| Document |
Document Title |
|
WO/2023/096622A1 |
The invention relates to an unmanned aerial vehicle (1) arranged to self-destruct near a target (H), comprising a body (10), foldable wings (20) that comprise the wing body (21 ) connected to the body (10) and flaps (22) partially movabl...
|
|
WO/2023/095022A1 |
In an aircraft component where the aircraft component comprises a metal sheet (1.1, 1.2, 1.3, 1.4, 1.5, 1.6), the metal sheet (1.1, 1.2, 1.3, 1.4, 1.5, 1.6) comprises a normal region (5.1, 5.2, 5.3, 5.4) and a first surface milling regio...
|
|
WO/2023/091672A1 |
An aerial device is provided. The aerial device includes a processor and a memory that includes instructions configured to cause the processor to perform certain operations when the processor executes the instructions. The operations may...
|
|
WO/2023/089273A1 |
The invention relates to an open composite panel (10), comprising: - a composite skin (12) having an inner surface (18) and an outer surface (16), - a plurality of stiffening ribs (14), each rib (14) extending over the inner surface (18)...
|
|
WO/2023/034302A9 |
A system and method for lift augmentation of an aircraft having a wing with a leading edge and a trailing edge extending along a wingspan, a plurality of thrust-producing devices connected to the bottom of said wing, at least one flap co...
|
|
WO/2023/062514A1 |
A vertical take-off and landing (VTOL) vehicle (1) has a main body (10) including airfoil sections (13) on either side of a central module (20) in which a load may be carried. Articulated forward thrust systems (SOL, 50R) are mounted on ...
|
|
WO/2023/051013A1 |
The present patent discloses a vertical take-off and landing aircraft based on variable propeller wing technology and a double-propeller wing layout. A main wing surface employs a propeller wing design and may be switched between a rotor...
|
|
WO/2023/055319A1 |
The present invention relates to at least one fuselage (2) located in an air and/or space vehicle; at least one structural part (3) in the fuselage (2), which supports an inner surface of the fuselage (2) in terms of strength; a pluralit...
|
|
WO/2023/043313A1 |
Actuation device for a high-lift device of a rotor blade, comprising a first link, movable in a span- wise direction, outwardly by a centrifugal force, a biasing member, connected with the first link and configured to exert an opposite f...
|
|
WO/2023/038318A1 |
An electric propulsion aircraft according to an embodiment of the present invention comprises: a fuselage having a power means; a front spar and a rear spar extending from the fuselage to the end of a wing; and a plurality of ribs extend...
|
|
WO/2023/026662A1 |
The present invention provides a skin member and a blade structure which are lightweight yet ensure strength. A skin member (100) forms an outer plate of the blade structure, and comprises: a lattice-like framework material (110) forming...
|
|
WO/2023/021054A1 |
An airborne craft comprises multiple crossflow fan LPCEs (Lift, propulsion and control element), arranged around a central fuselage in such a way that the LPCEs provide both distributed propulsion in forward flight and sufficient vertica...
|
|
WO/2023/022680A1 |
The present invention relates to an unmanned air vehicle (10) comprising a body (100); at least four propellers (101) where at least two of said propellers (101) are provided on a front edge of said body (100) and where at least two of s...
|
|
WO/2023/019404A1 |
An arm assembly (100), comprising a first component (10) and an arm (20). The first component (10) is movably connected to a fuselage (300) of an aerial vehicle (1000); the arm (20) is rotatably connected to the first component (10), so ...
|
|
WO/2023/016761A1 |
An aerostructure component (6) comprises a core (10) sandwiched between two skins (7, 8), each skin comprising at least one ply (e.g. 9a) of a plurality of elongate reinforcing elements in a metal matrix (36) and the core comprising a pl...
|
|
WO/2023/282294A1 |
This flight equipment (100) comprises: a thrust device (10) that provides thrust during flight; wings (20) that maintain the attitude during flight and change the direction of flight; a control part that controls the strength of output f...
