| Document |
Document Title |
|
WO/2022/019854A1 |
This invention relates to a body (2) located in an air and/or space vehicle, at least one control surface (3) which is located on the body (2) and which by moving relatively to the body (2), enables air flow to be controlled and the air ...
|
|
WO/2022/019853A1 |
The present invention relates to a body (2) in an air and/or space vehicle, at least one control surface (3) on the body (2), moving relative to the body (2), thereby enabling to control the air flow and the air vehicle to maneuver, at l...
|
|
WO/2021/262420A1 |
A multirotor drone comprises a main body and an air channel embedded within the main body having an air inlet on the surface of the main body, multiple propellers that induce an air flow toward the air inlet and into the air channel, a m...
|
|
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/2021/180504A1 |
An aircraft system has a first structure, and a second structure coupled to the first structure and movable between first and second positions relative to the first structure. The aircraft system has an electrical connector for providing...
|
|
WO/2021/180505A1 |
Disclosed is an electrical connection apparatus for providing an electrical connection between a first structure of an aircraft system and a second structure of an aircraft system, the second structure movable relative to the first struc...
|
|
WO/2021/178077A1 |
A wireless autopilot system includes an aircraft attachment device having a mounting plate for securement onto a flight control surface of an aircraft, and a flight control device that is hingedly connected to the aircraft attachment dev...
|
|
WO/2021/165268A1 |
The invention relates to a method for manufacturing an aerodynamic structure (34) comprising a first panel (42) having an aerodynamic face (F34) as well as a second reinforced panel (44), characterised in that the manufacturing method co...
|
|
WO/2021/122587A1 |
The present invention relates to the provision of a spoiler actuation apparatus for moving an aircraft spoiler. The spoiler is moveable between a stowed configuration and a deployed configuration. The spoiler actuation apparatus comprise...
|
|
WO/2021/104938A1 |
Described and claimed is a wing for an aircraft comprising a fixed wing, a high-lift device and a hold-down arrangement arranged between two supports of the high lift device comprising a first hold-down element attached to the high-lift ...
|
|
WO/2021/104808A1 |
Described and claimed is a wing (5) for an aircraft (1) comprising a fixed wing (7), a high-lift device (15) and a hold-down arrangement (27) arranged between two supports (23, 25) of the high lift device (15) comprising a first hold-dow...
|
|
WO/2021/104810A1 |
Described and claimed is a wing (5) for an aircraft (1) comprising a fixed wing (7), a high-lift device (15) and a hold-down arrangement arranged (27) between two supports (23, 25) of the high lift device (15) comprising a first hold-dow...
|
|
WO/2021/104940A1 |
Described and claimed is a wing for an aircraft comprising a fixed wing, a high-lift device and a hold-down arrangement arranged between two supports of the high lift device comprising a first hold-down element attached to the high-lift ...
|
|
WO/2021/099109A1 |
A slat arrangement (2) for a wing of an aircraft (58) is proposed, the arrangement (2) having a movable leading-edge slat (4) and a connection section (6), wherein the leading-edge slat (4) comprises a slat leading edge (5) having and a ...
|
|
WO/2021/099710A1 |
The aerodynamic element (1) has at least one fixed first aerodynamic part (2) having a box structure (3) covered at least in part by a plate (6A) with an end part (7A), a second aerodynamic part (13) having a peripheral surface (14) with...
|
|
WO/2021/094169A1 |
An aircraft wing comprising a first structure connected to a second structure such that the first and second structures are relatively moveable between a retracted configuration in which a contact edge of the first structure abuts the se...
|
|
WO/2021/083822A1 |
An aircraft wing (2) having a main wing (3) and a trailing edge flight control surface (4) movable between a retracted position, a first extended position in which the control surface is positioned rearwardly in the chord wise direction ...
|
|
WO/2021/083821A1 |
The invention provides an aircraft wing (102, Figure 2) comprising a leading edge slat (110') and a fixed aerofoil portion (104). The leading edge slat (110') is moveable between a stowed position and deployed position. In the deployed p...
|
|
WO/2021/083664A1 |
In order to improve sealing at the transition between high-lift devices and fairings, the inventions suggest a shutter assembly (54) which may be installed in a high-lift system (16), thereby forming the shutter arrangement (24). The shu...
|
|
WO/2021/087482A1 |
A heating system is configured to produce heated fluid. The system includes a source of primary fluid, a diffusing structure comprising an outlet structure out of which the heated fluid flows, at least one conduit coupled to the source a...
|
|
WO/2021/079250A1 |
A roller unit (13) for moving a slat of an aircraft wing is adjustable in height and axial position to adjust the gap (G) between the idle roller (14) and a guide (10) integral with the slat. The roller is carried by an eccentric pin (24...
|
|
WO/2021/078204A1 |
An unmanned aerial vehicle having dual coaxial propellers. The unmanned aerial vehicle comprises a protective housing (1), a propeller assembly (2), a first balance ring (3), a second balance ring (4), a mounting rod (5), a drive assembl...
|
|
WO/2021/062229A1 |
The 3D extension linkage 100 can include at least one arm that includes two elements connected by a joint. The linkage can include an actuation mechanism, additional arms and/or each arm can include more than two elements, tie rods and/o...
|
|
WO/2021/059787A1 |
A control device of this embodiment comprises: an acquisition unit that acquires information indicating the strain of a vane of a structure, and information indicating a control amount of a movable vane of the structure; a first determin...
|
|
WO/2021/052908A1 |
In order to improve space allocation, reduce weight and increase aerodynamic performance in high-lift devices (20), an actuator arrangement (24) for a fixed leading edge member (26) is proposed. The fixed leading edge member (26) has an ...
