| Document |
Document Title |
|
WO/2022/093987A1 |
Disclosed is an electric aircraft, which includes a fuselage and at least one wing coupled to the fuselage. The electric aircraft includes a plurality of tilting fans coupled to the at least one wing, the plurality of tilting fans being ...
|
|
WO/2022/090951A1 |
The method for manufacturing a panel (10) for aircraft comprises the steps of: arranging, on a curing surface (22), a skin (12) of pre-preg composite material; arranging a plurality of pre-formed, uncured composite stringers (14), each h...
|
|
WO/2022/084645A1 |
A flow control device (60) on a structure such that strain in the structure is at least partially transferred to the flow control device. The flow control device has at least two states, or shapes, separated by an elastic instability reg...
|
|
WO/2022/082383A1 |
A self-locking structure (100), an arm assembly (300) and a movable platform (1000), the self-locking structure (100) comprising a mounting member (10), a movable member (20) and a self-locking assembly (30). The movable member (20) is r...
|
|
WO/2022/082962A1 |
An aircraft propulsion system. The system comprises: a control apparatus, rotary power sets and fixed power sets, wherein the control apparatus is used for sending a target working mode to the rotary power sets and the fixed power sets a...
|
|
WO/2022/087607A1 |
An aircraft with a variety of control surfaces including but not limited to multiple winglet rudders. Each winglet can have multiple independently controlled rudders to improve the flight stability and maneuverability of the aircraft. Ad...
|
|
WO/2022/079415A1 |
A method of manufacturing an aircraft aerofoil such as a winglet. The aircraft aerofoil comprises: a first cover, a second cover, an aerofoil leading edge, and an aerofoil trailing edge where the first and second cover are joined at a tr...
|
|
WO/2022/079435A1 |
An aircraft (101) comprising: one or more main engines (104a, 104b); a first fuel in a first fuel tank (111a) configured to be fed towards at least one of the one or more main engines through a first fuel line; and a second fuel differen...
|
|
WO/2022/069101A1 |
A cover panel for an aircraft, comprising: a first region, a second region for forming an overlap with a second panel, and a ramp, wherein at least a portion of the ramp is between the first and second regions, wherein the ramp includes ...
|
|
WO/2022/067401A1 |
The present application relates essentially to a fixed-wing aircraft made up of a fuselage (02) in the shape of an aerofoil with four wings (10) having the same aerofoil shape with aerodynamic wing behaviour contributing to the lift and ...
|
|
WO/2022/068022A1 |
A tailsitter-type vertical take-off and landing unmanned aerial vehicle and a control method therefor. The unmanned aerial vehicle is mainly composed of a fuselage (1), wings (2), ailerons (3), an empennage (4), an engine (6), attitude a...
|
|
WO/2022/066001A1 |
An aircraft wing (1) provided with a trailing edge region (2) which is provided with a noise attenuation structure, which at least comprises in combination, looking in an upwards direction: a first micro perforated plate (2.1) with micro...
|
|
WO/2022/057115A1 |
An airplane wing fuel tank access cover and a structure of a peripheral area of the access cover, relating to the technical field of aviation. The airplane wing fuel tank access cover comprises an inner access cover (7), an outer access ...
|
|
WO/2022/056597A1 |
An aircraft structure (10) comprising a fuselage (24), first and second forward wings (20, 22) mounted to and/or extending from opposing sides of the fuselage (24), a continuous rear wing span (34) defining first and second rear wings (3...
|
|
WO/2022/053984A1 |
An aircraft frame includes a fuselage, at least one boom and a wing structure including a first lifting surface having a first root portion located proximate the at least one boom and a first tip portion where at least a portion of the f...
|
|
WO/2022/050928A1 |
A wing (1) for a vertical takeoff and landing aircraft (2) consists of an airfoil portion (3) and, hingedly attached thereto, a first high lift section (4) comprising a set of propulsors (6) arranged above the profile of the wing. The wi...
|
|
WO/2022/049379A1 |
A hybrid VTOL drone is provided and comprises a minimum of four propellers fixedly mounted and disposed onto a frame that includes a pitch shaft, and a wing rotatably mounted to the pitch shaft, wherein the wing is rotatable around a pit...
