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Patent Searching and Data


Matches 401 - 450 out of 60,004

Document Document Title
WO/2018/056484A1
The present invention provides a multipurpose air vehicle comprising: a frame (1) to which a propeller (11) and an engine-mounted machine part (10) are installed; and a cabin (2) coupled to the frame (1), wherein: the frame (1) includes ...  
WO/2018/053959A1
A drive structure having self-locking highly-integrated aeroplane connecting port and a passenger boarding bridge using said drive structure, comprising a bracket, a revolving drive apparatus having a self-locking function, and a plurali...  
WO/2018/054176A1
A power assembly and an aircraft having said power assembly. The power assembly comprises a propeller (100) and a drive mechanism, the drive mechanism being provided with a rotating shaft (210) driving rotation of the propeller (100), an...  
WO/2018/053925A1
Provided is a tripod-head shock-absorbing device, comprising a shock-absorbing panel (10) used for connecting to a tripod head (200), and a main-body frame (20) connected to the shock-absorbing panel (10); the shock-absorbing panel (10) ...  
WO/2018/053813A1
A powered device and an aerial wing outfit with a powered device. The invention comprises a control adjuster (8), and a highly oxygenated water storage chamber (1), catalytic reduction chamber (9), and jet propulsion compartment (3) conn...  
WO/2018/057229A1
An air injection assembly for an aircraft is provided. The aircraft includes a fuselage extending between a forward end and an aft end along a longitudinal direction and a boundary layer ingestion fan mounted to the fuselage at the aft e...  
WO/2018/053784A1
A vibration damper plate (3) used for being connected to a cradle head (30). The vibration damper plate (3) comprises a plate main body (31) and a sensor assembly (32). The sensor assembly (32) comprises a support member (322) fixed to t...  
WO/2018/055612A1
A propulsion system attached to a space vehicle for propelling the space vehicle in an essentially gravity free environment, comprises: a) a first section of tubing; b) a second section of tubing having a cross-sectional area significant...  
WO/2018/054483A1
The invention relates to an aircraft turbine having counter-rotating propellers and a primary drive, the noise development of which is significantly reduced with respect to aircraft turbines which have a primary drive based on the intern...  
WO/2018/055861A1
The present invention addresses the problem of providing technology that enables optical communication between a mobile object and a control device even when the mobile object moves freely in space. These mobile object control device and...  
WO/2018/053712A1
An unmanned aerial vehicle (UAV) (200, 300, 400, 700, 800, 1000, 1200, 1500) can include a central body(202, 302, 402, 702, 802, 1002, 1202, 1502), a plurality of rotors, and a plurality of arms (204, 306, 406, 706, 806, 1006, 1206, 1506...  
WO/2018/053994A1
Embodiments include devices and methods for adaptive image processing in an unmanned autonomous vehicle (UAV). In various embodiments, an image sensor may capture an image, while a processor of the UAV obtains attitude information from o...  
WO/2018/055827A1
A damage detection system according to an embodiment comprises a physical quantity detection unit, a flight condition changing unit, and a damage detection unit. The physical quantity detection unit detects the physical quantity of a str...  
WO/2018/053873A1
An electronic governor (100, 100a), comprising an upper metal casing member (11); a lower metal casing member (12) engaged with the upper metal casing member (11) to form one casing (1); a control circuit board (5) mounted within the cas...  
WO/2018/056783A1
A patch type controller according to the present invention comprises: a main body having a connection unit formed on the bottom surface or a side surface thereof, enabling connection to a mobile phone, a mobile phone case or a wireless c...  
WO/2018/057821A1
An unmanned aircraft system includes an automated recovery system (500) that can recover aircraft in a reliable, economical manner, using a dual-pole (513) and a capture line mechanism (514).  
WO/2018/054590A1
The invention relates to a method for predicting vibrations of an aircraft, the aircraft comprising an active system for reducing main-rotor and/or tail-rotor vibrations, in particular longitudinally adjustable control rods and/or trim t...  
WO/2018/057489A1
A technique for providing drone assistance is discussed. A computing device is in wireless communication with a mobile electronic device and an aerial drone. The computing device can control the aerial drone to travel to the location of ...  
WO/2018/057117A1
An amenities panel for a passenger seat includes a body and at least one convenience feature. The body includes an aft-facing side and is configured to connect to a backrest of the passenger seat. The amenities panel is configured to be ...  
WO/2018/055164A1
Communication system, used in a system of drones, based on a communication technique of TDMA type in which the time is divided into a plurality of levels of hierarchy of temporal decomposition. The set of the hierarchy levels is adapted ...  
WO/2018/057314A2
In some embodiments, unmanned aerial task systems are provided that comprise: multiple unmanned aerial vehicles (UAV) each comprising: a UAV control circuit; a motor; and a propulsion system coupled with the motor and configured to enabl...  
WO/2018/057629A1
An inventory management system managing a plurality of inventory items stored in a storage area. The inventory management system includes an autonomous vehicle configured to move within the storage area and a computing device communicati...  
WO/2018/057242A1
An aircraft is provided including a fuselage that extends along a longitudinal direction between a forward end and an aft end. A stabilizer assembly and a boundary layer ingestion fan is mounted to the fuselage at the aft end and is conf...  
WO/2018/053387A1
A latch for releasably connecting two elements is operable between engaged and released positions. An elongate handle opens and closes a latch mechanism about a first axis of rotation at the rear end of the handle. The latch handle is he...  
WO/2018/052302A1
Trolley (1), such as an airplane trolley or a railway trolley, comprising a substantially box-shaped main body (10) having a top side (10') provided with a recess (20) which defines a peripheral wall at least partly circumscribing the to...  
