, and a processor configured to: when the distance from the external drone is greater than ...  
WO/2018/115504A2
The invention relates to a temporary helipad (10, 10'), comprising at least two fiber reinforced plastic boards (1, 1', 1a-1n) which can be laid on the ground, and connectors (3) for the releasable connection of adjacent plastic boards (...  
WO/2018/113481A1
Provided in the present utility model are a detachable arm assembly and an aircraft. The detachable arm assembly comprises a first arm section and a second arm section. A first line core is fixedly provided inside the first arm section. ...  
WO/2018/113202A1
A detachable pan-tilt connection device (300) and an unmanned aerial vehicle (100). The detachable pan-tilt connection device (300) comprises: an alignment assembly, being used for aligning a circuit connection terminal of the unmanned a...  
WO/2018/115724A1
The invention relates to a flying drone which comprises: a fuselage made up of a single central body (5); an aerofoil made up of a front foil (1) and a rear foil (2); the rear foil being offset in height and in length on the fuselage rel...  
WO/2018/112635A1
An apparatus for storing airplanes includes a first airplane parking floor at a first elevation, a second airplane floor at a second elevation, and an elevator. The first airplane parking floor defines a vacant region within a notional c...  
WO/2018/113480A1
Provided in the present utility model are a detachable arm assembly and an aircraft. The detachable arm assembly comprises a first arm section and a second arm section. A first line core is fixedly provided inside the first arm section. ...  
WO/2018/117878A1
The subject of the invention is a device protecting the flight data recorder ejected from an aircraft, whose task is to provide protection against physical damage of the flight data recorder during a plane crash and to assist reliable se...  
WO/2018/113264A1
Disclosed is a centre of gravity adjustment apparatus for an airship. The centre of gravity adjustment apparatus for an airship comprises: a guide rail (30), the guide rail being provided at the bottom part of an airship gondola and exte...  
WO/2018/117872A1
The Intelligent Autopilot System is an Automatic Flight Control System based on Artificial Intelligence which is capable of performing piloting tasks, and handling flight uncertainties such as severe weather conditions and emergency situ...  
WO/2018/112798A1
A multi-rotor unmanned aerial vehicle (10) comprises a housing (12) and a plurality of propeller arms (20) movably mounted at the housing (12) such that each arm (20) is movable between a deployed position where the arm (20) extends outw...  
WO/2018/114545A1
Electromechanical device for actuating a movable flight surface (11, 12) having an envelope (20) articulated to an aircraft structure about an axis of rotation (21), comprising: – at least two electric motors (51) for rotating the enve...  
WO/2018/112847A1
A control device (10) for controlling a unmanned aerial vehicle (2), comprising: a brainwave collection device (100) for collecting a brainwave signal of a user; a processor (102), which is in communication connection with the brainwave ...  
WO/2018/115540A1
The invention relates to a connection/separation device (1) for separating satellites from shuttles or satellite dispensers, which comprises: a plurality of clamps (2, 2') aligned circumferentially and couplable by the internal face ther...  
WO/2018/112907A1
Disclosed is a gimbal structure, comprising a gimbal support (1) and a reflective mirror (5) arranged on the gimbal support (1), wherein the gimbal support (1) is used for fixing a photographing device (6) and enables the photographing d...  

Matches 51 - 100 out of 60,447