|
|
WO/2023/282278A1 |
This morphing wing (140) comprises: a link structure capable of expanding in a first direction and retracting in a second direction, which is opposite to the first direction; a plurality of front wing covers (180) mounted frontward, whic...
|
|
WO/2023/274826A1 |
A foldable sheet material (10) having a plurality of stiff sections (12) which are foldable or rotatably connected along straight edges (14), wherein a straight primary edge (16) extends from a first point (18) on the margin of the sheet...
|
|
WO/2022/266807A1 |
An unmanned aerial vehicle (100), comprising a fuselage (10) and a plurality of arms (20). The plurality of arms (20) are rotatably connected to the fuselage (10) to allow the unmanned aerial vehicle (100) to be in a folded state or an u...
|
|
WO/2022/263949A1 |
A series of convertible aircraft (1, 1') with a core (100) with an airframe (2) defining a first axis (Y) is described; a first, a second, a third, a fourth, a fifth and a sixth rotor (20a, 20b, 21a, 21b, 22a, 22b) which are rotatable ab...
|
|
WO/2022/260894A1 |
The present disclosure is drawn to an aircraft wing assembly that can include an airfoil including a leading edge, a first slat positioned or positionable upwind relative to the leading edge leaving a first airflow gap between the first ...
|
|
WO/2022/238431A1 |
The present invention relates to an aircraft 1. The aircraft 1 comprises a fuselage 11, a propulsion mounting spar 12, a propulsion unit 13, and a tillable wing 14. The propulsion unit 13 is mounted to the fuselage 11 by the propulsion m...
|
|
WO/2022/235684A1 |
The invention describes a Vacuum Shell Airfoil to produce lift that is necessary to propel and suspend aircraft such as Vertical Take Off and Land (VTOL) aerospace vehicles which includes: (1 ) a circular shell, and (2) multiple fins whe...
|
|
WO/2022/235145A1 |
The invention relates to aviation equipment. An object of this invention is to develop a new device, which can extend the range of aerodynamic devices for aviation, increase the efficiency of the air flow power use around the wing, and i...
|
|
WO/2022/003672A9 |
A wing system is provided for an air vehicle, the air vehicle having a fuselage including a fuselage longitudinal axis. The wing system includes a set of wings, configured for transitioning between a stowed configuration and a deployed c...
|
|
WO/2022/204278A1 |
Wind turbine blades and wind turbine systems that include a co-flow jet are described. An example wind turbine blade has a main body and a fluid pressurizer. The main body has a. first portion, a second portion, a leading edge, a trailin...
|
|
WO/2022/187426A2 |
A vehicle is provided, configured to selectively operate in a driving mode and in a flying mode. The vehicle comprises a body defining a passenger compartment and carrying driving and flying arrangements to facilitate the driving and fly...
|
|
WO/2022/180355A1 |
An aircraft wing comprising: a wingbox; a fuel tank; a fuel cell system comprising a fuel cell; a fuel line configured to deliver fuel from the fuel tank to the fuel cell system; a propulsion system carried by the wingbox; and an electri...
|
|
WO/2022/179743A1 |
The invention relates to a wing system (10) comprising an aerodynamic wing structure (20) which can be stowed, in particular a wing structure which can be rolled up and/or folded, comprising at least one pressure-tight tubular pressure c...
|
|
WO/2022/175071A1 |
The present invention relates to a wing assembly (10) for an aircraft with a fuselage and at least one pair of wings, the wing assembly (10) defining a direction of flow (F) with respect to which the wing assembly (10) is configured to c...
|
|
WO/2022/170733A1 |
A drag reduction device (2), comprising a first part (21) and a second part (22). The first part is connected to the second part, and the second part is detachably connected to a body (1); the first part is made of a flexible material, a...
|
|
WO/2022/167875A1 |
There is described a hybrid aircraft (1) of the unmanned type, configured for the joint and optimized use of aerostatic and aerodynamic force, comprising an inflatable body (10) including an outer shell (11) and a load-bearing structure ...
