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Patent Searching and Data


Matches 1 - 50 out of 1,253

Document Document Title
WO/2019/074349A1
The invention relates to aviation equipment. An object of this invention is to develop a new non-conventional aerodynamic apparatus that can increase the efficiency of the air flow power use to generate lifting force, control moments and...  
WO/2019/074393A1
The present invention relates to the field of aircraft. The proposed aircraft has the appearance of a "flying saucer" and calls to mind the astronomical phenomenon of the arrangement of the rings of Saturn, wherein the aircraft is capabl...  
WO/2019/068839A1
A control system for a vehicle having means to induce a flow of an ambient fluid. The control system comprises two or more arrays of vanes (130) arranged in proximity to the thrust axis of a means to induce fluid flow. Each array of vane...  
WO/2019/070124A1
Wind power generation system comprising a ground station (32) with an electrical energy generator (34) and an aerodynamic assembly with a wing body (2) having an aerodynamic profile with a major chord, and at least two thrust assemblies ...  
WO/2019/070752A1
An automated flying transport vehicle that capitalizes on the strengths and complexities of a fixed and rotary winged aircraft. The air transport vehicle comprises a body aerodynamically designed to generate lift and a plurality of rotor...  
WO/2019/062257A1
A double lift force ducted vertical take-off and landing aircraft based on a tilt duct, comprising an aircraft body (10), two wings (9), N tilt ducted fans (1, 2), two lift force ducted fans (5, 7), and two duct covers (6, 13), N being a...  
WO/2019/067873A1
A leg mechanism includes an articulated leg system (100), a passive device (130) and a cable (134). The articulated leg system (100) has a leg portion (128). The passive device (130) is coupled to the articulated leg system and is config...  
WO/2019/060933A1
The invention relates to a spokeless and hubless wheel (52) inside which at least one electrically driveable propeller (44) is integrated in such a way that the risks associated with propeller rotation are kept as low as possible. The wh...  
WO/2019/066484A1
The present invention relates to a vertical takeoff and landing aircraft. According to one embodiment of the present invention, the vertical takeoff and landing aircraft comprises: a flight fuselage (F) on which a main wing (3) and auxil...  
WO/2019/056053A1
A vertical take-off and landing (VTOL) aircraft (10) comprises a fuselage (24) first and second forward wings (20, 22) and first and second rearward wings (30, 32), each wing having a fixed leading edge (25, 35) and a trailing control su...  
WO/2019/056172A1
A flight control method for an unmanned aerial vehicle, the unmanned aerial vehicle, and a machine readable storage medium. The method comprises: control, based on a one-button start of a user, a vertical takeoff and landing fixed-wing u...  
WO/2019/056052A1
A vertical take-off and landing (VTOL) aircraft (10) includes a fuselage and first and second forward wings (20, 22), each wing (20, 22) having a fixed leading edge and a trailing control surface (50) which is pivotal about a generally h...  
WO/2018/226172A3
Balancing the drone is difficult with engines (5), when drones are equipped with engine (5) to increase the flight time. However, balancing the drone can be made easy by providing the drone with electric motor (10) or electric motor that...  
WO/2019/040008A1
The operator´s module (1) is wired and/or wirelessly connected to the ground station (2), whereby the operator´s module (1) also consists of semi-transparent glasses (1a) fitted with sensors to scan the operator´s control gestures, mo...  
WO/2019/034765A1
The invention relates to a vertical takeoff aircraft (1), preferably an unmanned aerial vehicle (UAV), drone and/or unmanned aerial system (UAS), comprising: a rigid wing (5) which is oriented substantially horizontally both when hoverin...  
WO/2019/036011A1
A vertical takeoff and landing (VTOL) aircraft is configured with a front set of propellers mounted to a front wing and an aft set of propellers mounted to an aft wing wherein the propellers may be repositioned by rotating them around a ...  
WO/2019/035378A1
A spacecraft (100) includes a principal airframe (6), a parachute (1), which is an air brake structure, and a jetting nozzle (5). The air brake structure is provided farther on one side in a traveling direction with respect to the princi...  
WO/2019/032167A1
Various embodiments include a drone having a landing control device that is configured to rotate wings into an auto-rotation descent configuration causing the drone to enter a nose-down attitude and spin about a long axis of the drone, a...  
WO/2019/033080A1
An intentional fluid manipulation apparatus assembly with a first thrust apparatus that imparts a first induced velocity to a local free stream flow during a nominal operation requirement. The first thrust apparatus creates a streamtube....  
WO/2019/026079A1
A hybrid aerial vehicle (HAV) comprising: a fuselage of the HAV; a first mechanism within the fuselage for accepting a plurality of wings of the HAV, the first mechanism allowing coordinated contraction of the plurality of wings essentia...  
WO/2019/026200A1
In vertical take-off and landing aircraft in which ducted fans are compactly arranged such that there is one on each of the front and rear of the fuselage, since the thrust generation surface is smaller in the lateral direction than in t...  
WO/2019/022618A1
A shroud for an aircraft configured to at least partially surround a noise source including a propeller. The shroud includes an outer layer and two or more sound absorbing materials located inside the shroud. The outer layer is configure...  
WO/2019/021521A1
Provided is a hovering vehicle capable of safely moving while hovering off the ground. This hovering vehicle 1 comprises: six or more impellers 37 arranged below an operator's cab 10 for blasting air drawn in through an air intake space ...  
WO/2019/017833A1
An aerial vehicle including a first wing structure and a second wing structure which intersects the first wing structure perpendicularly at a position offset from a midpoint of a transverse axis of the first wing structure in a direction...  
WO/2019/014386A1
A system for enhancing the thrust produced by an aircraft propulsion element having a propulsion fluid outlet includes a shroud element having an inlet, an outlet and a diffusing section positioned between the shroud element inlet and sh...  
