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WO/2019/124686A1 |
A flight controller of a vertical take-off and landing aircraft, according to one embodiment of the present invention, controls a tilt angle of a main rotor on the basis of a vertical posture control signal in a low-speed flight state. W...
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WO/2019/122926A1 |
The present invention provides an aircraft described as an Airborne Urban Mobility Vehicle with VTOL (Vertical Take-Off and Landing) capability. The aircraft has a fuselage freely pivoted between lateral arms of a yoke;the arms of the yo...
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WO/2019/114884A1 |
The invention relates to a modular vertical take-off and landing aircraft (1) for transporting persons and/or loads, having: — a flight module (2) with multiple drive units (4) arranged on a wing assembly (3), each drive unit (4) havin...
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WO/2019/114887A1 |
The invention relates to a take-off and landing station (1) for a flying vehicle (2) for transporting people and/or loads, which flying vehicle takes off and lands vertically and comprises a flight module (3), having a plurality of drive...
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WO/2019/114886A1 |
The invention relates to a transport module (1) for a vertical take-off and landing aircraft for transporting persons and/or loads, having a conveying pod (2) and a connection device (3) for connecting the conveying pod (2) to a flight m...
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WO/2019/114888A1 |
The invention relates to a charging station (2) for a vertical take-off and landing aircraft (1) comprising one or more energy stores, the station having a charging device for transferring electrical energy to the energy store or stores....
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WO/2019/114885A1 |
The invention relates to a flight module (1) for a vertical take-off and landing aircraft comprising multiple drive units (3) arranged on a wing assembly (2), the wing assembly (2) having wing assembly struts (5) interconnected at node p...
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WO/2019/118212A1 |
A corrugated lift fan rotor is disclosed. In various embodiments, a rotor includes an upper skin, a lower skin, and an at least partly corrugated core encased between the upper skin and the lower skin. In some embodiments, the core compr...
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WO/2019/116101A1 |
A variable-geometry vertical takeoff and landing (VTOL) aircraft system may transport passengers from a departure point to a destination via partially or fully autonomous flight operations. The VTOL aircraft system may operate in hover-b...
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WO/2019/110830A1 |
A propulsion device, including a platform configured to support a passenger thereon; a thrust engine coupled to the platform, wherein the thrust engine is configured to provide a thrust output substantially along a first axis; a deflecto...
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WO/2019/112682A1 |
Autonomous flight is performed in an open loop mode over a first range of altitudes, wherein a plurality altitude-related data from a plurality of altitude-related sensors is ignored while performing the autonomous flight in the open loo...
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WO/2019/109306A1 |
An unmanned aerial vehicle (100), comprising a vehicle body (10), multiple rotor power assemblies (20) provided on the vehicle body (10), and fixed-wing power assemblies (30) detachably mounted on the vehicle body (10). When the fixed-wi...
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WO/2019/108517A1 |
Devices, systems, and methods are provided in which a wing of a tiltrotor aircraft is rotated during operational flight, for example from a position perpendicular to the aircraft's fuselage through an angle of 30 or more in the direction...
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WO/2019/108091A1 |
The invention relates to the field of aviation, and more particularly to designs and flight methods for manned aircraft. A personal aircraft comprises an X-shaped body, and two retractable wings equipped with flaps and fastened to the fr...
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WO/2019/103661A1 |
The invention relates to the field of aviation, and more particularly to designs for vertical take-off and landing aircraft. A convertiplane comprising a fuselage, a pair of wings: fore and aft, propulsion systems comprising engines and ...
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WO/2019/098443A1 |
The present invention provides a method for setting a pest control route by using an unmanned vehicle, comprising: a step of acquiring position information of a plurality of waypoints arranged along the boundary of a working area; a refe...
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WO/2019/094804A1 |
Exhaust redirecting devices are described that are suitable for use in tilt rotor aircraft. Such devices are constructed of light weight material and permit redirection of exhaust gases from turbojet engines of tilt rotor aircraft as nac...