|
|
WO/2021/044141A1 |
A vehicle control system (110) for use with at least one fluidic control effector (102) for a vehicle, the vehicle control system (110) comprising a controller (110), wherein the controller is configured to: receive a vehicle control inp...
|
|
WO/2021/037981A1 |
The invention relates to a leading edge assembly (9) for a wing (3). The leading edge assembly comprises a housing (11) which is configured to be connectable to a fixed wing section (59) of the wing (3) and in which a first opening (19) ...
|
|
WO/2021/038911A1 |
Provided is a cross flow fan that makes it possible to reduce fluid loss. The cross flow fan is provided with a plurality of vanes (15) arranged around a rotation axis O1 at predetermined intervals in the circumferential direction, a ton...
|
|
WO/2021/009060A1 |
The invention relates to a wing (3) for an aircraft (1), comprising a main wing (5), a slat (7), and a connecting assembly (9) movably connecting the slat (7) to the main wing (5), such that the slat (7) is movable between a retracted po...
|
|
WO/2021/004110A1 |
A water-air amphibious cross-medium bionic robotic flying fish, comprising a body, pitching pectoral fins (4), structure variable pectoral fins (5), a tail propulsion module, a detection sensor and a controller. The present invention con...
|
|
WO/2021/005050A1 |
A movable flow body device for an aircraft is proposed, comprising an elongated flow body having a main extension axis, a first mechanical interface in a first position along the main extension axis, a second mechanical interface in a se...
|
|
WO/2020/260391A1 |
A leading-edge arrangement for an aircraft is proposed, comprising a plurality of movable flow bodies, a supply duct, an air transfer duct, and at least one perforated tube, wherein the movable flow bodies are arranged in a consecutive a...
|
|
WO/2020/254560A1 |
Disclosed is an actuation unit (15) for actuating a foldable wing tip portion (9) of a wing (3) for an aircraft (1), the actuation unit (15) comprising a motor (17) configured to be mounted to a fixed wing (5) for an aircraft (1), a driv...
|
|
WO/2020/245549A1 |
A space aircraft (1) comprises a fuselage (3), two wings (4A, 4B) arranged on either side of the fuselage (3), and two nacelles (7A, 7B) arranged at the ends of the wings (4A, 4B) and each carrying a horizontal tail (8A, 8B) and a vertic...
|
|
WO/2020/239699A1 |
A flow body for an aircraft, in particular for a wing leading edge device, is proposed, the flow body having a curved front skin having a leading edge and at least one trailing-edge component coupled with at least one spanwise edge of th...
|
|
WO/2020/239753A1 |
In order to reduce vibration of movable airfoil structures (38), such as rudders (22), elevators (24), and ailerons (20), a spring device (48), a leaf spring (50) for example, is mounted to an airfoil mounting structure (28), such as a v...
|
|
WO/2020/237529A1 |
Provided are a flight control method and apparatus for an unmanned aerial vehicle, and an unmanned aerial vehicle. The method comprises: acquiring a flight mode switching command, the flight mode switching command instructing an unmanned...
|
|
WO/2020/216737A1 |
An embodiment of the present invention provides an aerostructure assembly of an aircraft comprising a first aerostructure portion (201) extending in a direction between a first position (bl) and a second position (b2) and comprising stru...
|
|
WO/2020/212568A1 |
The invention concerns a spar structure (11) for connecting a moveable component (4) to an aircraft. The structure is formed from a single continuous body of material defining a plurality of attachment/actuation brackets (10A-10F) and a ...
|
|
WO/2020/196524A1 |
[Problem] To provide a flying vehicle capable of improving drive feelings and ride comfort for a person on board. [Solution] A flying vehicle which a person can get on board and which moves by floating above the ground is provided with a...
|
|
WO/2020/196525A1 |
[Problem] To provide a flying vehicle capable of improving drive feelings and ride comfort for a person on board. [Solution] A flying vehicle which a person can get on board and which moves by floating above the ground is provided with a...
|
|
WO/2020/187092A1 |
An unmanned aerial vehicle control device, comprising a master controller (11) and a rudder surface control structure (12). The rudder surface control structure comprises a driving controller (121), a driving mechanism (122), a transmiss...
|
|
WO/2020/186305A1 |
A vertical take-off and landing (VTOL) aircraft (100) having: a wing structure having right and left side forward wings (20, 22); and right and left side rearward wings (30, 32), each of the right side wings (20, 30) being connected, and...
|
|
WO/2020/187094A1 |
An unmanned aerial vehicle control device, comprising a main controller (11), a control surface control structure, and an angle detecting module; the control surface control structure comprises a drive controller (121), a drive mechanism...
|
|
WO/2020/185947A1 |
A winged vertical take-off and landing aircraft with compound control surfaces comprising flaps and ailerons which can be operated simultaneously with each other offers improved aerodynamic performance and maneuverability. Configuration ...
|
|
WO/2020/174084A1 |
A wing leading-edge device (2, 42) is proposed, which comprises a slat body (4, 42) having a front side (6) with a forward skin (8) and a back side (10) with a rearward skin (12), and at least a drive arrangement (14) having at least one...
|
|
WO/2020/157052A1 |
The invention relates to an aircraft (1). Said aircraft is characterized by a wing (2) which, viewed in section, is delimited on one side by a first profiled surface (4), which is at the bottom when the aircraft (1) is operated as intend...
|
|
WO/2020/142416A1 |
Technologies for providing blended wing body aircraft control surfaces are described herein. In some examples, one or more of the control surfaces have angular configurations that reduce the formation of air vortexes when in upward or do...
|
|
WO/2020/107581A1 |
A movable platform (10) and steering engine thereof. The steering engine (10) comprises: an upper cover (110), a lower cover (130), and a middle shell (120) disposed between the upper cover (110) and the lower cover (130), wherein a top ...
|
