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Matches 1 - 50 out of 56,126

Document Document Title
WO/2017/105657A1
Techniques are disclosed relating lighter-than-air aircraft. Such aircraft may be used for various purposes, such as providing network connectivity to areas that would otherwise lack such connectivity. For example, in some embodiments, a...  
WO/2017/105629A1
Methods, devices, and systems for operating a UAV. Embodiments include a UAV having a pivotal platform (140, 640,740), a tilt assembly, and a processor (160). The pivotal platform (140, 640,740) is configured to selectively tilt relative...  
WO/2017/101032A1
A system for servicing an object and methods for making and using same. A mobile platform can perform one or more tasks for the object while maintaining a distance from the object. The mobile platform can thus avoid colliding with the ob...  
WO/2017/105293A1
The utility model relates to devices for stabilizing the position of a three-dimensional body in space with force compensation of tilting effects, which comprises two flywheels with flywheel actuators, which are connected to the solid bo...  
WO/2017/103173A1
There is provided a satellite for observing a target from space, comprising an image capturing module for capturing an image of a target moving relative to the satellite, an image processing module for processing one or more images captu...  
WO/2017/106697A1
Disclosed herein are system, method, and computer program product embodiments for locating, identifying, and tracking a known criminal, fugitive, missing person, and/or any other person of interest. An embodiment operates by deploying an...  
WO/2017/106013A1
Aerial vehicles may be operated with discrete sets of propellers, which may be selected for a specific purpose or on a specific basis. The discrete sets of propellers may be operated separately or in tandem with one another, and at varyi...  
WO/2017/103481A1
The present invention relates to a method (50) for acquiring images by means of a constellation of satellites (20) in non-geosynchronous terrestrial orbit in which, said satellites (20) comprising respective means of inter-satellite comm...  
WO/2017/106721A1
A multi-level (ML) fulfillment center (100) is designed to accommodate landing and takeoff of unmanned aerial vehicles (UAVs) (108), possibly in an urban setting, such as in a densely populated area. Unlike traditional fulfillment center...  
WO/2017/106617A1
Multiple motors may drive (rotate) a single shaft coupled to a propeller. The motors may be selected such that a first motor is capable of rotating the drive shaft in an event of a failure of a second motor coupled to the drive shaft. A ...  
WO/2017/106324A1
The present disclosure provides various embodiments of a multicopter-assisted launch and retrieval system generally including: (1) a multi-rotor modular multicopter attachable to (and detachable from) a fixed- wing aircraft to facilitate...  
WO/2017/103389A1
The invention relates to a hydraulic control system for a thrust reverser of an aircraft turbofan nacelle, comprising devices for actuating and controlling the reverser, including hydraulic locks and cylinders, the corresponding hydrauli...  
WO/2017/105695A1
Embodiments of techniques, apparatuses, systems and computer-readable media for managing landscape of a property are disclosed. In some embodiments, a configuration module may be configured to receive data that specifies landscape or pre...  
WO/2017/101735A1
An exhaust assembly for an aerostat, and an aerostat provided with said exhaust assembly, the exhaust assembly comprising a valve base (2) having a valve port (1), and a valve cover (3) able to selectively cover the valve port (1), and a...  
WO/2017/103397A1
The present invention relates to a terminal (10) intended to be electrically connected to another identical terminal, the terminal (10) comprising a barrel (11) extending along an axis for the connection to an electrical cable (25), and ...  
WO/2017/103837A1
The invention relates to a drone comprising a fuselage and a plurality of housing structures (3) for a plurality of engine units (4), the mechanical connection between each engine unit (4) and each housing structure (3) for the engine un...  
WO/2017/103867A1
The invention relates to a multirotor drone (1) comprising a fuselage and a plurality of engine units driving a plurality of rotors (4), each rotor comprising two blades (5) mounted in a facing arrangement on either side of a blade tilti...  
WO/2017/103126A1
The invention relates to a technique for subsurface prospection by means of a drilling head system (10) having an integrated acoustic source (101, 102, 103) and an arm (20) which is equipped with electrodynamic detectors (201). The drill...  
WO/2017/103408A2
The invention relates to a device (100) for the measurement and compliance monitoring of an impact (220) on a structure (200). The device comprises: a support frame (10) including a hollow lower surface (13) to be positioned against a su...  
WO/2017/103374A1
The invention relates to a defrosting device comprising an actuator (110) having a stationary portion (112) and a movable portion (114) designed to alternately move away from and move towards the stationary portion (112), and an intermed...  
WO/2017/102102A1
The invention relates to a device assembly for improving the sensing quality of ground-position-display and traffic-guidance or traffic-management systems, in particular at an airport, which device comprises at least the following compon...  
WO/2017/103499A1
The invention relates to a method of controlling the braking of an aircraft equipped with a landing gear bearing braked wheels, the aircraft being propelled by jet engines and equipped with a thrust reversal system, the method involving ...  
WO/2017/106248A1
In some embodiments, systems and methods are provided to capture and distribute imaging content. Some embodiments, provide remote inspection systems, comprising: an unmanned aircraft system (UAS) base station control system that wireless...  
WO/2017/105266A1
The invention relates to an aircraft with vertical takeoff and landing and its operation method. Aircraft with vertical takeoff and landing of aerodyne type according to the invention comprises a circular symmetrical aerodynamic body (1)...  
WO/2017/103297A1
The invention relates to a dispenser (1) for lightweight spacecraft, consisting of a ring structure with multiple payload ports (2), the surface (3) of the ring structure being at least partially spherical.  
