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Matches 201 - 250 out of 1,376

Document Document Title
WO/2017/184438A1
An unmanned aircraft includes a forward propulsion system comprising one or more forward thrust engines and one or more corresponding rotors coupled to the forward thrust engines; a vertical propulsion system comprising one or more verti...  
WO/2017/184439A1
An aircraft, such as an unmanned aircraft, can include a forward propulsion system comprising one or more engines and one or more rotors coupled to a corresponding engine; a vertical propulsion system comprising one or more vertical prop...  
WO/2017/184437A1
An unmanned aircraft includes a forward propulsion system comprising one or more forward thrust engines and one or more corresponding rotors coupled to the forward thrust engines; a vertical propulsion system comprising one or more verti...  
WO/2017/184095A1
This invention presents a three-dimensionally and discreetly scalable, modular and customizable aircraft (V) which is composed of stably flyable plurality of planar unitary systems (S) in which each provides a coordinated thrusting vecto...  
WO/2017/180020A1
The present aircraft comprises a body in the form of a disc-like solid of revolution, in which an annular fan wheel is used as a propeller, said fan wheel generating a primary lift, and a counter-rotating airbreathing jet engine. The ann...  
WO/2017/123346A3
A technique is directed to operating an unmanned aerial vehicle (UAV) having a fuselage defining a flight direction of the UAV and wing-plate assemblies that propel the UAV in the flight direction defined by the fuselage. The technique i...  
WO/2017/176953A1
A vehicle includes a propulsion system using one or more impellers as opposed to propellers. The impellers impart circumferential and radial velocity components to the working fluid, which may be air or water. The air is deflected by cou...  
WO/2017/163587A1
A vertical takeoff and landing aircraft 1 according to an embodiment of the present invention includes: a pair of ducted fans 2; a body 3 which is disposed below the ducted fans 2; a frame body 4 which connects the body 3 and the ducted ...  
WO/2017/163200A1
The airplane (1) for civil transports comprising: - a fuselage element (2) adapted to transport persons and/or merchandise; - gliding means (4, 5) associated with the fuselage element (2) to assemble an aircraft body (2, 4, 5) fit for fl...  
WO/2017/158417A1
The present invention, in the field of aviation, is a Vertical Take-Off and Landing (VTOL) vehicle comprising fuselage, verticale tail, four tilting wings, electric generator which uses liquid fuel, rechargeable electric energy storage d...  
WO/2017/153807A1
A convertible rotor aircraft (CRA) able to convert between airplane and helicopter flight modes during flight, comprising: at least one tiltable proprotor assembly (TPA) comprising a proprotor that is titlable to change the axis of rotat...  
WO/2017/155348A1
A vertical take-off and landing aircraft according to one embodiment may comprise: a wing; a power supply unit, disposed in the wing, for supplying power; a control unit, disposed in the wing, for controlling a flight mode; a rotor dispo...  
WO/2017/145622A1
A vertical take-off and landing aircraft 1 is provided with: a pair of ducted fans 3a, 3b that generate a lift force and a thrust force; a frame 4 that connects the ducted fans 3a, 3b to each other; a motive power source 5 that supplies ...  
WO/2017/136906A1
This invention patent is aimed at innovating personal locomotion by free uni-steerable flight with new technologies using clean propulsion energies. The invention is characterised by a new concept of individual aerial locomotion, innovat...  
WO/2017/138902A1
A rotor system comprising hinged stabilizing flaps (6) which compensate for the torque generated by a main rotor of an air vehicle and provide the air vehicle with the rotation around its own axis, the rotor system further comprising def...  
WO/2017/134223A1
The invention relates to a transport means, having an outer element (1, 31, 32, 33, 34, 63) and an inner element (3, 67) arranged within the outer contour of the outer element, wherein the inner element has a drive device having at least...  
WO/2017/129953A1
Wing-in-ground effect vehicle (1) having a lift system with a pressure vessel (2) and a set of nozzles (3-14). The lift system allows the wing-in-ground effect vehicle to take off. The pressure vessel holds a fluid, such as air, under pr...  
WO/2017/121116A1
An engine for vertically taking off or landing with airfoil lift. The engine consists of a fan (1) and a circular-shaped airfoil lifting plate (2). The fan (1) creates airflows from a center to the periphery around the center, and the ai...  
WO/2017/123699A1
A hybrid propulsion aircraft (100) is described having a distributed electric propulsion system. The distributed electric propulsion system includes a turbo shaft engine (112) that drives one or more generators (116) through a gearbox (1...  
WO/2017/112983A1
The present invention belongs to the field of electric-eletronic entertainment devices, and was designed to achieve as its main advantage in comparison with the known prior art devices the possibility to move over any ground, dispensing ...  
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...  
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 ...  
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...  
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...  
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,...  
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...  
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...  
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...  
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 ...  
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...  
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...  
WO/2016/209350A3
A fairing for a landing gear wheel assembly on a tail sitter aircraft is disclosed, which includes a fairing housing defining a longitudinal axis, and at least one pair of laterally opposed aerodynamic tail surfaces extending radially ou...  
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...  
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...  
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 ...  
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-...  
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.  

Matches 201 - 250 out of 1,376