|
|
WO/2022/049764A1 |
[Problem] To provide a flying vehicle by which it is possible to simultaneously realize vertical taking-off and landing and improving fuel economy, and realize stable landing. [Solution] This flying vehicle comprises a flight unit to whi...
|
|
WO/2022/045539A1 |
The present invention relates to an aircraft wing. The aircraft wing comprises: a lightning protection apparatus which is installed on the surface of the aircraft wing to transmit the electrical energy of lightning to the surroundings wh...
|
|
WO/2022/038505A1 |
A wing movement mechanism of an aircraft, specifically an unmanned aircraft, has a wing (2) attached to the fuselage (9) of the aircraft at a single point (3) which is fixed relative to the fuselage (9), with the possibility of movement ...
|
|
WO/2022/040463A1 |
Airfoils and vehicles incorporating the same are disclosed herein. The airfoils include an upper surface and a lower surface. Each airfoil is configured for operative connection to an airframe via the upper surface of the airfoil. Each a...
|
|
WO/2022/027840A1 |
A deformable wing-based agricultural bionic bird repelling drone, comprising a body (1), wings, a tail wing (2), and a power module, a bionic audio transmitting module (3), an ultrasonic transmitting module (4), a strong light emission m...
|
|
WO/2022/023974A1 |
Process for manufacturing a structural component (1, 1', 1", 1"', 1"") made of composite material comprising a skin (2) and at least one stiffening stringer (3, 3', 3", 3"', 3"") applied rigidly and integrally to one face (2a) of the ski...
|
|
WO/2022/024051A1 |
Disclosed is a reconfigurable wing sail 10 for a yacht. The sail 10 is configured to have an effective sail area that can be adjusted by extending or retracting a nested wing sail 10 vertically through a boom 18 or head of a primary wing...
|
|
WO/2022/023045A1 |
A winglet (10) is disclosed, with first and second covers (20, 22), a front spar (24), a rear spar (26), and a mid spar (28) between the front spar (24) and the rear spar (26). Each spar is joined to the first cover (20) and to the secon...
|
|
WO/2022/023975A1 |
Process for manufacturing a structural component (1, 1', 1", 1''', 1"" ) made of composite material comprising a skin (2) and at least one stiffening stringer (3, 3', 3", 3"', 3"") applied rigidly and integrally to one face (2a) of the s...
|
|
WO/2022/019856A1 |
This invention relates to a body (2), at least one control surface (3) located on the body (2), enabling to control the flow of fluid by moving relative to the body (2), at least one actuator (4) produced from an electro-active polymer m...
|
|
WO/2022/012827A1 |
The invention relates to a wing locking system (10) for vertical power plants in EVTOL aircraft and to an EVTOL aircraft (42) comprising at least one such wing locking system (10). According to the invention, a wing locking system (10) f...
|
|
WO/2022/011802A1 |
Disclosed is a flying car, comprising a car module (1) and a flying module (2). The flying module (2) is arranged on the upper part of the car module (1). The flying module (2) comprises wings (21), wherein each wing (21) has a folded st...
|
|
WO/2022/005328A1 |
A device for supplying additional electrical energy to the power system of an aircraft is provided with at least one flexible element arranged along the length of the wing of an aircraft and fastened by one end to said wing, the second e...
|
|
WO/2022/000367A1 |
A wing structure for a vehicle, and a vehicle. The wing structure comprises at least one multi-connecting-rod structure. The multi-connecting-rod structure is arranged in a direction extending from the main body of a vehicle to a wingtip...
|
|
WO/2021/261676A1 |
Disclosed is an elastic shape-memory polymer composite skin having a zero Poisson's ratio. The elastic shape-memory polymer composite skin comprises: a body formed of conductive fibers; a plurality of metal frames that are disposed on a ...
|
|
WO/2021/260688A1 |
A wing system is provided for an air vehicle, the air vehicle having a fuselage including a fuselage section and a fuselage longitudinal axis, the wing system having at least one wing deployment module. Each wing deployment module includ...