WO/2018/052527A3
A configuration for a satellite constellation has a plurality of planes, each plane including a plurality of satellites therein, at least some of the planes situated at a different altitude than other of the planes, in some embodiments, ...  
WO/2018/051004A1
Device for supplying electrical energy in an aircraft comprising a housing (300), this housing (300) comprising at least: - one fuel cell stack (1); - a hydrogen generator (5); - a gas supply circuit linking the hydrogen generator (5) to...  
WO/2018/051572A1
[Problem] To achieve a stable airspeed control that takes remote turbulence into account. [Solution] This aircraft speed information providing system is provided with: an airspeed measurement device that measures the present airspeed of ...  
WO/2018/052506A1
A heavy-lift UAV frame includes a central frame portion having a symmetrical shape and forming a pocket area for receiving an avionics package. Top and bottom plates are secured to the central frame portion and include four corner member...  
WO/2018/053182A1
A fluid bearing includes a housing including an internal plenum disposed in the housing and an inlet in fluid communication with the plenum, wherein the inlet is configured to provide fluid to the plenum from an external source, a cushio...  
WO/2018/051474A1
Provided is an aircraft steering control apparatus capable of improving the travelling stability of an aircraft. An actual steering angle determination unit (13) in the steering control apparatus (1) determines the actual steering angle ...  
WO/2018/051152A1
Trailer-tops and aircraft are overlaid with carbon fiber chops in a felt-like structure, encased by electrodes at a constant distance or according to the density of carbon fiber layup.  
WO/2018/051060A1
The invention relates to a method of fastening panels to a substrate, and a fastener, accordingly there is a method of fastening a panel to a substrate, comprising the steps of i. providing on the substrate a first projection, ii. attach...  
WO/2018/052334A1
The invention relates to the field of logistics, namely to systems for delivering goods to collection points using drones. The system comprises drones, distribution centers (DC) 1, collection points (CP) 2, and a control center (CC) 3 ha...  
WO/2018/052288A1
The transmission device (is constructed and arranged to rotate any one of the cam slot members (102, 302) in opposite direction to a direction of rotation of an adjacent cam slot member (104, 302), and to align the cam slot (110, 112, 31...  
WO/2018/051003A9
A method for supplying electrical power to an electrical load (2) in an aircraft, said method comprising: - supplying of electrical power to the electrical load (2) by a main electrical power generating source (1); - measuring an instant...  
WO/2018/050868A1
The invention relates to a device and to a method for performing open -and closed -control of n actuators An (101 ), n = 1, 2,..., N, where N ≥ 1, which drive aerodynamic control surfaces (102) of an aircraft. The proposed device compr...  
WO/2018/051496A1
This aircraft seat unit is characterized by being provided with: a seat which is configured such that the form can be changed between a seat state and a bed state; a right side panel that is arranged upright at the right side of the seat...  
WO/2018/051497A1
Provided is an aircraft box seat structure that demarcates an internal space having therein a plurality of seat units, the aircraft box seat structure comprising: an upper surface panel that is substantially rectangular and determines th...  
WO/2018/052352A1
A method performed by an unmanned aerial vehicle, UAV (10), or a remote control (30) for the UAV, for executing an operating session for the UAV in controlled airspace, comprises the steps of transmitting a request for permission to oper...  
WO/2018/049466A1
An aircraft seat (10) comprising: a seat base (12) having a base support surface (22); an outer backrest (14) mounted to and extending upwardly from the seat base (12); an inner backrest (16) mounted to the outer backrest (14) and/or the...  
WO/2018/051025A1
In order to provide a temporary connection between two structure elements (12, 14), such as two parts of a space launcher or of another type of spacecraft or aircraft, a connection device (16) with controlled separation comprises a therm...  
WO/2018/050837A1
The invention relates to a device (100; 200) for airlifting an object (300), comprising a support structure, said support structure having an upper end section and a lower end section, the upper end section and the lower end section havi...  
WO/2018/051003A1
A method for supplying electrical power to an electrical load (2) in an aircraft, said method comprising: - supplying of electrical power to the electrical load (2) by a main electrical power generating source (1); - measuring an instant...  
WO/2018/050145A1
The invention relates to a flying or sliding element (10) with an outer skin (12), comprising a front element (14, 190) and at least one sail (24, 50, 50', 199, 212, 214, 216, 236, 238), said front element (14, 190) and/or one or more ad...  
WO/2018/049720A1
Disclosed are an aircraft arm assembly of an aircraft and an aircraft, the aircraft arm assembly (10) of the aircraft comprising an aircraft arm housing (12) and an air guide mechanism (14), wherein the aircraft arm housing (12) is inter...  
WO/2018/050866A1
The invention relates to a device and a method for reducing gust loads acting on an aircraft. The aircraft has at least one aerodynamic control surface (101) which can be moved by at least one actuator (102), and a flight control system ...  
WO/2018/046779A1
The present invention relates to an aircraft able to take off vertically and hover because it is based on the principle of the helicopter but has three or more rotors (14) distributed regularly around a central platform (10). The aircraf...  
WO/2018/047283A1
There are cases when the optical element is not sufficiently vibrated and it is not possible to sufficiently remove dust or the like, due to a change in peripheral environment conditions. Thus, an imaging device equipped with an image se...  
WO/2018/048706A1
In some embodiments, methods and systems of dispensing an insecticide to defend a crop-containing area against crop-damaging pests include an unmanned vehicle having a sensor that detects a crop-damaging pest in the crop-containing area ...  

Matches 401 - 450 out of 60,004