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WO/2019/034432A1 |
Disclosed is an actuation unit (15) for actuating a foldable wing tip portion (9) of a wing (3) for an aircraft (1). The object, to provide a highly compact and strong actuation unit, is achieved in that the actuation unit (15) comprises...
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WO/2019/025807A1 |
A method of manufacturing a part, the method involving providing an apparatus, the apparatus having a metal skin component; a metal HIP can and a hollow space between a portion of the HIP can and a portion of the skin component, the meth...
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WO/2019/021521A1 |
Provided is a hovering vehicle capable of safely moving while hovering off the ground. This hovering vehicle 1 comprises: six or more impellers 37 arranged below an operator's cab 10 for blasting air drawn in through an air intake space ...
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WO/2019/015366A1 |
An unmanned aerial vehicle (100), comprising a vehicle body (20) and vehicle arms (11) connected to the vehicle body. The vehicle arms are hinged on the vehicle body by means of spherical hinge parts (112), and are capable of being folde...
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WO/2019/013012A1 |
A fuel tank dam (10) comprises a first section (11), a second section (12), a third section (13), and a flange section (14). The first section (11) can be fixed to a first structural component, and the second section (12) can be fixed to...
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WO/2019/012297A1 |
Embodiments relate to reconfigurable unmanned vehicles (100). Such vehicles (100) comprise a fuselage (102) presenting a bay (118) for receiving a plurality of components (120-128), each of the plurality of components (120-128) relating ...
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WO/2019/005137A1 |
A monitoring system (5, 205) for an aircraft (10) has sensors (20, 30) that are used to sense the air movement around the aircraft. The monitoring system may use information from the sensors to estimate the effects of the air movement on...
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WO/2019/005131A1 |
The present disclosure pertains to self-piloted, electric vertical takeoff and landing (VTOL) aircraft that are safe, low-noise, and cost-effective to operate for cargo-carrying and passenger-carrying applications over relatively long ra...
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WO/2018/234199A1 |
A metallic structure with a reinforced skin according to the invention (1), comprises at least one skin (10) and local reinforcement (3a) connected to the skin (10). Each local reinforcement (3) has a transition zone (31a) extended by a ...
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WO/2018/234798A1 |
An aircraft (1) has at least one main wing (2) and at least one boom fuselage (3). The main wing has an aerofoil section having a leading edge (20), a trailing edge (21), a chord length extending between the leading edge and the trailing...
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WO/2018/224327A1 |
A control system for a moveable control surface on a wing or stabilizer of an aircraft, for example a flying car, comprising: a wing or stabilizer having a moveable control surface; a mounting structure for mounting the wing or stabilize...
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WO/2018/224033A1 |
An aircraft with imitation beetle elytron wings, belonging to the technical field of aviation. Imitation beetle elytron wings (2) are used as horizontal wings of an aircraft. The left and right imitation beetle elytron wings (2) are conn...
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WO/2018/218370A1 |
Disclosed is an aircraft and a method of controlling an aircraft. The aircraft comprises a continuous wing assembly extending from port to starboard sides of the aircraft. The aircraft is controlled partially by flexing portions of the w...
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WO/2018/212831A1 |
A lift fan includes a stator which is configured to output a magnetic field. The lift fan also includes a first housing which in turn includes a blade, a second housing, and a magnet array. The magnet array is coupled to either the first...
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WO/2018/203189A1 |
Assemblies and methods for facilitating the assembly of aircraft wings to a fuselage are disclosed. In some embodiments, a wing unit includes features that are configured to define one of more parts of a pressure vessel that is partially...
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WO/2018/203191A1 |
Assemblies and methods for facilitating the assembly of aircraft wings to a fuselage are disclosed. In some embodiments, a wing unit includes features that are configured to define one of more parts of a pressure vessel that is partially...
