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Matches 1 - 50 out of 1,153

Document Document Title
WO/2018/106382A1
A lift fan position lock mechanism is disclosed. In various embodiments, a position lock mechanism includes a ring structure having a first surface, the ring structure including one or more detents defined in the first surface of the rin...  
WO/2018/105897A1
The present invention relates to an vertical take-off and landing method and apparatus of an automobile capable of vertically taking off and landing an automobile by using exhaust gas generated during an engine operation of an automobile...  
WO/2018/099856A1
Electrically powered Vertical Take-off and Landing (VTOL) aircraft are presented. Contemplated VTOL aircraft can include one or more electrical energy stores capable of delivering electrical power to one or more electric motors disposed ...  
WO/2018/090790A1
A rotor control mechanism (1) and a dual-rotor blade unmanned aerial vehicle. The rotor control mechanism (1) comprises a rotor blade beam (3), an external rotor blade beam (8), an x-axis motor (10), and an x-axis transmission and reduct...  
WO/2018/091981A1
The invention relates to a vehicle for transporting people and goods, capable of air, land, underwater, sea and river-based travel, capable of taking off and landing vertically and horizontally on a solid and liquid surface without causi...  
WO/2018/078386A1
A lift rotor or 'thrust' system or assembly for a VTOL aircraft, comprising first and second lifting thrusters or rotors contained within a housing, the housing containing a leading edge, a trailing edge, a upper surface and a lower surf...  
WO/2018/078388A1
A vertical take-off and landing aircraft, and a control method for the aircraft, are disclosed. The aircraft has a vertical motion mode and a forward thrust mode. The aircraft comprises an airframe, having a wing section; a forward thrus...  
WO/2018/075414A1
A multicopter aircraft with boom-mounted rotors is disclosed. In various embodiments, a multicopter as disclosed herein includes a fuselage; a port side wing coupled to the fuselage; and a starboard side wing coupled to the fuselage. Eac...  
WO/2018/075413A1
Described embodiments provide a rotor mounting boom assembly for a personal aircraft. The rotor mounting boom assembly includes a rotor mounting boom releasably attachable to a wing of the personal aircraft, one or more vertical lift rot...  
WO/2018/070867A1
An aerial vehicle (50) for vertical take-off and landing and horizontal flight comprises two wings (31, 32) extending substantially parallel to a Y-axis in spanwise direction, substantially parallel to an X-axis in chordwise direction, a...  
WO/2018/067499A1
In some embodiments, systems and methods are provided that limit the change in temperature and/or control a temperature of a product during delivery. Some embodiments provide systems comprising an unmanned delivery vehicle (UDV) comprisi...  
WO/2018/060970A2
An oblique rotor-wing aircraft may be capable of vertical take-off and landing, subsonic cruise, transonic cruise, and/or supersonic cruise. The oblique rotor-wing aircraft may comprise one or more of a fuselage, a rotor-wing, a thrust-v...  
WO/2018/064209A1
In various embodiments, a tilt-wing aircraft includes a fuselage; a first wing tiltably mounted at or near a forward end of the fuselage; and a second wing rotatably mounted to the fuselage at a position aft of the first wing. A first pl...  
WO/2018/063019A1
The present invention relates to a vertical take-off and landing ("VTOL") aircraft and especially to this having hybrid or electric drive, used to transport people or goods from one point to the other without the necessity of airport run...  
WO/2018/057034A1
A UAV includes a fork lift system and a length component. The forklift system includes one or more elongated members extending at least partially in a horizontal direction. The forklift system also includes an extension mechanism configu...  
WO/2018/048574A1
An aircraft includes a fuselage, a forward wing assembly, and aft wing assembly, and a propulsion system. The propulsion system includes a port forward propulsor and a starboard forward propulsor, each of which rotatable between a forwar...  
WO/2018/048645A1
An aircraft includes a fuselage and a wing assembly attached to or formed integrally with the fuselage. The aircraft also includes a propulsion system having a port propulsor and a starboard propulsor. The port and starboard propulsors a...  
WO/2018/048573A1
An aircraft includes a fuselage and a wing assembly attached to or formed integrally with the fuselage. The aircraft also includes a hybrid electric propulsion system having a port propulsor and a starboard propulsor, with the port and s...  