|
|
WO/2021/257271A1 |
Fluid systems are described. An example fluid system includes a body and a housing. The body has a leading edge, a trailing edge, a first portion, and a second portion attached to the first portion. The second portion is moveable relativ...
|
|
WO/2021/250660A1 |
A wing system is provided for an air vehicle, the wing system having a stowed configuration, a pre-deployed configuration, and a deployed configuration. The wing system includes two wings, each wing having aerofoil profiles and being piv...
|
|
WO/2021/248003A1 |
A fixed wing drone comprises an air channel embedded therein. The air channel has an upstream an air inlet. A microcontroller mounted within the drone is configured to control navigation of the drone. An air scoop having a section positi...
|
|
WO/2021/238637A1 |
The present invention provides a sickle-winged vertical take-off and landing aircraft, which is of a high wing structure. The wing comprises a wing root part and a wing tip part; a leading edge of the wing root part is integrally straigh...
|
|
WO/2021/232753A1 |
An aircraft and an aircraft control system. The aircraft (100) comprises a fuselage (10) and a wing (20) that is connected to the fuselage (10), and further comprises a detection apparatus (30) that is assembled on the fuselage (10) and ...
|
|
WO/2021/233574A1 |
The invention relates to an aircraft having the following features: The aircraft has a wing (10) with an integrated ducted propeller (20); the ducted propeller (20) is provided with inlet blades (13) and outlet blades (14); and at least ...
|
|
WO/2021/233572A1 |
The invention relates to an aircraft having the following features: The aircraft has a wing (10) with an integrated ducted propeller (20); the inducted propeller (20) is selectively provided with inlet blades (13) and outlet blades (14);...
|
|
WO/2021/233573A1 |
The invention provides an aircraft having the following features: the aircraft comprises an airfoil (10) having an integrated ducted fan (20); an inlet lip runs around at least parts of the ducted fan (20); and the inlet lap has a gentle...
|
|
WO/2021/224844A1 |
A method of realization of an aeronautical item with hybrid composite materials by means of additive technology comprising the steps of: design of the product by means of a three-dimensional mathematical model which defines, in a referen...
|
|
WO/2021/224207A1 |
The invention relates to a method for producing an arc-shaped fibre composite component. A preform with a flat fibre layer arrangement along an arc is formed, the arrangement having an outer edge associated with a convex outer side of th...
|
|
WO/2021/212707A1 |
A wing vortex-breaking structure, a wing, and an aircraft, the wing vortex-breaking structure comprises a first opening (11) arranged on the leading edge of an aircraft wing body (1) and a second opening (12) arranged on the trailing edg...
|
|
WO/2021/209899A1 |
An unmanned aircraft, preferably a multirotor drone, equipped with means of orientation against the wind, comprising a wind sensor (6), in order to maintain said aircraft, during take-off and flight, with its nose (5) oriented against th...
|
|
WO/2021/198964A1 |
An aircraft including a fuselage with one or more wings extending from the fuselage. The aircraft may include one or more apertures in a surface of at least one of the fuselage and the one or more wings. The one or more apertures may be ...
|
|
WO/2021/186896A1 |
This composite-material blade formed by using a fiber-reinforced resin containing a resin and reinforcing fibers is provided with: a base material part provided on the inner surface of the composite-material blade; and a first cover part...
|
|
WO/2021/186411A1 |
A helicopter (1) is described comprising a fuselage (2) elongated along a first axis (X) and extending between a nose (6) and a tail boom (7); a tailplane (9) with a pair of first aerodynamic surfaces (11) elongated along a second axis (...
|
|
WO/2021/171096A1 |
A fixed-wing aircraft, comprising a fuselage (1) with at least two wings (2), one or more engines, a tail rudder (3) and stabilisers (4), and comprising two rollers (9) on two sides (8) of the fuselage (1) aligned with the plane of the c...
|
|
WO/2021/173039A1 |
The invention relates to the field of aerohydrodynamics and can be used on wings of aircrafts, controlled spoilers of cars, all-movable masts and sails of sailing yachts and on blades of various bladed machines. An aerohydrodynamic surfa...
|
