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WO/2023/027612A1 |
The inventions relate to the field of aviation. An aircraft comprises a multisided body having rotatable cylinders (1) mounted about the perimeter thereof. For supplying air into the aircraft, the body is provided with inlets (2) that le...
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WO/2023/027611A1 |
The invention relates to the design of unmanned vertical takeoff and landing aircraft. The claimed device comprises a multisided body having rotatable cylinders (1) mounted about the perimeter thereof. Situated inside the body is a gas i...
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WO/2023/021099A1 |
A system for controlling yaw during vertical take-off and landing (VTOL) operation of an airborne craft, where the airborne craft comprises multiple crossflow fan lift, propulsion and control elements (LPCEs) disposed around a central lo...
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WO/2023/021095A1 |
A system for providing lift, propulsion and control for an aircraft vehicle that facilitates vertical take-off and landing/short take-off and landing operations is described. The system is configured to provide an airfoil that has a lead...
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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...
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WO/2023/003684A1 |
In an aspect, a system comprising a computing device. The computing device is configured to determine a drag minimization axis of a rotor connected to an aircraft. The rotor includes a first end and a second end. The rotor is configured ...
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WO/2023/000571A1 |
A flying car, comprising a car body (100) provided with a control system used for controlling the flying car to be switched between a flying state and a traveling state; wings (200) provided on two opposite sides of the car body (100), t...
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WO/2023/286785A1 |
Provided are an electric fan and an electric vertical take-off and landing craft, wherein the following are included: a boss part, a periphery part disposed around the boss part, a moving wing disposed between the boss part and the perip...
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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...
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WO/2023/282789A1 |
The invention relates to the field of aviation, and more particularly to designs for vertical take-off and landing aircraft. The present aircraft comprises a body and a power module, which are coupled to one another. The power module is ...
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WO/2023/272353A1 |
An aerial vehicle configured to fly both vertically and horizontally, suited to fighting fires or assisting search and rescue operations. The aerial vehicle has an airframe, a drive shaft, a rotor having blades that allow the angle of pi...
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WO/2022/271429A1 |
A vehicle includes a fuselage, a wing, a pylon that is coupled to the wing, and a tractor tiltrotor. The tractor tiltrotor is coupled to the pylon and is located forward of the wing; the tractor tiltrotor tilts upwards during a hover mod...
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WO/2022/263947A1 |
A convertible aircraft (1, 1') with an airframe (2) defining a first longitudinal axis (Y) is described; a pair of half-wings (3); a first, a second, a third, a fourth, a fifth and a sixth rotor (20a, 20b, 21a, 21b, 22a, 22b) rotatable a...
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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...
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WO/2022/263948A1 |
A series of convertible aircrafts (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 a...
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WO/2022/263879A1 |
The disclosure relates to hybrid unmanned aerial vehicle (UAV) having vertical take-off and landing (VTOL) capabilities. Specifically, the disclosure relates to a stable hybrid fixed angle rotor arrays UAV having VTOL capabilities with h...
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WO/2022/258946A1 |
Disclosed is a rotor assembly comprising a first rotor, a second rotor and a damper system. The first and second rotors are arranged to be rotated about a common axis for thrust generation by a drive system. The first rotor is rotatable ...
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WO/2022/260555A1 |
The invention relates to the field of aviation, and more particularly to rotary wing aircraft structures. The present aircraft comprises a fuselage, airfoils, a tail assembly, a pusher propeller disposed on the tail end of the fuselage, ...
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WO/2022/261620A1 |
A passenger vertical take-off and landing aircraft includes a flying wing comprising a passenger compartment, a first set of rotors positioned at least partially forward of a leading edge of the flying wing, and a second set of rotors po...
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WO/2022/260021A1 |
[Problem] To provide: a vertical takeoff/landing aircraft placement apparatus that is capable of shielding noise and high wind during takeoff/landing and taxing of a vertical takeoff/landing aircraft and that also enables prompt preparat...
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WO/2022/256217A1 |
Vertical take-off, landing and horizontal straight flight of an aircraft includes activation a plurality of front and rear lifting propellers, each of which is connected to a respective independently operating electric motor. In addition...
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WO/2022/243559A1 |
The invention relates to an aircraft (100) comprising an aircraft body (120) which defines a longitudinal direction, a vertical direction and a transverse direction, and at least two drive devices (1) which can rotate about a respective ...
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WO/2022/245474A2 |
Walking VTOL vehicles and related systems and methods are disclosed. A representative system can include one or more vertical thrust propulsion systems for providing vertical thrust for the vehicle, one or more horizontal thrust propulsi...
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WO/2022/243113A1 |
An electrical power distribution network (306) of an electric power system (300) of an aircraft is operated such that it sequentially adopts a plurality of different partial load sharing modes in a time variable manner, which provide for...
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WO/2022/245798A1 |
An aircraft for fixed pitch lift includes a fuselage, a plurality of flight components attached to the fuselage, wherein the plurality of flight components further comprises at least a lift propulsor component, wherein the lift propulsor...
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WO/2022/243112A1 |
An electrical power distribution network (306) of an electric power system (300) of an aircraft is operated in at least one normal operation mode such that it provides for load sharing across electrical power sources (A, B, C, D) with re...
