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Matches 1 - 50 out of 1,499

Document Document Title
WO/2021/000028A1
The invention relates to a novel vertical take-off and landing cocoon-type flying vehicle that pertains to the field of articles for air transportation, preferably for use in individual transportation, but optionally capable of being con...  
WO/2020/247148A9
An electrically powered vertical takeoff and landing aircraft (EVTOL) includes a payload module, a plurality of electrical power sources, a wing, and a plurality of electric thrust generators. The wing is pivotally attached to the payloa...  
WO/2020/243364A3
The subject matter described herein relates to aircraft designs and more particularly to aircraft designs using tandem wings and a distributed propulsion system. The embodiments described enable synergies between aerodynamics, propulsion...  
WO/2020/261149A1
The present invention is related to a flight propulsion system for Vertical Take-Off and Landing (VTOL) and Short Take-Off and Landing (STOL) aircraft, which comprises a two cyclorotors (1, 8), installed in the front and rear portions of...  
WO/2020/188604A4
The present invention discloses a VTOL aircraft with retractable wings and TEMCS (trailing edge mounted control surface) mounted tilt-able engines. The aircraft has two hover modes; a first hover mode with retracted wings which allows ta...  
WO/2020/260581A1
An aircraft is disclosed, having wings (2) which extend outward from the longitudinal axis and in each of which at least two rotors (3) for generating lift are provided, wherein the rotors (3) are connected to at least one flywheel in or...  
WO/2020/253614A1
Disclosed are a solar floating parking apron and a matching single-blade unmanned aerial vehicle, comprising a parking apron and a single-blade unmanned aerial vehicle. The parking apron is suspended in the air by means of the buoyancy o...  
WO/2020/256571A1
A foldable tandem wing aircraft may be fixed for flight and fold for storage, packaging or transporting and otherwise using the aircraft while not in flight is disclosed. An embodiment includes forward and rear wings which folds and unfo...  
WO/2020/247148A2
An electrically powered vertical takeoff and landing aircraft (EVTOL) includes a payload module, a plurality of electrical power sources, a wing, and a plurality of electric thrust generators. The wing is pivotally attached to the payloa...  
WO/2020/237082A1
A vertical take-off and landing aircraft which uses fixed rotors for both VTOL and forward flight operations. The rotors form a synthetic wing and are positioned to achieve a high span efficiency. The rotors are positioned to even out th...  
WO/2020/231244A1
The invention relates to oscillating propulsors. A parallelogrammatic oscillating foil mechanism comprises a foil, a drive shaft with a crank attached thereto for translational movement of the foil, said shaft having a kinematic link to ...  
WO/2020/225815A1
A vehicle adapted to travel on a road and to fly in the air comprises a vehicle fuselage, right and left foldable and deployable wings where each of the wings comprises two folding mechanisms and one tillable ducted fan. The vehicle also...  
WO/2020/215304A1
A sea-land-air-underwater adapted vehicle capable of vertical take-off and landing, comprising a fuselage (1), two main wings (2), auxiliary wings (3), a vertical tail wing (4), a rudder (5), a horizontal tail wing (6), elevators (7), a ...  
WO/2020/217117A1
An aircraft (1, 1', 1''', 1'''', 1''''', 1'''''', 1''''''', 1'''''''', 1''''''''', 1'''''''''', 1''''''''''', 1'''''''''''', 1''''''''''''') capable of vertical take-off and landing is described, comprising a first propulsion unit (6a, 6...  
WO/2020/188604A3
The present invention discloses a VTOL aircraft with retractable wings and TEMCS (trailing edge mounted control surface) mounted tilt-able engines. The aircraft has two hover modes; a first hover mode with retracted wings which allows ta...  
WO/2020/180373A3
The unified command system and/or method includes an input mechanism, a flight processor that receives input from the input mechanism and translates the input into control output, and effectors that are actuated according to the control ...  
