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Patent Searching and Data


Matches 1 - 50 out of 1,345

Document Document Title
WO/2019/217427A1
A request for transport services that identifies a rider, an origin, and a destination is received from a client device. Eligibility of the request to be serviced by a vertical take-off and landing (VTOL) aircraft is determined based on ...  
WO/2019/217920A1
An aircraft including an airframe and a plurality of propulsion assemblies coupled to the airframe, wherein each propulsion assembly includes an electric motor, a propeller coupled to the electric motor, and a tilt mechanism that connect...  
WO/2019/213540A1
A vertical takeoff and landing (VTOL) aircraft, configured to transport passengers and/or cargo, uses propellers during vertical flight and wings during forward flight to generate lift. The VTOL aircraft includes a front wing and a rear ...  
WO/2019/211875A1
The present invention provides an energy efficient VTOL aircraft capable of flying like helicopter as well as fixed wing airplane based on requirement. The propulsion for the aircraft is either all electric or hybrid/electric. The aircra...  
WO/2019/212744A1
Features for an aircraft having efficiently designed propulsive elements are disclosed. The aircraft includes propellers at or near the wingtips that rotate about a rotation axis to provide thrust and also rotate about an axis that is an...  
WO/2019/213315A1
A method for extracting a person or package from a ground point involves dropping a pod, connected to a tether, with parachute and radio from an aircraft, connected by tether line to the fixed-wing aircraft, tracking descent of the pod t...  
WO/2019/210010A1
A propulsion unit includes a motor rotor, a clip-in base mount, a clip-in rotor cap, propeller mounts, and propeller blades. The motor rotor spins about a central rotational axis. The clip-in base mount is disposed on the motor rotor. Th...  
WO/2019/207377A1
A request for transport services that identifies a rider, an origin, and a destination is received from a client device. Eligibility of the request to be serviced by a vertical take-off and landing (VTOL) aircraft is determined based on ...  
WO/2019/210003A1
An aircraft has a boom, a propulsion assembly coupled to a first end of the boom, and a first wing coupled to a second end of the boom. The propulsion assembly is coupled to the boom by a rotating joint. A second wing is optionally coupl...  
WO/2019/210009A1
An aerial vehicle includes an airframe; vertical propulsion units, and a controller. The vertical propulsion units are mounted to the airframe and include propellers oriented to provide vertical propulsion to the aerial vehicle. The vert...  
WO/2019/135791A3
An integrated transportation system with vertical take-off and landing capabilities utilizes multiple common ground, pod, and flight components to facilitate efficient vertiport operations. Automated system operations, enable individuals...  
WO/2019/202325A1
Methods, apparatus, systems and a vertical take-off and landing (VTOL) vehicle are provided. The VTOL vehicle includes: a fuselage having longitudinally a front section, a central section and a rear section; a first lifting surface compr...  
WO/2019/204688A1
A VTOL fixed wing aircraft capable of high-speed forward flight. The aircraft has a main wing internally reinforced with front and aft spars. Spar boxed are located in roll-balanced locations along the wing. Each spar box serves as a con...  
WO/2019/203673A1
A personal flight apparatus with vertical take-off and landing conceived as a biplane apparatus constituted by two distinct parts articulated there between, the first distinct part consisting of the cockpit (1), which is hinged to the se...  
WO/2019/184869A1
A multi-purpose helicopter having a dual compartment structure, an electronic omni-directional rotor assembly, and an application thereof. The helicopter comprises: an upper fuselage, a lower fuselage, and a middle rotor propeller positi...  
WO/2019/191237A1
A propeller-less unmanned aerial vehicle having a body having a plurality of channels, an inlet formed in the body and configured to allow air flow to enter the plurality of channels from an exterior of the body, an anechoic chamber form...  
WO/2019/180304A1
A structure construction (100) for an aircraft (200) comprises first (101) and second (102) fuselage portions and at least one wing (103). In addition the structure construction (100) comprises a supporting structure (104) for supporting...  
WO/2019/172804A1
The invention relates to the field of aviation, particularly to designs for vertical take-off and landing aircraft. A convertiplane comprises a fuselage, a pair of wings (a fore wing and an aft wing), propulsion systems comprising engine...  