WO/2019/010554A1
Remotely piloted aircraft provided with parts and components that enable use in different configurations, including a fixed-wing configuration, a fixed-wing VTOL configuration and a multi-rotor configuration, said remotely piloted aircra...  
WO/2019/006469A1
An electric aircraft has a fault-tolerant electrical system designed to optimize competing concerns related to cost, performance, and safety. An electrical system in accordance with some embodiments of the present disclosure has a plural...  
WO/2019/006469A8
An electric aircraft has a fault-tolerant electrical system designed to optimize competing concerns related to cost, performance, and safety. An electrical system in accordance with some embodiments of the present disclosure has a plural...  
WO/2018/236448A3
A precision delivery vehicle having a vehicle body assembly, a fixed wing system, a rotor system and a guidance system. The vehicle body assembly can retain a payload. The fixed wing system includes first and second wings coupled to the ...  
WO/2018/232429A1
The invention relates to a protective propeller frame, in the interior of which at least one electrically driven propeller (12) is integrated and a protective device (9, 10, 16) of which surrounds the propeller to such a degree that the ...  
WO/2018/232430A1
The invention relates to a protective propeller frame, in the interior of which at least one electrically driven propeller (12) is integrated and a protective device (9, 10, 16) of which surrounds the propeller to such a degree that the ...  
WO/2018/236295A1
Making drones travel greater distances and stay in mid-air for longer time periods, by making them use the wings at their horizontal movements enabled by developing drones with foldable wings to consume less energy, which can depart from...  
WO/2018/230552A1
An assist system (10A) comprises: a detection unit (12) mounted in an aircraft capable of hovering, the detection unit (12) being provided on the outside of the fuselage (31), and detecting objects that could be obstacles; imaging units ...  
WO/2018/226172A2
Balancing the drone is difficult with engines (5), when drones are equipped with engine (5) to increase the flight time. However, balancing the drone can be made easy by providing the drone with electric motor (10) or electric motor that...  
WO/2018/224567A1
The invention relates to a control method for controlling a yaw angle γ z and a roll angle γ x of an aircraft (1) that takes off vertically, said aircraft having at least two drive groups (3) arranged in opposite side regions of the ai...  
WO/2018/223089A2
Systems and methods are contemplated for favorably improving flight dynamics of aircraft, including enhanced aerodynamic braking and improved flight maneuverability. Air braking systems selectively position a first set of blades at a neg...  
WO/2018/222844A1
A vertical take-off and landing (VTOL) rotary aircraft or helicopter (10) has eight propellers (42) in a quad propeller arm (34) configuration where each propeller arm (34) has two counter-rotating propellers (42). Folding propeller arms...  
WO/2018/222388A1
We describe an aircraft design, which is capable of vertical takeoff and landing and also high-speed cruise on a fixed wing. The aircraft comprises a fuselage with a probe-deployment mechanism, which deploys a sample-gathering probe, loc...  
WO/2018/223089A3
Systems and methods are contemplated for favorably improving flight dynamics of aircraft, including enhanced aerodynamic braking and improved flight maneuverability. Air braking systems selectively position a first set of blades at a neg...  
WO/2018/217667A1
Apparatus, systems, and methods are contemplated for electric powered vertical takeoff and landing (eVTOL) aircraft. Such are craft are engineered to carry safely carry at least 500 pounds (approx. 227 kg) using a few (e.g., 2-4) rotors,...  
WO/2018/211386A1
The present invention relates to an unmanned aerial vehicle with the capacity for vertical take-off and landing, which is provided with hybrid propulsion and lift systems, capable of simultaneously integrating the functionalities of an u...  
WO/2018/211279A1
The present invention provides a propulsion system for an aircraft. The system includes one or more thrust producing portions, wherein the one or more thrust producing portions include one or more duct means (8). The duct means are at le...  
WO/2018/208596A1
A multi-copter lift body aircraft has a lift body that has a first airfoil shape on a front to rear cross-section. The lift body has a nose and a tail. A multi-copter propeller is attached to the lift body. The multi-copter propellers pr...  
WO/2018/208220A1
An aerial vehicle may include a first wing structure. The aerial vehicle may further include a first propeller and a second propeller disposed along the first wing structure. The aerial vehicle may further include a second wing structure...  
WO/2018/208652A1
An aircraft includes a fuselage module (104) and at least two vertical lift rotor modules (300) supporting at least four rotor assemblies (302). Each rotor assembly (302) is supported by a rotor boom (308) having at least one boom free e...  
WO/2018/203036A1
An unmanned aerial vehicle (2) comprising: a fixed wing (6); a pair of nacelles (10) connected to the wing (6) and spaced laterally either side of a centreline of the wing (6), wherein each nacelle (10) comprises a stationary portion (14...  
WO/2018/204134A1
A power conversion unit may include two or more power modules for providing high- voltage direct current power to electrical loads, such as one or more propulsion motors aboard an aerial vehicle. Each of the power modules may be controll...  
WO/2018/197772A1
The aircraft (10) comprises a fuselage (11) and a rhombohedral wing structure (12) comprising front wings (13, 14) mounted on a front wing-root support (17) and rear wings (15, 16) mounted on a rear wing-root support (18). At least two w...  
WO/2018/200879A1
An electric tail-sitter aircraft configured to transport passengers and/or cargo between locations. The aircraft includes a flight module, a ground module and a payload module. The flight module is a wing that can rotate with respect to ...  
WO/2018/194214A1
A fixed-wing drone using a variable pitch propeller, according to an embodiment of the present invention, comprises: a body section formed in a lengthwise direction from a front end to a rear end; wing sections formed on both sides of th...  

Matches 1 - 50 out of 1,253