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Patent Searching and Data


Matches 301 - 350 out of 1,479

Document Document Title
WO/2017/040493A1
The universal vehicle system is designed with a lifting body which is composed of a plurality of interconnected modules which are configured to form an aerodynamically viable contour of the lifting body which including a front central mo...  
WO/2017/035677A1
The invention relates to a machine that travels like a car, takes off like a helicopter and flies like an aeroplane. A prime mover is arranged below the two seats - pilot and copilot - of a two-seater helicopter, moving a vertical gimbal...  
WO/2017/037401A1
The invention relates to a helicopter comprising a structural frame (5), at least one main lift and propulsion rotor (10) secured to said structural frame (5), and a drive train for moving said main rotor (10), comprising a power transmi...  
WO/2017/035503A1
An aircraft includes a fuselage, a wing, a ducted fan and a controller. The wing and the ducted fan are coupled to the fuselage. The controller is operable to control the aircraft in a vertical flight mode, a horizontal flight more, and ...  
WO/2017/030462A1
´╗┐The invention relates to the field of aircraft construction, and more specifically to vertical take-off and landing aircraft. The aircraft includes a bearing frame of a spatial structure, a seat, controls, moto-units, a control system...  
WO/2017/021918A1
The invention concerns a convertible aircraft comprising a fuselage (F), a pair of wings (A1, A2) disposed to either side of the fuselage (F), at least one ducted rotor (1) installed in a horizontal position at one of the ends of the fus...  
WO/2017/021391A1
The invention relates to a VTOL aircraft (1, 10) having a displaceable mass (9) attached to or fitted in the fuselage (7), and at least two pivotable rotors (3). The rotors (3) are arrangeable in a substantially horizontal position and a...  
WO/2017/022209A1
A flying body equipped with: a plurality of rotor units (30) which each have a propeller (32) and a motor (33) driving the propeller (32); a cushioning body which extends across the vertical height of the plurality of rotor units (30) an...  
WO/2017/016096A1
Disclosed are a novel vertical take-off and landing aircraft and a control method therefor. The aircraft comprises an aircraft main body (1), wherein the aircraft main body (1) comprises a fuselage (2), at least one pair of aerofoils (3)...  
WO/2017/014508A1
A vertical take-off and landing aircraft using a hybrid electric propulsion system is disclosed. A hybrid vertical take-off and landing aircraft according to one embodiment comprises: an engine; a generator which generates electric power...  
WO2017010439A1
[Problem] To configure the frame supporting an unmanned aerial vehicle so as to be lightweight and strong. [Solution] An unmanned aerial vehicle 1 is equipped with: an upper frame 10 that is formed by connecting, at intersection points, ...  
WO/2016/133427A4
The invention relates to the field of aviation and cosmonautics, and more particularly to designs for vertical take-off and landing aircraft. The present vertical take-off and landing aircraft comprises jet propulsion units containing co...  
WO/2017/010909A1
The invention relates to the field of aviation, and more particularly to designs for vertical take-off and landing aircraft. The present aircraft comprises an engine (11), which is connected by means of an output shaft (18) to a differen...  
WO/2016/209697A1
Embodiments described herein relate to multicopters with separate engines to power each rotor, wherein the multicopters also include with unique controls to guide the multicopter.  
WO/2016/009376A9
A vertical take-off and landing (VTOL) aircraft is provided comprising a fuselage (12) defining a forward end and an aft end, the fuselage accommodating at least one engine (56), a left wing (18) and a right wing (20) extending from eith...  
WO/2016/200502A2
A manned/unmanned aerial vehicle adapted for vertical takeoff and landing using the same set of engines for takeoff and landing as well as for forward flight. An aerial vehicle which is adapted to takeoff with the wings in a vertical as ...  
WO/2016/153328A3
The present invention relates to SMAs (self-moving apparatuses) which use any type of propulsion means, including, without limitation, an FPGB (propeller-gear block) comprising an FP (propeller) and a drive for supplying power thereto. M...  
WO/2016/193690A1
An aerial device (100) capable of controlled flight has a body (110), a rotor (120) arranged to rotate relative to the body; and a deployable sheet (130), the sheet having an undeployed configuration in which the sheet is folded against ...  
WO/2016/133427A3
The invention relates to the field of aviation and cosmonautics, and more particularly to designs for vertical take-off and landing aircraft. The present vertical take-off and landing aircraft comprises jet propulsion units containing co...  
WO/2016/181044A1
Convertible airplane capable of flying with the speed and economy of use of an airplane and of taking off/landing vertically and of flying/hovering like a helicopter. The craft that forms the subject of the invention takes the appearance...  
WO/2016/153580A3
A flying vehicle with a fuselage having a longitudinal axis, a cockpit extending substantially from the center of the fuselage, a left front wing extending from the fuselage, a right front wing extending from the fuselage, a left rear wi...  
WO/2016/159383A1
This flying body is provided with: a base; multiple frames which are extended from the base; multiple thrusters which are respectively disposed on the multiple frames while arranged in the same plane and which generate thrust forces in t...  
WO/2016/142555A1
The invention relates to a flying motorcycle (100) for transporting people and luggage, which aesthetically resembles a conventional motorcycle and is driven in a similar manner. The lift for the elevation and movement of said motorcycle...  
WO/2016/109003A3
A vertical take-off and landing (VTOL) aircraft is provided. The aircraft includes a wing, nacelles supportively disposed at opposite ends of the wing, proprotors respectively attached to each of the nacelles with each of the proprotors ...  
WO/2016/137362A1
The invention relates to two aircraft forming the fuselage of an aeroplane that flies vertically and horizontally, moves forward and backward, and separates to form two self-contained aircraft while in flight mode. When required, the fus...  