WO/2017/102277A1
The present invention relates to an unmanned flying device (1) which is capable of hovering and has a main body (2) on which at least three vertically acting drive units (3) which span a plane (4) are held at a distance from one another,...  
WO/2017/103390A1
The invention relates to a method of manufacturing a composite sandwich panel, the panel comprising a core formed of a plurality of cells which extend vertically between a first skin and a second skin, characterized in that it comprises ...  
WO/2017/102362A1
The invention relates to a method for monitoring an electromechanical actuator system including the steps of estimating the drop in voltage in the power supply of the motor linked to faults in the inverter using a Kalman filter, estimati...  
WO/2017/106546A1
Multiple propeller blades (504, 506) may be joined by tip connectors (508) to form a closed propeller apparatus. The tip connectors may create continuous structure between adjacent tips of a first propeller and a second propeller. Use of...  
WO/2017/103459A1
The present invention relates to a device for controlling and monitoring at least one three-phase AC motor driving at least one component integrated within an aircraft turbojet nacelle, comprising: -an electronic power chain (100) of sai...  
WO/2017/106376A1
Sounds are generated by an aerial vehicle (101) during operation. For example, the motors and propellers (102) of an aerial vehicle (101) generate sounds during operation. Disclosed are systems, methods, and apparatus for actively adjust...  
WO/2017/103768A1
Flying chamber (2) for wind tunnels (1), preferably non- recirculating wind tunnels. The flying chamber (2) comprising a support structure (20) defining an inlet opening (21) and an outlet opening (22), which allow an air flow (F) to flo...  
WO/2017/099058A1
[Problem] To provide a transport system using an unmanned aerial vehicle that overcomes restrictions on distance, time, and the like, thereby expanding a deliverable range for improved convenience. [Solution] A transport system using an ...  
WO/2017/099665A1
A method and system for generating a set of values for respective ones of a set of parameters used in determining rotor blade profiles for a coaxial rotor system. The method includes establishing (302) a ratio of respective desired thrus...  
WO/2017/100055A1
An example computer-implemented method involves determining that an aerostat is located within a first atmospheric layer. A first wind-velocity measure is indicative of wind velocity in the first atmospheric layer. The method also involv...  
WO/2017/097292A1
The invention relates to an automatic deployment mechanism for a parachute assembly that can be fastened to a person, the parachute assembly comprising a main parachute and a spare parachute. The automatic deployment mechanism includes: ...  
WO/2017/097021A1
A wearable unmanned aerial vehicle comprises an aerial vehicle body (1). The aerial vehicle body (1) is a hollow box body. Two sides of the aerial vehicle body (1) are symmetrically provided with four wing arms (2) capable of being inwar...  
WO/2017/098232A1
An unmanned disposable air vehicle (1) comprising a structural part (3) that has an outer structure (17) and an inner structure (15) located inside the outer structure (17), the inner structure (15) being arranged to support the outer st...  
WO/2017/098571A1
The present invention easily and accurately estimates the wind direction and/or wind velocity at a desired position even without using a wind direction/wind velocity sensor. A movement instruction means (32) of a wind estimation system (...  
WO/2017/098374A1
A blended wing body aircraft wherein at least each profile section corresponding to the normalized half-span values from 0 to 0.2 has a thickness ratio having a nominal value within the range set forth in Table 1. Also, a blended wing bo...  
WO/2017/099528A1
Disclosed is a boarding bridge having a transparent display. The boarding bridge includes a first tunnel connected to a terminal gate, a second tunnel connected to be capable of overlapping with the first tunnel, and a control unit. The ...  
WO/2017/098411A1
A wind tunnel, in particular to perform simulations of free fall or parachuting, comprising: a flying chamber (10), for accommodating a person who is intended to float when hit by an air flow; a fan device (14) for producing the air flow...  
WO/2017/100579A1
Methods, systems, and apparatus, including computer programs encoded on a computer storage medium, for sending a flight plan for execution by a drone, where the flight plan is adapted to a flight controller of the drone. Receiving flight...  
WO/2017/098172A1
The invention relates to an unmanned aerial vehicle (1) comprising: – a bearing structure, – a wing structure (5) able to allow the unmanned aerial vehicle to take off and move around, the wing structure being mounted on the bearing ...  
WO/2017/100360A1
A propeller alignment device (102) is described. The propeller alignment device (102) can include a second retainer attached to a propeller (112) and a motor (104). The propeller alignment device (102) can also include a first retainer (...  
WO/2017/098397A1
The present invention relates to an accepting station (1) for articles (P) comprising: a conveyor (2) configured to receive an article (P) in a loading area (2a) and move it to an unloading area (2b) along an advancement direction (A), a...  
WO/2017/097265A1
A sky tree and a sky forest for unmanned aerial vehicles. The sky tree for unmanned aerial vehicles comprises a trunk (11), a flight platform (12), an elevator (13), a parking room (14), a command center (15), and a supply station (16). ...  
WO/2017/097669A1
The invention relates to an autogyro rotor blade for generating lift by autorotation, comprising a root-side inner profile region (9), which has a first profile (21c), a tip-side main profile region (10), which has a second profile (21e)...  
WO/2017/096604A1
A method and system for exchange, transmission, and reception of flight data, a storage device, and an aircraft. The method and system for exchange of flight data are applicable to an aircraft and a server, so as to upload the flight dat...  
WO/2017/096547A1
Systems, methods, and devices are provided herein for controlling one or more movable objects (302) via a graphical user interface. A method for controlling a movable object (302) may be provided. The method may comprise obtaining one or...  

Matches 1 - 50 out of 56,126