WO/2020/212836A1
The invention relates to a propulsion device (1) for a rotating blade aerodyne with vertical take-off and landing, comprising a hollow chassis (4) and contra-rotating coaxial rotors (2, 3) with fixed-pitch blades (22, 32). The means for ...  
WO/2020/202143A1
A multirotor aircraft that comprises a body, at least three motors and at least one wing that is connected to the body. The wing is designed to be folded and unfolded during flight of the multirotor aircraft and designed to change during...  
WO/2020/193364A1
The invention relates to an aircraft with a longitudinal central axis, comprising: · a fuselage structure (2) which is designed to accommodate persons and/or payload; · a wing structure (3) which has at least two wing halves (3.1) whic...  
WO/2020/190223A1
VTOL aircraft that takeoff and land as a multirotor and cruises as airplane. The aircraft comprises two major parts: First; winged carrier frame comprises wings, engines, propellers and landing gears. Second; tilting fuselage comprises c...  
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/2020/183739A1
A tailsitter aircraft 100 provided with a body 120, two pairs of horizontal main wings 30a, 30b, 30c, and 30d when viewed from the front, each connected to the body 120, and eight propellers 50a, 50b, 50c, 50d, 60a, 60b, 60c, and 60d tha...  
WO/2020/184934A1
A vertical take-off and landing aircraft using a hybrid electric propulsion system, according to an embodiment of the present invention, includes: a first control step (S1) of changing a destination when an engine (10), a power generator...  
WO/2020/117384A3
An aircraft capable of Vertical Take-Off and Landing (VTOL) and traverse flight. The aircraft generally includes a fixed outer structure including at least a generally cylindrical wing having an internal body situated within the fixed ou...  
WO/2020/183594A1
The purpose of the present invention is to provide a tailsitter aircraft capable of roll control, pitch control, and yaw control with higher accuracy and responsiveness than conventionally. A tailsitter aircraft 1 is provided with: a b...  
WO/2020/180173A1
A flying vehicle (1) comprises: - a body (10) having a tail section (20); - a main rotor (100) having a rotation axis on top of the body; - a central thrust unit (200) arranged along the longitudinal axis of the vehicle, at a distance fr...  
WO/2020/177739A1
An aircraft realizing vertical take-off and landing and horizontal flight using bottom-drive flaps tilted in sections. A large-area plate-shaped wing is used, and movable strip-shaped flaps (4; 8; 9) and fixed strip-shaped flaps (5) are ...  
WO/2020/174648A1
Provided is a pod that is for transporting goods and that is suitable for drone transport. A pod 10 comprises: a pod housing 12 that is narrow and long and that has formed therein a main goods-chamber 18 and a sub goods-chamber 20 which ...  
WO/2020/169940A1
An aircraft comprising at least one propulsion unit configured to propel the aircraft in a first direction and at least one further propulsion unit configured to propel the aircraft in a second direction substantially opposite to the fir...  
WO/2020/169346A1
The invention relates to a method for controlling a vertical take-off and landing multirotor aircraft and to a multirotor aircraft using the controller (1).  
WO/2020/165264A1
The invention relates to a wheel propeller arrangement (1, 16) for powering vehicles (2) in driving, flying, floating or diving mode, comprising a wheel propeller (1) and a chassis (16), which wheel propeller (1) has an axis of rotation ...  
WO/2020/161607A1
The invention concerns an aerial vehicle (100) comprising: - a central frame (10), - a tail extending from the central frame (10) along a first axis (X), - at least two arms (30) extending from the central frame (10) and able to rotate a...  
WO/2020/141513A3
A VTOL aircraft comprising a plurality of motor assemblies, each configured to generate thrust by movement of air past the motor assembly along a respective axis of thrust of the motor assembly, and a wing, wherein 1) the orientations of...  
WO/2020/155460A1
Disclosed are a method for flight on the moon and a flight device using the method. A medium on the surface of the moon and a medium accelerating unit are adopted in the flight method. Under the action of electric power, the medium accel...  