WO/2016/136848A1
Provided is a multicopter with which it is possible to minimize the occurrence of the vortex ring state in rotor blades, and to control lift and thrust efficiently and with a high degree of precision. This multicopter comprises a plurali...  
WO/2016/131127A1
An unmanned aerial vehicle and process for automatically calibrating the unmanned aerial vehicle having at least one magnetic sensor is described. The calibration process involves receiving an internal or external control command to init...  
WO/2016/132040A1
The Aerodyne includes a supporting structure (4), to which are connected: - at least one supporting axial blower (1), attached relative to the supporting structure (4); - at least one main engine (2) for driving the supporting blower (1)...  
WO/2016/120833A1
A tiltrotor (100) comprises a fuselage (110), a couple of wings (120) connected to the fuselage (110) and having a longitudinal axis x, each wing (120) arranged to rotate about longitudinal axis x with respect to the fuselage (110), a co...  
WO/2016/085610A4
This disclosure is generally directed to a High Speed vertical takeoff and landing (VTOL) aircraft that includes fixed wing flight capabilities. The High Speed VTOL aircraft may include at least two thrust producing rotors located equidi...  
WO/2016/118230A1
A flying wing vertical take-off and landing (VTOL) aircraft is provided and includes an empennageless-fuselage from which foldable wings extend outwardly, an empennageless-nacelle supported on each of the wings and a rigid rotor propelle...  
WO/2016/110756A1
Not requiring aileron, elevator, rudder, flap, slat, horizontal and vertical stabilizer and not transferring vibration to the fuselage. In this invention the engine and fuselage (hanging under wing) are the same as those in other airplan...  
WO/2016/092102A1
The disclosure thus relates to a light unmanned vertical takeoff aerial vehicle (1) which comprises at least two fixed coplanar propulsion devices (7) and at least one wing (3) providing the drone (1) with lift. The coplanar propulsion d...  
WO/2016/085610A1
This disclosure is generally directed to a High Speed vertical takeoff and landing (VTOL) aircraft that includes fixed wing flight capabilities. The High Speed VTOL aircraft may include at least two thrust producing rotors located equidi...  
WO/2016/028358A4
The present disclosure relates to a high performance Vertical Takeoff and Landing (VTOL) aircraft for executing hovering flight, forward flight, and transitioning between the two in a stable and efficient manner. The VTOL aircraft provid...  
WO/2016/078622A1
The present invention relates to a combined vertical take-off and landing aircraft. The combined vertical take-off and landing aircraft comprises an aircraft body (2), a rotor/wing (1) which can be switched between a rotor state and a fi...  
WO/2016/068383A1
The present invention discloses an unmanned flying object. The present invention is provided with a base unit, a first actuator, and a propeller which rotates by means of the power of the first actuator, and the present invention compris...  
WO/2016/066848A1
The invention relates to a driving module for a motor vehicle. Said driving module comprises two driving devices with a total of at least three impellers that have rotor blades; at least two of the impellers are coupled to a swiveling me...  
WO/2016/062223A1
The present invention relates to a vertical take-off and landing aircraft, comprising a fuselage (1), a main wing, a main thrust apparatus (2) that can tilt between the horizontal position and the vertical position, a tilt apparatus that...  
WO/2016/062921A1
An electrically powered vertical takeoff and vertical landing (VTOL) aircraft, which comprises at least two main propellers (101a, 101b), wherein the main propellers are adapted to generate at least 70% of the aircraft propulsion. The ai...  
WO/2016/059555A1
An unmanned aerial vehicle (UAV) system provides for UAV deployment and remote, unattended operation with reduced logistics requirements. The system includes a launcher that can include one or more containers, or hangars, configured to h...  
WO/2016/060720A1
The Curtis Protocol, a standardized aircraft control interface, e.g. for aircraft with multiple flight regimes and flight modes, is provided. The Curtis Protocol standardizes the division and selection of aircraft flight regimes and flig...  
WO/2016/058502A1
Disclosed is a tail-sitter aircraft, comprising an aircraft body (1), an aircraft wing (2), an attitude control device and a main thrust device (3) using a heat engine as a power device, wherein the aircraft wing (2) comprises a left hal...  
WO/2016/059040A1
A flying apparatus is provided that comprises a airfoil (1) with a streamlined profile for generating an aerodynamic lift force vector (L) acting on the flying apparatus when being exposed to an apparent air flow. The flying apparatus al...  
WO/2016/028358A3
The present disclosure relates to a high performance Vertical Takeoff and Landing (VTOL) aircraft for executing hovering flight, forward flight, and transitioning between the two in a stable and efficient manner. The VTOL aircraft provid...  
WO/2016/018486A3
A vertical takeoff and landing aircraft includes a pair of ducted lift/thrust fans that are rotatably movable between a first vertical lift position and a second horizontal thrust position. The lift/thrust fans are disposed within curvil...  
WO/2016/047343A1
This vertical take-off and landing aircraft (1) is provided with: a fuselage (2); a plurality of engines (3) that are installed on the fuselage and generate jet streams to produce thrust; an abnormality signal-acquiring unit for acquirin...  
WO/2016/037543A1
A suction-cup-type aircraft comprises a propulsion device (1) and a venting device (9); the venting device (9) actively drives the air above the upper surface of the propulsion device (1) to flow quickly to produce a negative pressure, o...  
WO/2016/003530A3
One example embodiment includes a vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV)(12). The VTOL UAV (12) includes a flight control system configured to provide avionic control of the VTOL UAV (12) in a hover mode and in...  
WO/2016/028358A2
The present disclosure relates to a high performance Vertical Takeoff and Landing (VTOL) aircraft for executing hovering flight, forward flight, and transitioning between the two in a stable and efficient manner. The VTOL aircraft provid...  

Matches 301 - 350 out of 1,479