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Patent Searching and Data


Matches 701 - 750 out of 61,901

Document Document Title
WO/2018/122769A9
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/2018/125309A3
Described herein are methods and systems for motorized control of a tether, such as for purposes of user interaction and feedback. In particular, a UAV's control system may determine one or more operational parameters of a motor for a wi...  
WO/2018/124867A1
The present invention relates to a smart microcellular antenna in the form of an array based on miniature microstrip technology and covering the GSM, 3G and 4G frequency bands. The underlying model is modelled and simulated using a finit...  
WO/2018/125309A2
Described herein are methods and systems for motorized control of a tether, such as for purposes of user interaction and feedback. In particular, a UAV's control system may determine one or more operational parameters of a motor for a wi...  
WO/2018/121191A1
Provided is a seating system, comprising: a first type of seats (2) and a second type of seats (1). Every two rows of the first type of seats (2) are spaced apart by at least one row of the second type of seats (1). The first type of sea...  
WO/2018/120744A1
Disclosed are an envelope material, an envelope, an aerostat, and a method for preparing the envelope material. The envelope material comprises a bearing layer and TPU coatings. The bearing layer is combined with the TPU coatings by mean...  
WO/2018/125483A1
In some embodiments, the disclosed subject matter involves a system and method for dynamic object identification and environmental changes for use with autonomous vehicles. For efficient detection of changes for autonomous, or partially ...  
WO/2018/122243A1
The invention relates to a driving device comprising: a frame (19), a screw-nut system comprising a threaded stem (18) and a first nut (20) helically linked with the threaded stem (18), the threaded stem (18) being connected to the frame...  
WO/2018/122370A1
There is disclosed a rotor (3, 3', 3'') for an aircraft (1) capable of hovering, comprising: a stationary support structure (10); a rotative element (11), which is rotatable about a first axis (A) with respect to said stationary support ...  
WO/2018/122843A1
An aircraft pylon is provided, configured for mounting to the underside of an aircraft wing projecting from a fuselage and for carrying an external payload suspended therefrom. The pylon comprises an attachment mechanism configured for f...  
WO/2018/121804A1
An electric drive system of a gyroplane (28) comprising a support rotor (11), a primary engine (7) connected with a pusher propeller (8) for movement in air, and an electric motor (1) for movement on road, wherein the primary engine (7) ...  
WO/2018/119803A1
Provided is a gimbal load installation assembly (12) used for being slideably installed on a gimbal support (20), so as to adjust the centre of gravity of a load installed on the gimbal load installation assembly (12). The gimbal load in...  
WO/2018/123187A1
A multicopter 10 including: four single rotors 40b, 42b, 46b, 48b; and two pairs of coaxial contra-rotating rotors 44c, 44d and 50c, 50d. In the planar view, these eight rotors are provided at the vertices of a hexagon and are arranged s...  
WO/2018/124549A1
Disclosed are a simulation device for virtual experience of air leisure-sports and a control method thereof. A control method according to the present invention comprises the steps of: sensing a user's motion state by using a pre-configu...  
WO/2018/124942A1
A multifunctional helicopter avionics suite comprises a flight computer panel (1) with a satellite receiver, an autopilot system (2), an electronic display system (3), a navigation system (4) comprising a roll and pitch determining devic...  
WO/2018/123186A1
A multicopter 10 comprising: eight rotors arranged having gaps therebetween and so as to surround a center point P1 in the planar view; and a spraying device 52 having a plurality of nozzles 62, 64. In the planar view, the eight rotors a...  
WO/2018/125333A2
A software-defined receiver (SDR) using real long term evolution (LTE) signals may be used for navigation. The LTE SDR leverages the structure of the downlink LTE signal, and provides signal acquisition, navigation-relevant high-level sy...  
WO/2018/119768A1
A connection device, a cradle head assembly provided with the connection device and a capture assembly, comprising: a capture device (300) and a cradle head (20) which is used for carrying the capture assembly; the cradle head assembly c...  
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/2018/122842A3
A universal aerial platform (11, 41) supports lift elements (13, 14), thrusters (15), landing gear (21, 22) and a fuel supply (16) and has a coupling mechanism (17) external to the aerial platform for coupling to a terrain vehicle (20) s...  
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/2018/124943A3
The invention relates to the field of commerce, in particular to delivery. More specifically, the invention relates to methods of delivery using unmanned aircraft and to preparation for such delivery. The present method comprises: affixi...  
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/2018/122842A4
A universal aerial platform (11, 41) supports lift elements (13, 14), thrusters (15), landing gear (21, 22) and a fuel supply (16) and has a coupling mechanism (17) external to the aerial platform for coupling to a terrain vehicle (20) s...  
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...  

Matches 701 - 750 out of 61,901