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WO/2013/066390 |
A flying device is provided, including a disk configured to rotate around its axis, a ring in parallel with the disk, multiple loads coupled to the disk and the ring, multiple first pivots circularly arranged in the peripheral region of ...
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WO/2013/060318 |
An unmanned high altitude aircraft, in particular a stratosphere aircraft, comprising at least one fuselage (10), wings (13, 14), control surfaces (13", 14", 20', 20", 21', 21") and at least one drive device (15, 16, 17) that has at leas...
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WO/2013/057192 |
The subject matter of the invention is a method for surveying a production plant (13) having production facilities (19a, 19b, 19c, 19d). The invention provides for the survey to be performed by means of an aircraft (12), which to this en...
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WO/2013/055265 |
The present invention relates to a system and method for automatic launch and landing UAVs (Unmanned Aerial Vehicles). The system comprises a ground station adapted for automatic UAV launching and landing. The ground station comprises: m...
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WO/2013/048339 |
An unmanned aerial vehicle (UAV) capable of vertical and horizontal flight modes, a method for assembling a UAV, and a kit of parts for assembling a UAV. The UAV comprises a wing structure comprising elongated equal first and second wing...
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WO/2013/040847 |
A through-flow air suspension platform comprises at least two through-flow blower fans (4). The through-flow blower fans (4) are arranged on the same plane. Each through-flow blower fan comprises a cylindrical blower fan shell (2). Two o...
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WO/2013/041786 |
The invention concerns a propulsion device (10) comprising a body (11) arranged to accommodate a passenger (1) and cooperating with a thrust group (12a, 12b, 13a, 13b) supplied with a pressurised fluid from a compression station. The arr...
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WO/2013/041787 |
Personal watercraft capable of delivering a pressurised fluid and an associated system. The invention concerns a personal watercraft (30) or PWC capable of operating as a fluid compression station in addition to its primary transport fun...
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WO/2013/037379 |
The invention relates to aviation technology and can be used for improving the lift-drag ratio of helicopters and aeroplanes, including classically configured large airliners, and amphibious craft, aerodynamic ground-effect craft and hov...
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WO/2013/039853 |
A vertical takeoff and landing aircraft having at least three wings and at least six propulsion units, each of which are located radially from two adjacent propulsion units, by equal or substantially equal angles. The at least six propul...
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WO/2013/037379 |
The invention relates to aviation technology and can be used for improving the lift-drag ratio of helicopters and aeroplanes, including classically configured large airliners, and amphibious craft, aerodynamic ground-effect craft and hov...
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WO/2013/032078 |
The present invention relates to a method and system for unmanned airborne collection and transmission of information during flight, and to technology for performing an unmanned flight using an air-collecting body, descending from a pred...
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WO/2013/012456 |
An aircraft (100) for use in fixed wing flight mode and rotor flight mode is provided. The aircraft can include a fuselage (102), wings (112,114), and a plurality of engines (132,134). A rotating section comprises a rotating support (502...
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WO/2013/004070 |
A spherical saucer-shaped aviation aircraft, capable of rapid vertical takeoff and flight, differs from the takeoff and flight principle of all aviation aircrafts, comprising vertical power system devices, a transverse power system devic...
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WO/2013/006072 |
The present invention is an improvement to waterborne platforms that are used to anchor aerial and airborne systems deployed over water. The system basically consists of a fully submerged main body (1), which is immersed in a body of wat...
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WO/2013/006072 |
The present invention is an improvement to waterborne platforms that are used to anchor aerial and airborne systems deployed over water. The system basically consists of a fully submerged main body (1), which is immersed in a body of wat...
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WO/2012/175187 |
The present invention relates to a rotary-wing drone (1) comprising a frame in which are located: - a set of sensors (13) designed for performing tasks of surveillance and/or intelligence gathering and/or assisting with the guidance of t...
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WO/2012/175953 |
Apparatus and a method performed by the apparatus, the apparatus being mounted on an unmanned vehicle (2) (e.g. an aircraft) and arranged to act upon a payload (18) (e.g. a weapon), the payload (18) being mounted on the unmanned vehicle ...
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WO/2012/160111 |
Embodiments of the present invention relate to a rocket or ballistic launch rotary wing air vehicle.
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WO/2012/161630 |
The present invention relates to a method for steering a UAV, Unmanned Aerial Vehicle, to enable a high level command of the UAV. The method comprising the steps of: determining (500) a reference position (200, 300, 400) related to a pos...
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WO/2012/160111 |
Embodiments of the present invention relate to a rocket or ballistic launch rotary wing air vehicle.
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WO/2012/159056 |
Generally, an inventive aircraft (1) having at least a first lift body (2) and a second lift body (3) each controllably configurable to correspondingly generate an amount of lift (4) sufficient to remain aloft at a first elevation (5) an...
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WO/2012/145780 |
A method for inspecting a surface area of a known position for material defects by means of a camera assembly arranged on an unmanned and autonomously navigating aerial vehicle is disclosed, comprising: automatically flying the vehicle t...
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WO/2012/145780 |
A method for inspecting a surface area of a known position for material defects by means of a camera assembly arranged on an unmanned and autonomously navigating aerial vehicle is disclosed, comprising: automatically flying the vehicle t...
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WO/2012/148035 |
The present invention relates to a flying automobile, wherein a flying device is installed in a vehicle driven on a normal road to enable flying as well as driving on a road, and the driving force of a jet engine is increased to enable d...
