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Patent Searching and Data


Matches 301 - 350 out of 2,619

Document Document Title
WO/2016/132302A3
Exemplary embodiment of the present disclosure is directed towards an aeroplane multipurpose wing stability system. The system includes a wing shell connected to a fuselage of the aeroplane configured with a wing socket for providing fle...  
WO/2016/162374A1
The invention relates to a wing structure (1) for flying objects, comprising a wing leading edge (4) and a wing box (2), wherein the wing leading edge should be arranged on the wing box in particular in a detachable manner. For this purp...  
WO/2016/109004A3
A scissor link is provided and includes a first component defining a first bore and including first outer pads defining first and second holes and a first recession defining a first threaded hole, a second component defining a second bor...  
WO/2016/154500A1
A three stage watercraft for operation in the water as a traditional boat at low speeds in stage one, for operation on the water's surface at mid-range speeds at stage two, and for traveling in ground effect at higher range speeds is dis...  
WO/2016/150561A1
Traction air device with multiple wing contours for a wind power generation plant and wind power generation plant comprising said air device.  
WO/2016/142559A1
The aircraft forms a supporting volume that includes at least part of the central body in which the cargo to be transported is accommodated, preserving said volume, a conventional wing profile in the longitudinal direction of the aircraf...  
WO/2016/141742A1
Disclosed is a fixed-wing unmanned aircraft capable of being quickly disassembled and installed, comprising an aircraft body, and a wing and a tail installed on the aircraft body, wherein the tail comprises a tail wing and a tail rod fix...  
WO/2016/139465A1
An unmanned high altitude aircraft operating above 15 km with transmitting and/or receiving antennas, enclosed or more than half enclosed on a projected area basis normal to the plane of the antenna (s), in a wing structure where the cho...  
WO/2016/138173A1
Methods of manufacturing and operating a solar powered aircraft having segmented wings that can be reconfigured during flight to optimize collection of solar energy are described. The aircraft have rigid construction that is resistant to...  
WO/2016/138139A1
A solar powered aircraft having segmented wings that can be reconfigured during flight to optimize collection of solar energy are described. The aircraft have rigid construction that is resistant to inclement weather and is configured to...  
WO/2016/135554A1
The invention provides an unmanned aerial vehicle (UAV) having modular components. The modular components include a self-governing wing, a free fuselage and a pivot point connector. The connector is optionally a quick connect and release...  
WO/2016/137362A1
The invention relates to two aircraft forming the fuselage of an aeroplane that flies vertically and horizontally, moves forward and backward, and separates to form two self-contained aircraft while in flight mode. When required, the fus...  
WO/2016/134475A1
A structure adapted to traverse a fluid environment exerting an ambient fluid pressure is provided. The structure includes an elongate body extending from a root to a wingtip and encapsulating at least one interior volume containing an i...  
WO/2016/124730A1
The invention relates to producing a panel with cross stiffening (10) having a high resistance to deformation, by implementing production steps without assembly or attachment. To achieve this, according to the invention such a panel (10)...  
WO/2016/122486A1
A telescoping wing comprised of multiple nestling sections, capable of automatically extending and retracting, varying the span of the wing and greatly reducing the space needed for storage of the wing. The telescoping wing utilizes an i...  
WO/2016/116102A1
The invention relates to a device of a safety system and/or resource and energy-efficiency improvement system for influencing the flow around an aero- or hydrodynamic body (3), preferably an aerofoil (3), according to the principle of a ...  
WO/2016/107528A1
A foldable unmanned aerial vehicle for improving the portability of unmanned aerial vehicles comprises an unmanned aerial vehicle body (1) and a rotor portion connected to the unmanned aerial vehicle body (1). The rotor portion comprises...  
WO/2016/107950A1
The present invention refers to a technique for coupling the run-out section of stringers (5) with ribs, frames or other structural elements (2). A structural element of an aircraft composite structure comprises at least one pair of clea...  
WO/2016/095886A1
Known towed bodies can be maneuvered in all three dimensions but, as pure airborne targets, do not have a large load capacity. The towed body (01) according to the invention is designed for bearing large loads and serves exclusively scie...  
WO/2016/092102A1
The disclosure thus relates to a light unmanned vertical takeoff aerial vehicle (1) which comprises at least two fixed coplanar propulsion devices (7) and at least one wing (3) providing the drone (1) with lift. The coplanar propulsion d...  
WO/2016/092293A1
Components having fibre-reinforced composite structures are disclosed. The component comprises a plurality of structural fibres embedded in a cured matrix material and a plurality of nanostructures such as carbon nanotubes extending from...  
WO/2016/078562A1
Disclosed in the present invention is a high-speed aircraft, comprising a shell and an engine, an outer fluid channel and an inner fluid channel being arranged in succession within the shell, the outer fluid channel and the inner fluid c...  
WO/2016/079202A1
The subject matter of the invention is a multilayer sealed skin, in particular for an inflatable structure and that comprises a first polymer film (10a or 10b), a reinforcing fabric (20a or 20b) disposed on the first polymer film and a s...  
WO/2016/079743A1
A pressurized, fluid-filled channel network embedded in an elastic structure, asymmetrically to the neutral plane, is used to create a deformation field within the structure by the pressurization of the embedded fluidic network, which ca...  
WO/2016/057004A1
A central wing panel for a hybrid transportation vehicle for ground and air transportation. The central wing panel has a front frame section and a rear frame section connected by one or more cross members. The central wing panel can also...  