WO/2019/173831A1
The present invention relates to a method, system, and apparatus of flight system for individual users using electric ducted fans. The flight system comprises a modular unit, which comprises a plurality of electric ducted fans, means for...  
WO/2019/147196A3
The invention is related to an autonomous unmanned aerial vehicle for land, sea and air use. The invention is more specifically related to an unmanned aerial vehicle which can vertically take off and land, fly with fixed wings (5) and st...  
WO/2019/158793A1
The invention relates to a vertical take-off aircraft that can travel in the air and on land, comprising: a central compartment with seats for accommodating passengers; a perimeter structure that surrounds and closes the compartment and ...  
WO/2019/155173A1
The hybrid propulsion is obtained by arranging, around a conventional turbomachine, a reversible electric machine (23) linked to the low-pressure shaft (7) via a mechanical movement transmission (25), a one-way clutch (29) being arranged...  
WO/2019/154067A1
Disclosed is an active main rotor blade vertical take-off and landing aircraft, at least comprising two main rotor blades. One end of each main rotor blade is connected to a middle connecting piece; the middle connecting piece is connect...  
WO/2019/150128A1
A VTOL aircraft is having four electric fans (3a, 3b, 4a, 4b) distributed around the centre of gravity of the aircraft. Of the four electric fans, two (3a, 3b) are set into openings through the body (1)and two (4a, 4b) are rotatable abou...  
WO/2019/150206A1
A fixed-wing VTOL hybrid UAV is disclosed comprising: a central frame 104; a pair of quick lockable fixed-wings 102 comprising right wing 102-2 and left wing 102-1 that lock with each other over the central frame; and four electrically o...  
WO/2019/145694A1
The disclosure relates to a vertical take-off and landing, VTOL, flying machine. The machine includes a ducted fan having an intake side and an outlet side, at least two co-axial rotors configured to contra-rotate about a fan axis X when...  
WO/2019/148183A1
Systems, devices, and methods for a vertical take-off and landing (VTOL) aerial vehicle (800) having a first GPS antenna (810) and a second GPS antenna (816), where the second GPS antenna is disposed distal from the first GPS antenna; an...  
WO/2019/145704A1
An aircraft comprising a fore thrust means arranged to produce thrust along a first thrust axis, and an aft thrust means arranged to produce thrust along a second thrust axis, wherein the fore thrust means is associated with a fore fixed...  
WO/2019/145584A1
Specially designed for fire fighting, the drone of the invention is in the form of a hexacopter in which the main rotors are distributed according to two parallel alignments of three motors, and the motors are in the form of thermal moto...  
WO/2019/142014A1
The invention relates to electric drones and gliders. The electric drone glider arrangement comprising: a heavy-lift multi-rotor drone with batteries; a manned or unmanned glider; a high voltage generator; an electric cable and rope conn...  
WO/2019/139574A1
Example moveable mounting structures and methods are described. In one implementation, an unmanned aerial vehicle (UAV) includes a body and a moveable mounting structure coupled to the body. The moveable mounting structure can move betwe...  
WO/2019/139559A1
The invention relates to aviation technology, more particularly to aircraft construction, and even more particularly to a cycloidal rotor that can be used to generate lift and to control an aircraft. The present cycloidal rotor comprises...  
WO/2019/135264A1
[Problem] To provide a flying vehicle having both a more basic structure and safety measures in place. [Solution] This flying vehicle comprises: a flying unit that is equipped with a plurality of rotary wings for producing thrust; a leg;...  
WO/2019/130238A1
A convertiplane (1) is described that has a fuselage (2) with a first axis (A), a pair of half-wings (3), and a pair of rotors (5) arranged on mutually opposite ends of the half-wings (3). The rotor (5) comprises a mast (6) hinged on a s...  
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...  
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...  
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...  
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...  
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...  
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....  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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 ...  
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...  

Matches 1 - 50 out of 1,345