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WO/2019/090999A1 |
A vertical takeoff and landing fixed-wing aircraft comprises a fuselage and semicircular wings (2) symmetrically distributed relative to the fuselage on the left and on the right. Propellers (3) rotating around the axial directions of th...
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WO/2019/094765A1 |
A system and method of an airflow control system for a vehicle is described herein. The airflow control system (100) includes an airflow housing (120) defining an airflow passageway (125) extending between a bypass opening (122) and an i...
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WO/2019/093913A1 |
The solution according to the present invention is a drive unit for air vehicle, which allows building the vertical take-off and landing vehicles, intended for application, for instance, in the production of flying taxis, as well as in t...
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WO/2019/091549A1 |
The aim of the invention is to provide an aircraft (100) which, on the one hand, facilitates simple taking off and landing in limited space and, on the other hand, facilitates a large range and a high travelling speed. This aim is achiev...
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WO/2019/089839A1 |
A bladeless unmanned aerial vehicle includes a body and two or more thruster assemblies coupled to the body. The thruster assemblies each includes a ducted fan compressor and a discharge frame. The discharge frames may be bladeless fans ...
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WO/2019/090046A1 |
An aircraft includes an airframe having a fixed-wing section and a plurality of articulated electric rotors, at least some of which are variable-position rotors having different operating configurations based on rotor position. A first o...
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WO/2019/090191A1 |
A vertical landing and take-off aircraft VTOL transitions from a vertical takeoff state to a cruise state where the vertical takeoff state uses propellers to generate lift and the cruise state uses wings to generate lift. The aircraft ha...
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WO/2019/086742A1 |
The present invention relates to an assembly of three wings joined with or without marginal plates, for aerial, water, land or space vehicles, to reduce induced drag and interference drag and provide greater manoeuvrability, independence...
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WO/2019/082043A2 |
A vertical take-off and landing aerial vehicle (VTOL) includes a plurality of rotors for producing lift. For each respective rotor the VTOL has an auxiliary power source (APS) and a transformation gear set (TGS) both being associated wit...
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WO/2019/080179A1 |
An unmanned aerial vehicle release mechanism, comprising: a servo motor (101), the servo motor (101) comprising an output shaft; a servo plate (102), one end of the servo plate (102) being fixedly connected to the output shaft; a transmi...
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WO/2019/083639A1 |
Features for a tail-sitter aircraft having efficiently designed propulsive elements are disclosed. The aircraft may have a tail with landing mounts to support the aircraft in a vertical position for takeoff and landing. The aircraft may ...
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WO/2019/083646A1 |
Method and apparatus for a flight vehicle including a wing having a high aspect ratio and first and second rotors having a high aspect ratio, with a ratio of the rotor diameter to wing length ratio is equal to or greater than about 0.25....
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WO/2019/084487A1 |
A hybrid aircraft embodies an array of rotors for vertical flight positioned on support booms and wing elements for cruise flight coupled to a central fuselage housing avionics and a pusher propeller for forward propulsion. The aircraft ...
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WO/2019/083638A1 |
Features for a tail-sitter aircraft having efficiently designed propulsive elements are disclosed. The aircraft may have a tail with landing mounts to support the aircraft in a vertical position for takeoff and landing. The aircraft may ...
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WO/2019/079930A1 |
A sea-air-land-dive four-environment tilting three-rotor unmanned aerial vehicle capable of vertical take-off and landing. A right rear airbag (13), an airbag controller (14), a left rear airbag (15), a cylinder (16) and a front airbag (...
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WO/2019/079028A1 |
A VTOL aircraft (10) has a substantially delta-shaped lifting body fuselage (12) with airfoils (14, 16, 18) disposed along all three sides (20, 22, 24). In vertical flight mode the airfoils (14, 16, 18) act as exhaust diverters. A flow o...
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WO/2019/074349A1 |
The invention relates to aviation equipment. An object of this invention is to develop a new non-conventional aerodynamic apparatus that can increase the efficiency of the air flow power use to generate lifting force, control moments and...