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WO/2018/203036A1 |
An unmanned aerial vehicle (2) comprising: a fixed wing (6); a pair of nacelles (10) connected to the wing (6) and spaced laterally either side of a centreline of the wing (6), wherein each nacelle (10) comprises a stationary portion (14...
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WO/2018/196810A1 |
Disclosed is an aircraft, comprising a fuselage (1) and a wing (2), a first open channel (12) for extending the fluid flow path being provided at a front portion (211) and/or a middle portion (212) of a windward side (21) of the wing (2)...
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WO/2018/197772A1 |
The aircraft (10) comprises a fuselage (11) and a rhombohedral wing structure (12) comprising front wings (13, 14) mounted on a front wing-root support (17) and rear wings (15, 16) mounted on a rear wing-root support (18). At least two w...
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WO/2018/200093A1 |
Airframes configured for stable in-flight transition between forward flight and vertical takeoff and landing are described herein. In one embodiment, an aircraft can include a fuselage, opposed wings extending from opposed sides of the f...
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WO/2018/192787A1 |
In order to bring the primary structure of an aircraft engine attachment pylon as close as possible to a wing box, the invention provides: - an aircraft wing (2) comprising a wing box (14) made partly by means of a front spar (16) and an...
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WO/2018/189299A1 |
An uplock (101) for use with an aircraft component. The uplock comprises a hook (102) configured to engage a capture pin (126) mounted on the aircraft component. The hook (102) is mounted for movement between a closed position and an ope...
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WO/2018/190921A1 |
In one embodiment, an aircraft includes one or more first wings configured to produce lift in a first direction when the aircraft is moving in a second direction that is substantially perpendicular to the first direction. The first wings...
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WO/2018/189231A1 |
A seating system for a vehicle, comprises first and second seat portions, each providing upper load-bearing surfaces; the first seat portion including a mounting structure for connection to a vehicle body; and the second seat portion inc...
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WO/2018/190922A1 |
In one embodiment, an aircraft includes a number of propellers N prop , wherein each propeller comprises a diameter d prov , has a propeller efficiency η ρτορ , and is configured to absorb power p prop to rotate at a rate RPM to gen...
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WO/2018/185377A1 |
A composite element and a method of manufacturing the same. The composite element comprises a first skin plate (17) and second skin plate (23), which are manufactured as separate pieces and are assembled in a separate phase. At least the...
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WO/2018/186907A1 |
A control system of a flight vehicle automatically varies the relationship between the center of gravity and the center of pressure of the flight vehicle. The control system automatically adjusts a center of pressure of the flight vehicl...
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WO/2018/171089A1 |
Disclosed is an aircraft (100) with a super high aspect ratio based on self-unfolding folding wing technology, the aircraft comprising: an aircraft body (10); a fixed wing (20); and a movable wing assembly comprising a first movable wing...
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WO/2018/169403A1 |
An airfoil-shaped body having a variable outer shape, comprising: a first skin, defining a suction surface, a second skin, defining a pressure surface and connected to the first skin at least at a leading edge and/or a trailing edge of t...
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WO/2018/165313A1 |
An aerodynamic device for enhancing lift and reducing drag of an airfoil, comprising a central portion oriented in a substantially chordwise direction on the airfoil, and a first outer portion and a second outer portion arranged substant...
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WO/2018/163159A1 |
A multirotor aircraft that includes a chassis, vertical rotors, foldable wings, and a means for deploying and folding the foldable wing. The foldable wing is attached to the chassis and the means for deploying and folding the foldable wi...
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WO/2018/156335A2 |
Disclosed herein is a distributed pressure sensor system that quickly detects and counters changes in lift, onset of stall, and flutter. The distributed pressure sensor system may employ a plurality of integrated pressure ports distribut...
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WO/2018/156165A1 |
An apparatus configured to reduce acoustic interactions between a propeller and a surface of an aircraft positioned downstream of the propeller includes a surface modification element of the surface of the aircraft. The surface modificat...