|
|
WO/2022/157245A1 |
An aircraft propulsion module comprises a hydrogen storage system, an electrochemical converter (7) connected to the hydrogen storage system, wherein the at least one electrochemical converter is adapted to convert hydrogen supplied from...
|
|
WO/2022/148940A1 |
A propulsion unit for an aircraft comprising a turbomachine (1) having at least one rotary part (30) rotating about an axis of rotation (A), a mounting pylon (40), and a structural element (10) supporting the turbomachine (1) by way of t...
|
|
WO/2022/140925A1 |
A fluid guiding device (100), an aircraft (200), a blade (201), a control method for the fluid guiding device (100), and a control method for the aircraft (200). The fluid guiding device (100) comprises a rotating mechanism (11), a base ...
|
|
WO/2022/146248A1 |
The present invention relates to a self-healing sandwich composite structure that comprises, at least one thermoset polymer resin filled capsule (1), at least one thermoset polymer resin activator filled capsule (2), at least one sandwic...
|
|
WO/2022/144723A1 |
The invention relates to a monolithic structure (1) in composite material manufactured starting from a fiber-reinforced prepreg material and comprises two walls (6, 7) facing each other and at least one interconnection element (8) extend...
|
|
WO/2022/140362A1 |
The disclosed embodiments are directed to a modular autonomous vehicle system comprising a blended wing body module, at least two high speed long range wing panel modules configured to interchangeably mount to the blended wing body modul...
|
|
WO/2022/130818A1 |
Provided is a flying body, comprising: a wing part; a battery disposed in the wing part; an intake part formed in a position corresponding to the battery on the front side of the wing part; a heat sink part which is disposed with respect...
|
|
WO/2022/132832A1 |
Aspects of the disclosure relate to an aerial vehicle. The aerial vehicle may include an envelope having a plurality of tendons and formed from a first plurality of gores. The aerial vehicle may also include one or more ballonets arrange...
|
|
WO/2022/114697A1 |
Disclosed is a transformable wing, which comprises: a main wing including multiple ribs extending in the forward and backward direction of the wing wherein the multiple ribs are arranged at intervals in a lengthwise direction of the wing...
|
|
WO/2022/111678A1 |
An aircraft leading edge assembly (10) having a leading edge end (11) facing a forward direction and a trailing edge end (12) facing away from the forward direction, the leading edge assembly comprising: a first bulkhead plate (110), a s...
|
|
WO/2022/104775A1 |
Provided are a wing panel structure for an aircraft, a wing structure, and an aircraft. The wing panel structure comprises a plurality of wing panel units, and adjacent wing panel units are connected by means of an airfoil control unit (...
|
|
WO/2022/104769A1 |
Embodiments of the present disclosure provide an airfoil structure, a wing structure and an ornithopter. The airfoil structure comprises multiple airfoil units. Adjacent airfoil units are connected by means of an airfoil control unit and...
|
|
WO/2022/104779A1 |
A wing panel structure for an aircraft, a wing structure comprising the wing panel structure, and an aircraft. The wing panel structure comprises a plurality of wing panel units; the adjacent wing panel units are connected by means of an...
|
|
WO/2022/107109A1 |
A method is described for manufacturing a structural element (2) in composite material extending along a straight or curvilinear longitudinal direction (D), having a Z-shaped cross section and comprising, in its final configuration, a ce...
|
|
WO/2022/101525A1 |
The invention discloses a procedure for manufacturing an inflatable structure, where the structure comprises at least one body (1) formed by a piece of thermoplastic polymer fabric (2) configured to house an air chamber (3), such that th...
|
|
WO/2022/102336A1 |
Provided is a flight device having a wing part that is capable of efficiently providing lift during flight. This flight device 10 is equipped with: an air frame base 14; a first leg 26 and a second leg 27 which are provided to the air fr...
|
|
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...
|