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WO/2022/239342A1 |
The present invention provides a ducted fan apparatus and an aircraft that can achieve suppression of lip separation, increase in thrust, improvement of silencing property, and the like. This ducted fan apparatus comprises: a plurality o...
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WO/2022/238751A1 |
Vertical take-off aircraft provided with canards (1) and primary wings (2), which primary wings (2) are provided with two or more primary thrusters (20). The primary wings (2) are rotatable alternately in a vertical configuration for ver...
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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...
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WO/2022/229201A1 |
The invention relates to a vertical takeoff aircraft (1) having two wings arranged on an aircraft fuselage (2) of the aircraft (1). Along each wing (3), in each case at least one pivoting drive unit (5) is arranged pivotably on the wings...
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WO/2022/221916A1 |
Some embodiments relate to a system for communicating with vertical take-off and landing (VTOL) aerial vehicles. An example system comprises: a central server system comprising: a central server system wireless communication system; at l...
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WO/2022/225421A1 |
The invention relates to the field of aviation, and more particularly to designs for compound aircraft capable of vertical take-off and landing and of horizontal flight in copter mode, with the axes of rotation of the propellers in a nea...
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WO/2022/216602A1 |
A mobile emergency communication and vehicle propulsion power system, method, and apparatus for full-scale, clean fuel, electric -powered vehicles having a fuel cell module including a plurality of fuel cells working together to process ...
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WO/2022/211406A1 |
An unmanned non-stop flight device according to an aspect of the present invention comprises: a cold jet propulsion device; one or more hybrid propulsion devices including a jet engine propulsion device; and a flight control device. The ...
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WO/2022/204572A1 |
A detachable, self-balancing, pod for an unmanned aerial vehicle. The pod is configured to hold a plurality of different payloads, and to dynamically shift the location of these payloads in order to maintain an optimal center of mass (ce...
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WO/2022/200883A1 |
An aircraft, in particular a personal air mobility aircraft or a drone, comprising one or more annular propellers (2), with one or more blades (3) extending radially from a rotor ring body (2A) towards the axis (4) of the rotor ring (2A)...
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WO/2022/198225A1 |
A system of a multi-rotor aircraft that capitalizes on the advantages of fixed wing elements combined with rotary wing structures. The fixed wing elements can help to generate lift once the aircraft is airborne and can thus reduce the ne...
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WO/2022/192977A1 |
A brushless DC motor is integrated with an aeropropulsive thrust generator that is hubless, not in tandem (co/counter) rotating propeller disks, and not having magnetic bearings.
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WO/2022/189898A1 |
An aircraft (1) capable of hovering is described, comprising a motor member (10); a rotor (5) connected to the motor member (10); a transmission shaft (11) rotatable around a first axis (B) and adapted to drive the rotor (5); and a trans...
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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...
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WO/2022/184672A1 |
The invention relates to a vertical takeoff and landing hybrid drone comprising at least two substantially parallel fixed wing structures (12, 14) each one comprising at least two ailerons (16a, 16b, 18a, 18b) distributed one on each sid...
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WO/2022/184355A1 |
The present invention provides an engine (310) of a vertical take-off and landing aircraft (300), wherein the engine is configured to be movable with respect to an aircraft component (342) of the aircraft (300) between a hover position f...
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WO/2022/184499A1 |
The present invention provides an engine (310) of a vertical take-off and landing aircraft (300), wherein the engine is configured to be movable with respect to an aircraft component (342) of the aircraft (300) between a hover position f...
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WO/2022/180755A1 |
An aircraft 1 takes off vertically. The aircraft 1 comprises: a fuselage 10; one or more pairs of fixed wings (20-1 to 20-4) which extend from the fuselage in the right/left direction; and a plurality of first rotor blades (402-1, 402-2)...
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WO/2022/180754A1 |
An aircraft 1 that takes off and lands vertically. The aircraft 1 comprises a fuselage 10, at least one pair of fixed wings 20–1–20–4 that extend from the fuselage 10 in the left/right direction, a plurality of first rotor blades 4...
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WO/2022/179789A1 |
Ducted fan engine (1) configured for providing thrust for an aircraft (100), in particular an aircraft having vertical takeoff and landing capability, comprising: a shroud (3) having a substantially circular cross section; a stator (5) h...
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WO/2022/175116A1 |
The present invention relates to an aircraft (10), comprising a fuselage (12), wings (14, 16), and a battery system comprising at least one battery pack (24) which is disposed between an inner structural wall (20) defining an interior sp...
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WO/2022/174293A1 |
A manned vertical take-off and landing (VTOL) aerial vehicle (AV) comprising a body comprising a cockpit; a propulsion system carried by the body to propel the body during flight; pilot-operable controls accessible from the cockpit; a se...
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WO/2022/175065A1 |
The invention refers to an aircraft (1, 3), particularly an aircraft (1, 3) capable of vertical take-off and landing, comprising a fuselage (3, 4), and a variable lift body (5, 7) defining an aerofoil (51, 53) and being moveably attached...
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WO/2022/175099A1 |
The present invention relates to an integrated controller unit (10) for controlling at least one engine motor (26) and at least one servo motor (28), comprising a power link section (12) for connecting the controller unit (10) to an exte...
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