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WO/2018/152792A1 |
Disclosed are a foldable frame (100), a frame assembly (200) and an unmanned aerial vehicle (300). The foldable frame (100) is applied to the unmanned aerial vehicle (300) and comprises a central frame (2) and at least one folding struct...
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WO/2018/153734A1 |
An aircraft including a body and a pair of wings connected to the body by a mounting structure, the wings being movable between a first position in which the wings extend laterally from the body, and a second position in which the wings ...
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WO/2018/147810A1 |
According to various embodiments, there is provided an aircraft including: a fuselage defining a body frame with longitudinal, lateral and height axes extending perpendicular to each other and intersecting in a center of gravity of the a...
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WO/2018/143802A1 |
A blade made of layered material, such as composite material, configured for exposure to a fluid flow, comprises skins (1, 2) defined between a leading edge (3) and a trailing edge (4) which skins in cross-section form a flow profile. Th...
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WO/2018/138477A1 |
A passively controlled fluid foil has a span; and a rigid spar extending in the spanwise direction,a cellular material and a flexible outer surface defining a profile of the outer surface of the foil and encapsulating the cellular materi...
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WO/2018/135739A1 |
A shape memory morphing member using a kirigami pattern is disclosed. The shape memory morphing member using a kirigami pattern comprises: an upper SMP skin layer; a lower SMP skin layer disposed below the upper SMP skin layer; and a cor...
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WO/2018/135962A1 |
Proposed are original airfoils with a sharp leading edge which significantly enhance the aerodynamic qualities of a wing and of aircraft propellers for aviation. The advantage of the present airfoils is based on a method preventing influ...
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WO/2018/129768A1 |
A fused wing and body aircraft, comprising a body (1) and wings, which are fused together. The wings comprise wings (2) that are located on a left side and right side of the body (1); the body (1) has a central symmetry surface; the body...
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WO/2018/131821A1 |
The present invention provides an automatic angle-of-attack control wing that always maintains a reference angle of attack with optimum efficiency by automatically controlling the angle of attack of a wing according to changes in the dir...
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WO/2018/120155A1 |
Disclosed are an aerial vehicle (300), and a flying unit (100) and a lifting structure (10) thereof. The lifting structure (10) comprises a lifting main body (1), the lifting main body (1) being provided with an air channel (12), the air...
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WO/2018/113480A1 |
Provided in the present utility model are a detachable arm assembly and an aircraft. The detachable arm assembly comprises a first arm section and a second arm section. A first line core is fixedly provided inside the first arm section. ...
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WO/2011/087475A9 |
A method of providing an aircraft having a fuselage and a wing configured for extensive laminar flow at design cruise conditions, the method characterized by a) providing wing biconvex-type airfoils having values of thickness, chord and ...
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WO/2018/104251A1 |
An aircraft wing assembly (5) is presented comprising a main wing portion (21), a high-lift device (9) comprising a flow surface with an upper skin portion (25) and a lower skin portion (27), wherein the high-lift device is movable betwe...
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WO/2018/096070A1 |
Described and claimed is an arrangement of a structural element for an aerospace vehicle and a battery set. The structural element extends along a longitudinal direction and has a main web, a first flange and a second flange. The flanges...
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WO/2018/091475A1 |
The invention relates to an electrohydraulic module (1) for driving at least one component of an aircraft, in particular an airplane, wherein the electrohydraulic module (1) comprises at least one electric motor (2) and at least one comp...
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WO/2018/087213A1 |
The present invention relates to an aircraft (100) comprising: a fuselage (101) comprising a plurality of panels (105) adapted to define an aerodynamic shape for a cockpit or a cargo hold of the aircraft (100);at least one wing (103) str...
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WO/2018/089583A1 |
Systems, devices, and methods for an extruded wing protection and control surface (126) comprising: a channel (206) proximate a leading edge (202) of the control surface, a knuckle (210) disposed about the channel, a leading void (212), ...
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