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Patent Searching and Data


Matches 601 - 650 out of 60,379

Document Document Title
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 ...  
WO/2018/049257A1
Systems and methods for detecting an unmanned aerial vehicle (UAV). Network access (for example, to the Internet) may be provided by detecting a UAV and fixing one or more beams from one or more ground terminals to the UAV. In one embodi...  
WO/2018/047549A1
A spacecraft (10) is provided configured so that after entering the atmosphere by a nose entry, the spacecraft (10) changes posture so as to achieve a target posture angle in which a vertical landing can be performed, and then lands afte...  
WO/2018/046936A1
A blade or wing element includes a plurality of ribs (20) rotatable and/or slidable with respect to one another whereby to vary the aerodynamic configuration of the blade or wing element by causing a twist thereof. A blade or wing or bla...  
WO/2018/047089A1
A window (7) with an emergency exit function for a helicopter (1) is described that comprises: a frame shaped as a framework (8) that can be coupled to a door (6) of said helicopter provided with an opening (9); and a transparent element...  
WO/2018/048496A1
An unmanned aerial vehicle system is provided including an unmanned aerial vehicle (UAV) having a fuselage, a tether having a first end secured to a winch system positioned in the UAV and a second end secured to a payload coupling appara...  
WO/2018/048741A1
In some embodiments, methods and systems of identifying at least one pest based on crop damage detection in a crop-containing area include an unmanned vehicle including at least one sensor configured to detect at least one type of pest d...  
WO/2018/048574A1
An aircraft includes a fuselage, a forward wing assembly, and aft wing assembly, and a propulsion system. The propulsion system includes a port forward propulsor and a starboard forward propulsor, each of which rotatable between a forwar...  
WO/2018/048363A1
A backrest mechanism (30) providing connection of the backrest (20) with the seat base frame (10) vehicle seats (60) and enabling rotational motion by means of a backrest hinge (21) formed on backrest (20) and a bushing (31) that passes ...  
WO/2018/047282A1
There are cases when an optical element is not sufficiently vibrated and it is not possible to sufficiently remove dust or the like due to a change in the amplitude of the vibration of the optical element. The present invention involves ...  
WO/2018/048774A1
Described herein are methods and systems to dampen oscillations of a payload coupled to a tether of a winch system arranged on an unmanned aerial vehicle (UAV). For example, the UAV's control system may dampen the oscillations by causing...  
WO/2018/046612A1
A rotor (3, 3', 3'') for a hover-capable aircraft (1) is described that comprises: a hub (7) rotatable about a first axis (A) and at least two blades (6) hinged to the hub (7); each blade (6) comprises a main portion (10) hinged to the h...  
WO/2018/048665A1
In some embodiments, methods and systems of pollinating crops in a crop-containing area include at least one unmanned vehicle having a receptacle including pollen, a pollen dispenser configured to dispense the pollen from the receptacle ...  
WO/2018/047817A1
When finding a gimbal angle trajectory that satisfies the boundary conditions set by a posture boundary condition setting unit 2131 of a ground station 21, a gimbal angle trajectory calculation unit 2132 calculates a gimbal angle traject...  
WO/2018/045806A1
The present invention relates to a motor speed adjustment system for a multi-rotor aerial vehicle, and a multi-rotor aerial vehicle. The motor speed adjustment system comprises a flight control unit, and further comprises a motor speed a...  
WO/2018/045413A1
There is provided a system for determining real-time parameters of an aircraft, the system comprising: at least two sensing apparatus, each of the at least two sensing apparatus including a plurality of in-ground sensors; and at least on...  
WO/2018/045635A1
A moving photographing device for an unmanned aerial vehicle, comprising a photographing device mounting base (1) and a moving photographing device body (2). The photographing device mounting base (1) comprises a left mounting base (3), ...  
WO/2018/048858A1
Systems, apparatuses, and methods are provided herein for unmanned flight optimization. A system for unmanned flight comprises a set of motors configured to provide locomotion to an unmanned aerial vehicle, a set of wings coupled to a bo...  
WO/2018/048681A1
Described herein are methods and systems for detecting and correcting errors when jacking up and lowering a payload coupled to a tether of a winch system arranged on an unmanned aerial vehicle (UAV). For example, the winch system may inc...  
WO/2018/046976A1
Axial airplane airscrew-, fan-, and wind turbine blade of low loading characterised by the fact that the aspect ratio of the airscrew-, fan- and wind turbine blades is low; near to the wide blade ends, but in an appropriate distance an a...  
WO/2018/045825A1
A folding device for avoiding clearances in an aircraft, comprising two parallel fixed plates (101), a fixed rod (102) fixed between the two fixed plates (101), a limiting rod (105), a spring (103) and a rotary arm (201). The fixed plate...  
WO/2018/048645A1
An aircraft includes a fuselage and a wing assembly attached to or formed integrally with the fuselage. The aircraft also includes a propulsion system having a port propulsor and a starboard propulsor. The port and starboard propulsors a...  
WO/2018/048495A1
A payload coupling apparatus is provided including a housing, wherein the housing is adapted for attachment to a first end of a tether, a slot extending downwardly from an outer surface of the housing towards a center of the housing ther...  
WO/2018/045757A1
A movable walkway braking system, comprising a braking plate (223), a braking pin (67) and a triggering mechanism. A passenger boarding bridge comprising said movable walkway braking system, having three or more walkways, and an extendin...  
WO/2018/048573A1
An aircraft includes a fuselage and a wing assembly attached to or formed integrally with the fuselage. The aircraft also includes a hybrid electric propulsion system having a port propulsor and a starboard propulsor, with the port and s...  
WO/2018/047281A1
There are cases when it is not possible to sufficiently perform dust removal or the like depending on optical element orientation. Thus, an imaging system equipped with: an image sensor; an optical member positioned to the front of the i...  
WO/2018/047187A1
A modular vehicle system includes at least one body module having at least one body connection interface, and a kit. The kit includes a plurality of utility modules including at least one first utility module (in the form of a fixed-wing...  
WO/2018/048501A9
An arcjet thruster system for a spacecraft is provided. The arcjet thruster system may include a power supply that includes a radio-frequency start power supply and a continuous direct-current power supply, each selectively coupled to el...  
WO/2018/048501A1
An arcjet thruster system for a spacecraft is provided. The arcjet thruster system may include a power supply that includes a radio-frequency start power supply and a continuous direct-current power supply, each selectively coupled to el...  
WO/2018/045661A1
An information protection method for an unmanned aerial vehicle, the unmanned aerial vehicle comprising an ARM controller (1) and an information protection module (4). The method comprises: an ARM controller (1) transmitting, back to a c...  
WO/2018/048627A1
Some embodiments provide an aerial monitoring system to monitor a geographic area, comprising: a unmanned aerial vehicle (UAV) comprising: a plurality of lift motors to drive a propeller; a substructural support supporting the lift motor...  
WO/2018/046806A1
The invention relates to a control device for power kites. It consists of a tall Y-shaped structure (1), the base of which is connected to the center of a horizontal control bar (3) arranged perpendicular to the structure (1). An articul...  
WO/2018/049247A1
In some embodiments, unmanned aerial task systems are provided that include a plurality of unmanned aerial vehicles (UAV) each comprising: a UAV control circuit; a motor; propulsion system; and a universal coupler configured to interchan...  

Matches 601 - 650 out of 60,379