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WO/2019/074393A1 |
The present invention relates to the field of aircraft. The proposed aircraft has the appearance of a "flying saucer" and calls to mind the astronomical phenomenon of the arrangement of the rings of Saturn, wherein the aircraft is capabl...
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WO/2019/068839A1 |
A control system for a vehicle having means to induce a flow of an ambient fluid. The control system comprises two or more arrays of vanes (130) arranged in proximity to the thrust axis of a means to induce fluid flow. Each array of vane...
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WO/2019/070124A1 |
Wind power generation system comprising a ground station (32) with an electrical energy generator (34) and an aerodynamic assembly with a wing body (2) having an aerodynamic profile with a major chord, and at least two thrust assemblies ...
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WO/2019/070752A1 |
An automated flying transport vehicle that capitalizes on the strengths and complexities of a fixed and rotary winged aircraft. The air transport vehicle comprises a body aerodynamically designed to generate lift and a plurality of rotor...
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WO/2019/062257A1 |
A double lift force ducted vertical take-off and landing aircraft based on a tilt duct, comprising an aircraft body (10), two wings (9), N tilt ducted fans (1, 2), two lift force ducted fans (5, 7), and two duct covers (6, 13), N being a...
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WO/2019/067873A1 |
A leg mechanism includes an articulated leg system (100), a passive device (130) and a cable (134). The articulated leg system (100) has a leg portion (128). The passive device (130) is coupled to the articulated leg system and is config...
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WO/2019/060933A1 |
The invention relates to a spokeless and hubless wheel (52) inside which at least one electrically driveable propeller (44) is integrated in such a way that the risks associated with propeller rotation are kept as low as possible. The wh...
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WO/2019/066484A1 |
The present invention relates to a vertical takeoff and landing aircraft. According to one embodiment of the present invention, the vertical takeoff and landing aircraft comprises: a flight fuselage (F) on which a main wing (3) and auxil...
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WO/2019/056053A1 |
A vertical take-off and landing (VTOL) aircraft (10) comprises a fuselage (24) first and second forward wings (20, 22) and first and second rearward wings (30, 32), each wing having a fixed leading edge (25, 35) and a trailing control su...
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WO/2019/056172A1 |
A flight control method for an unmanned aerial vehicle, the unmanned aerial vehicle, and a machine readable storage medium. The method comprises: control, based on a one-button start of a user, a vertical takeoff and landing fixed-wing u...
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WO/2019/056052A1 |
A vertical take-off and landing (VTOL) aircraft (10) includes a fuselage and first and second forward wings (20, 22), each wing (20, 22) having a fixed leading edge and a trailing control surface (50) which is pivotal about a generally h...
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WO/2019/040008A1 |
The operator´s module (1) is wired and/or wirelessly connected to the ground station (2), whereby the operator´s module (1) also consists of semi-transparent glasses (1a) fitted with sensors to scan the operator´s control gestures, mo...
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WO/2019/034765A1 |
The invention relates to a vertical takeoff aircraft (1), preferably an unmanned aerial vehicle (UAV), drone and/or unmanned aerial system (UAS), comprising: a rigid wing (5) which is oriented substantially horizontally both when hoverin...
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WO/2019/036011A1 |
A vertical takeoff and landing (VTOL) aircraft is configured with a front set of propellers mounted to a front wing and an aft set of propellers mounted to an aft wing wherein the propellers may be repositioned by rotating them around a ...
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WO/2019/035378A1 |
A spacecraft (100) includes a principal airframe (6), a parachute (1), which is an air brake structure, and a jetting nozzle (5). The air brake structure is provided farther on one side in a traveling direction with respect to the princi...
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WO/2019/032167A1 |
Various embodiments include a drone having a landing control device that is configured to rotate wings into an auto-rotation descent configuration causing the drone to enter a nose-down attitude and spin about a long axis of the drone, a...
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