WO/2020/157402A1
The invention relates to an aircraft (10) comprising a fuselage housing at least a first lift propeller having an air inlet (26) and an air outlet (28) and means for shutting off the air inlet (26) and the air outlet (28), characterized ...  
WO/2020/158361A1
This motor-integrated fan has a suction port and a blowing port, and is provided with: a rotating part rotatably supported on a shaft part; and a motor that rotates the rotating part. The motor is a peripheral drive motor that rotates th...  
WO/2020/154186A1
Systems and methods to reduce aerodynamic drag and/or affect flight characteristics of an aerial vehicle may include adjustable fairings (103-1) associated with one or more components of the aerial vehicle. The adjustable fairings (103-1...  
WO/2020/148295A1
An aircraft (1) comprising a fuselage (4), an anhedral rearwardly-swept leading wing (5) for generating lift connected to an upper portion of the fuselage, and a dihedral forwardly- swept trailing wing (7) for generating lift attached to...  
WO/2020/149495A1
A jet engine according to an embodiment of the present invention has four lift nozzles and one main nozzle for vertical takeoff and landing. Therefore, cruising, vertical takeoff and landing, transition flight and the like of an aircraft...  
WO/2020/150204A1
The present vertical lift vehicle system can include a single internal combustion engine, a single propeller, and a plurality of small ducts. The small ducts can connect to a single main duct acting as a combustion chamber, wherein the c...  
WO/2020/145640A1
The present invention relates to an aerial vehicle comprising a fixed wing and a rotary wing in a hybrid type such that vertical takeoff/landing is possible, and same can fly by means of lift of the fixed wing caused by tilting of the ro...  
WO/2020/141513A2
A VTOL aircraft has both fixed wing and fixed-position multi-rotors. The aerial vehicle is capable of vertical takeoff and landing, forward flight and maneuverability control by using a same set of thrust producing elements. Relative rot...  
WO/2020/141567A1
[Problem] To provide an aircraft that can safely and efficiently transition from hovering to horizontal flight. [Solution] This aircraft comprises: a lift generation part such as a main wing; a thrust generation part that makes it possib...  
WO/2020/139307A1
A flying machine consists of an autonomous flying machine (1) which is connected to a transport device (2) with the aid of coupling means (4) and at least one cable (3) wound by at least one winch (7) on one drum. With the aid of the win...  
WO/2020/136460A1
Convertiplane (1) comprising a fuselage (2); a pair of wings (3, 3'), a pair of nacelles (4) fixed with respect to the wings (3, 3'), and a pair of rotors (5) rotatable about respective second axes (B) and tillable about a third axis (C)...  
WO/2020/128662A1
An aircraft (1) is described that comprises: a fuselage (2) with a first axis (A) of longitudinal extension; and a tail portion (14) arranged at a tail end (13) of the fuselage (2); the tail portion (14) comprises two surfaces (15a, 15b)...  
WO/2020/130333A1
The present invention relates to a vertical take-off and landing type hybrid drone comprising: a pair of front rotary rotors, which are formed on a fixed blade, perform a vertical rotation operation so that vertical taking-off and landin...  
WO/2020/128661A1
A vertical take-off and/or landing aircraft (1) comprising: a fuselage (2) having a longitudinal axis (d); a pair of semi-wings (3) protruding from the fuselage (2) in a transversal direction with respect to the longitudinal axis (D); a ...  
WO/2020/121671A1
A motor-integrated fan 1 including one or more motors integrated therein comprises: a shaft part 11 which serves as a supporting system disposed at the center of a rotational axis; a rotation part 12 which is a rotating system rotating a...  
WO/2020/122056A1
The present invention provides a motor-integrated fan that suctions air through a suction port and blows out the suctioned air through a blow-out port, wherein: the motor-integrated fan comprises a shaft part provided in the center of a ...  

Matches 1 - 50 out of 1,499