WO/2016/055990A1
Methods are provided for operating an air vehicle, the air vehicle including fixed wings configured to provide mild stall characteristics including a post-stall regime, and a propulsion system capable of generating a controllable thrust,...  
WO/2016/053259A1
An aerodynamic structure incorporated in an aircraft control surface (10) provides a spar (16) extending along at least a portion of the control surface in a direction and the spar includes a plurality of bends along the direction of ext...  
WO/2016/050198A1
An airplane wing assembly comprises a wing (20), a winglet (10) and a connection element. The wing is provided with a wing box. The winglet is located at a wing tip of said wing (20) and is connected with the wing (20) by the wing box. S...  
WO/2016/046787A1
A skin for an aircraft is configured to be disposed on a first rigid member (182). The first rigid member has at least a portion of a structural frame for the aircraft. The skin is configured to be disposed on a second rigid member (184)...  
WO/2016/038097A1
The invention relates to an aircraft having a fuselage and wings connected thereto, wherein a support strut extends in each case between the fuselage and the wings, said support strut being connected both to the fuselage and the wing. Th...  
WO/2016/003530A3
One example embodiment includes a vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV)(12). The VTOL UAV (12) includes a flight control system configured to provide avionic control of the VTOL UAV (12) in a hover mode and in...  
WO/2016/028134A1
The invention relates to airfoils, called jn1431-265 and 1413-362, which operate intelligently by adjusting the variable aerodynamics thereof, not only through the attack and sine angle, but also through the effect of scale (air speed), ...  
WO/2015/179122A3
A vehicle for providing one or more people air and ground transportation includes a body, a wing, and a coupler that attaches the wing to the body. The body is configured to carry one or more people. The wing is moveable from a first pos...  
WO/2016/023056A1
The invention relates to a control surface element (4) for an airplane, in particular a spoiler, comprising a composite fiber element (3) that has a surface (8) around which air flows, a mounting device (5) for movably mounting the compo...  
WO/2016/018477A1
Method and apparatus for controlling a shape of a composite structure. A shape memory structure associated with the composite structure is activated. The shape memory structure changes from a buckled shape to an original shape and causes...  
WO/2016/012763A1
Aircraft frame structure, method of making an aircraft frame structure, method of repairing an aircraft and aircraft component An aircraft frame structure is provided comprising a grid support (typically a geodetic support) (2) and (i) a...  
WO/2015/183347A3
A new flap design for fixed wing aircraft increases stability and performance of the aircraft through a wide range of air speeds and flight dynamics when implemented on the flap of a fixed wing aircraft. The flap comprises a step configu...  
WO/2015/193617A1
The invention relates mainly to a wing for the propulsion of a vehicle, characterised in that it comprises an outer shell (11) and at least one airfoil structure (10) surrounded by said outer shell (11), said airfoil structure (10) havin...  
WO/2015/190124A1
Provided is a morphing wing capable of greatly deforming the wing as a whole through a lightweight and simple mechanism without accompanying increases in structural complexity and size, thereby achieving a high wing area increasing effec...  
WO/2015/094859A3
An example method may include receiving data representing an initial position and an initial attitude of an aircraft. The method further includes determining a change to a first attribute and a second attribute of the position or the att...  
WO/2015/189242A1
The invention relates to a method, and wings (100) for an aircraft obtained by said method, for assembling a casing structure (100) including basic parts (230, 240, 321) that are assembled according to a sub-structure of stiffeners (230,...  
WO/2015/160394A3
An asymmetric aircraft (1) and an aircraft (1) that can operate from small ships (8) and be stored in high density with three aircraft or more in one helicopter hangar (107) without needing a landing gear or wing fold. These aircraft sli...  
WO/2015/156857A3
The present disclosure is generally directed to a composite trailing edge control surface (600) including a contiguous one-piece composite control surface skin (200) wrapped around a plurality of stiffening cores (300), a plurality of hi...  
WO/2015/172869A1
The invention relates to a high-load gearing for a high-lift support (21) of an aircraft, wherein the high-load gearing comprises two outer segments (11) that cannot be rotated in relation to each other and an inner segment (12) that can...  
WO/2015/172892A1
The invention relates to a method for mounting an aircraft structure to a mounting frame, wherein the mounting frame is not part of an aircraft, and wherein in one step, structural parts and/or auxiliary structures of the aircraft struct...  
WO/2015/170090A1
An aircraft fuel tank(16), comprising: a plurality of tank walls enclosing a liquid storage space (14), the plurality of tank walls including a first tank wall (10) (e.g. an external skin of the aircraft) and a second tank (8) wall (e.g....  
WO/2015/162399A1
An aircraft comprises a wing (1) and a wing tip device (6). The wing tip device (6) is moveable between a flight configuration for use during flight and a ground configuration for use during ground-based operations. In the ground configu...  
WO/2015/163855A1
A propeller blade is provided including a leading edge and a trailing edge. The trailing edge is arranged opposite the leading edge to form an airfoil there between. At least one of the leading edge and the trailing edge include at least...  
WO/2015/160394A2
An asymmetric aircraft (1) and an aircraft (1) that can operate from small ships (8) and be stored in high density with three aircraft or more in one helicopter hangar (107) without needing a landing gear or wing fold. These aircraft sli...  
WO/2015/150835A1
A method of manufacturing a foldable aerodynamic structure, such as a wing, for an aircraft. The wing (1) comprising an inner region (1) and an outer region (3) rotatable relative to the inner region between a flight configuration and a ...  

Matches 301 - 350 out of 2,619