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WO/2012/143717 |
Embodiments of the present invention relate to a man-portable UAV.
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WO/2012/140188 |
The invention relates to a geodetic marking system (1) for marking a known target point (5), having an automotive, unmanned, remotely controllable air vehicle (10) and having a geodetic position determination arrangement (20) for determi...
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WO/2012/140191 |
The invention relates to a geodetic measuring system (1) having a geodetic measuring unit (30), in particular a total station, a theodolite, a laser tracker or a laser scanner, having a beam source for emitting a substantially collimated...
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WO/2012/140190 |
A measuring system (10) according to the invention for determining 3D coordinates, in particular a multiplicity of 3D coordinates, of measurement points on an object surface, in particular on an industrial product, in an outer object coo...
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WO/2012/130790 |
The embodiments herein disclose a personal UAV kit for storing, preparing and remote control of micro UAVs. The UAV kit includes a base unit, a control unit and at least one UAV. The UAVs can typically be a winged aircraft with foldable ...
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WO/2012/130790 |
The embodiments herein disclose a personal UAV kit for storing, preparing and remote control of micro UAVs (40). The UAV kit includes a base unit (10), a control unit (30) and at least one UAV. The UAVs can typically be a winged aircraft...
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WO/2012/130856 |
The invention relates to a microscale radio-controlled aerial vehicle, having a fixed wing (as opposed to a rotary wing) comprising propulsion means (23, 24), said vehicle comprising a means for traveling on the ground, which are attache...
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WO/2012/127108 |
Flying device, in which there is a fuselage (2, 2'), wings (8, 9), which are connected to each other to form an essentially looped structure, means (4, 5) for creating a flying force, and the desired means (e.g., 7, 7') for controlling t...
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WO/2012/125052 |
The invention pertains to aeronautical engineering and consists of an airborne platform that can be built to large sizes without requiring a rigid structure of comparable dimensions and which uses both buoyancy and the aerodynamic Magnus...
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WO/2012/125052 |
The invention pertains to aeronautical engineering and consists of an airborne platform that can be built to large sizes without requiring a rigid structure of comparable dimensions and which uses both buoyancy and the aerodynamic Magnus...
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WO/2012/125600 |
In an aspect, the invention features a method for mission planning. The method includes displaying a graphical representation of a geographical area and displaying a graphical representation of one or more regions within the geographical...
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WO/2012/117197 |
The invention relates to an aircraft comprising: a sealed volume forming an air cushion above which a cabin is arranged, said sealed volume extending substantially across the entire width of the aircraft and comprising: - at least one in...
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WO/2012/117197 |
Aircraft, characterized in that it comprises: ■ a sealed volume forming an air cushion above which a cabin is arranged, said sealed volume extending substantially across the entire width of the aircraft and comprising: - at least one i...
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WO/2012/118731 |
Lighter-than-air systems, methods, and kits for obtaining aerial images are described. For example, various methods for determining planned ascent, drift, and/ or descent of a lighter-than-air system are described. In addition, various s...
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WO/2012/113158 |
A helicopter includes a fuselage (1) and propellers (3). The propellers (3) are provided under the fuselage (1). The helicopter solves the problem of prior art that the low carrier capacity is caused by the low lifting capacity and impro...
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WO/2012/113576 |
The invention relates to an ultra-lightweight airplane (100) for transporting loads, comprising a hull (110), at least three individually controllable rotors (130), and at least one first airfoil (120a) arranged on the hull. Axes of the ...
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WO/2012/107650 |
The invention relates to an airplane (1) comprising a fuselage (2) which is elongated in a longitudinal direction X of the airplane, a wing (3) attached to the fuselage in a central portion of the fuselage, and a rear fuselage (21) which...
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WO/2012/107034 |
The invention relates to a remote-controlled small flying object comprising at least one lift area (17), comprising at least one pair of propeller drives (12, 13), and comprising a weight element (20), the position of which can be varied...
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WO/2012/101645 |
Method for dynamically limiting the inclinations of monoblock flight control surfaces (FCS) in an aircraft. Dynamic limitation of the FCS is activated if a stall susceptibility condition is detected in the current aircraft environment. T...
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WO/2012/101645 |
Method for dynamically limiting the inclinations of monoblock flight control surfaces (FCS) in an aircraft. Dynamic limitation of the FCS is activated if a stall susceptibility condition is detected in the current aircraft environment. T...
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WO/2012/091533 |
The options of the invention relate to the aviation and can be used in order to create lifting vehicle as well as load lifting devices. In order to achieve technical result - the decrease of energy losses on the while creating and change...
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WO/2012/084635 |
Apparatus and a method performed by the apparatus, the apparatus being wholly or partially mounted on an unmanned vehicle (e.g. an unmanned air vehicle) and arranged to act upon a payload (e.g. a lethal effector), the payload being mount...
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WO/2012/078122 |
The invention relates to transport means in fluids. The method for producing traction consists in that a circulating fluid is sucked into the region below a dome-shaped body of a device for producing traction through an upper opening wit...
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WO/2012/055062 |
The invention relates to a vertical take-off aircraft. Said vehicle has a cylindrical central body having four rectangular wings in a radial arrangement about said central body and arranged in vertical planes when inactive, capable of ro...
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WO/2012/053276 |
[Problem] To horizontally stabilize the airframe of a disc air vehicle by generating centrifugal force like a spinning top with an unreal vertical axis passing through the gravity of the disc air vehicle as the center on the horizontal s...
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