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WO/2017/107661A1 |
A flying mowing method and apparatus. The apparatus comprises a mower and an unmanned aerial vehicle, wherein the mower is mounted on the unmanned aerial vehicle. The mowing method comprises the following steps: acquiring a mounting posi...
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WO/2017/096392A1 |
This disclosure generally relates to a method and system for autonomous UAV systems for logistic delivery. The present technology relates techniques that enable an efficient logistic delivery using a UAV in conjunction with an automatic ...
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WO/2017/077144A1 |
The invention relates to an aerodyne with vertical-takeoff-and-landing ability and the ability to generate lift by means of both rotors and fixed wings, which comprises: a fuselage (1); two fixed wings (2); two front (11) and two rear (1...
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WO/2017/072520A1 |
A wing member (14b) for an air vehicle (10), said wing member comprising a core section (20) defining its longitudinal axis and having upper and lower surfaces, at least one of said surfaces comprising apparatus (22) selectively configur...
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WO/2017/072518A1 |
An air vehicle (10) comprising a main body (12) and a pair of opposing wing members (14a, 14b) extending substantially laterally from the main body(12) having a principal axis orthogonal to the longitudinal axis(20) of said wing members,...
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WO/2017/073300A1 |
The objective of the present invention is to make it possible for an underwater image capturing position and direction to be controlled easily and flexibly using a small unmanned aircraft provided with a plurality of rotating blades. Thi...
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WO/2017/072519A1 |
An air vehicle (10) comprising a main body (12)and a pair of opposing wing members (14a, 14b) extending substantially laterally from the main body (12), at least a first propulsion device (16) associated with a first of said wing members...
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WO/2017/072517A1 |
A rotary-wing air vehicle comprising a main body (12) and at least two rotor devices (16a, 16b) arranged and configured to generate propulsion and thrust, in use, to lift and propel said air vehicle, said rotor devices (16a, 16b) being a...
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WO/2017/065102A1 |
Provided is a flying-type inspection device that can use a small unmanned aircraft to perform inspection while controlling angle and distance with respect to a planar inspection target. Also provided is an inspection method. The present ...
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WO/2017/052396A1 |
The object of the invention is a vertical take-off and landing aircraft in the manned or unmanned version powered by one or more electric motors which rotate two contra-rotating, fixed-pitch or variable-pitch propellers located at the fr...
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WO/2017/048336A2 |
A hybrid VTOL/high speed aircraft may comprise systems and functions for in flight configuration changes from high lift helicopter or VTOL mode to fixed or swing-wing high speed aircraft mode to accommodate a variety of functions or miss...
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WO/2017/042354A1 |
A VTOL (vertical take-off and landing) aerial flying vehicle comprising an inner frame, a gimbal system and an outer frame, the inner frame comprising a propulsion system and a control system, the propulsion system being able to generate...
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WO/2017/042291A1 |
The invention relates to a vertical take-off and vertical landing aircraft (1,1b) configured for flying in a first flight mode (200) and a second flight mode (201), wherein the aircraft (1,1b) comprises: -a front section (2) comprising t...
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WO/2017/043980A1 |
A rotor assembly for a multirotor aircraft, and a multirotor aircraft, are disclosed herein. The rotor assembly has a first motor having a first axis of rotation and a first propeller connected to the first motor. The rotor assembly has ...
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WO/2017/044388A1 |
One example embodiment includes a vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV) (12). The VTOL UAV includes a flight control system configured to provide avionic control of the VTOL UAV in a hover mode and in a level-...
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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...
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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...
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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...
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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 ...
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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...
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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...
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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...
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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...
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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)...
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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...
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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, ...
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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...
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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.
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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...
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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 ...
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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 ...
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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...
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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...
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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...
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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...
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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...
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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...
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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)...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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