WO/2018/048644A1
An aircraft includes a fuselage, a forward wing assembly, and aft wing assembly, and a propulsion system. The propulsion system includes a first primary thrust propulsor and a first secondary thrust propulsor, the first primary thrust pr...  
WO/2018/048565A1
A method for operating a propulsion system of an aircraft includes moving a plurality of forward and aft propulsors to a vertical thrust position. While in the vertical thrust positions, the method also includes providing a first forward...  
WO/2018/027315A1
A lightweight, pocket-sized unmanned aerial vehicle (UAV) that can be held in an outstretched hand by a user for take-off and landing of the UAV. The UAV comprises a semi-toroidal or a substantially toroidal hollow body that defines a du...  
WO/2018/031075A1
An aircraft includes a wing where a first rotor and a second rotor are coupled to the wing at a fixed position relative to the wing. The aircraft also includes a fuselage and a bearing. The bearing mechanically couples the wing and the f...  
WO/2018/021943A1
The invention relates to the field of aircraft engineering, and more particularly to vertical take-off and landing aircraft. The present aircraft comprises a main bearing frame with a spatial structure, a seat, a cabin, steering members,...  
WO/2018/013529A1
A gearbox includes a housing including a lubricant reservoir, at least one gear system arranged in the housing, at least one lubricant delivery passage operable to direct a flow of lubricant from a lubricant reservoir onto the at least o...  
WO/2018/004626A1
Disclosed herein is a water helicopter includes a fuselage, first and second fixed wings extending outwardly from left and right ends of the fuselage, first and second propellers disposed in a spaced apart configuration on a top surface ...  
WO/2018/000096A1
An aircraft includes a fuselage having an outer surface profile selected to conform to an airfoil profile and at least one engine located within the fuselage. The aircraft further includes a plurality of air intakes distributed over a to...  
WO/2017/209820A2
A vehicle, includes a main body. A fluid generator is coupled to the main body and produces a fluid stream.. At least one fore conduit and at least one tail conduit are fluidly coupled to the generator. First and second fore ejectors are...  
WO/2017/208199A1
A mobile case system is provided. The mobile case system may include a case for a control device and a headset worn by a user. The case may enclose the control device and may include an expandable body, propellers disposed in the expanda...  
WO/2017/210595A3
Systems, devices, and methods for an aircraft having a fuselage (110); a wing (120) extending from both sides of the fuselage; a first pair of motors (132b, 133b) disposed at a first end of the wing; and a second pair of motors (142b, 14...  
WO/2017/209820A3
A vehicle, includes a main body. A fluid generator is coupled to the main body and produces a fluid stream.. At least one fore conduit and at least one tail conduit are fluidly coupled to the generator. First and second fore ejectors are...  
WO/2017/200609A1
The present disclosure pertains to self-piloted, electric vertical takeoff and landing (VTOL) aircraft that are safe, low-noise, and cost-effective to operate for cargo-carrying and passenger-carrying applications over relatively long ra...  
WO/2017/200610A1
The present disclosure pertains to self-piloted, electric vertical takeoff and landing (VTOL) aircraft that are safe, low-noise, and cost-effective to operate for cargo-carrying and passenger-carrying applications over relatively long ra...  
WO/2017/197316A1
An unmanned aerial vehicle includes at least one rotor motor configured to drive at least one propeller to rotate; a passenger compartment sized to contain a human or animal passenger; and a hybrid generator system configured to provide ...  
WO/2017/188699A1
A discharge device according to an embodiment of the present invention comprises: a housing having an inlet for introducing a fluid to a central region thereof, an outlet at an edge thereof, and a stator; a mouth composed of an outer wal...  
WO/2017/189410A1
An unmanned aerial vehicle includes a tubular base structure, a motor having a stator, the stator being connected to the tubular base structure, an energy storage module configured to supply power to the motor, and at least one propeller...  
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/2017/184270A3
A tailsitter aircraft includes one or more rotatable wings. The tailsitter aircraft optionally includes a fuselage from which wing supports extend. Each rotatable wing optionally includes a rotatable wing section having an inboard portio...  
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/2017/184272A3
The present disclosure provides various embodiments of a rotorcraft-assisted launch and retrieval system including a rotorcraft having a fixed-wing aircraft capture assembly configured to capture a fixed-wing aircraft.  
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/2017/176953A1
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...  

Matches 1 - 50 out of 1,153