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Matches 1 - 50 out of 1,716

Document Document Title
WO/2018/188188A1
An upper cover (100) of an unmanned aerial vehicle, mounted on a body (200) of the unmanned aerial vehicle. The body (200) is provided with a first positioning member (202) and a plurality of first clipping members (204). The upper cover...  
WO/2018/184095A1
A battery-powered aerial vehicle has a central controller, one or more propelling modules, and one or more battery assemblies for powering at least the one or more propelling modules. The battery assemblies are at a distance away from th...  
WO/2018/184291A1
A blade (100) for use in a propeller (300). At where the distance on the blade (100) to the center of gyration of the propeller (300) is 58.33% of the radius of gyration of the propeller (300), the angle of attack of the blade (100) is 1...  
WO/2018/175037A1
Electrically operated propellant thrust assist supplements an airplane's takeoff, landing or inflight maneuvers. Unlike conventional SRM propellants, the burn rate of the electrically operated propellant can be varied via an electrical i...  
WO/2018/165498A1
An unmanned aerial vehicle includes at least one rotor motor configured to drive at least one propeller to rotate; and a micro hybrid generator system configured to provide power to the at least one rotor motor. The micro hybrid generato...  
WO/2018/164170A1
Provided is an ornithopter that does not require additional devices such as a tail or rudder, in which each of the lead/lag angles of the left and right wings is changed nonsymmetrically, rotational moment is generated from the differenc...  
WO/2018/165057A1
An aircraft can include a frame and a plurality of electrical rotors coupled to the frame. The aircraft can further include a control system physically coupled to the frame and communicatively coupled with each of the plurality of electr...  
WO/2018/156165A1
An apparatus configured to reduce acoustic interactions between a propeller and a surface of an aircraft positioned downstream of the propeller includes a surface modification element of the surface of the aircraft. The surface modificat...  
WO/2018/156972A1
A safety system for an aerial vehicle, preferably including: a ballistic subsystem, preferably including one or more rockets operable to adjust motion of the aerial vehicle and a mounting unit that couples the ballistic subsystem to the ...  
WO/2018/146422A1
The invention relates to a method for controlling the speed and the power of a turbine engine propeller, wherein at least two operating modes are implemented: - one operating mode, called "speed mode", in which the pitch (β) of the prop...  
WO/2018/148636A1
An unmanned aerial vehicle includes an atmospheric sensor configured to measure an atmospheric condition. The unmanned aerial vehicle includes a rotor motor configured to drive rotation of a propeller of the unmanned aerial vehicle. The ...  
WO/2018/142058A1
Clevis (100), particularly for a turbomachine, comprising a body (102) comprising means (104) of attachment to a casing (105) and at least one aperture (106) for fitting a hinge pin, characterised in that said body is formed in one piece...  
WO/2018/144476A1
An aircraft includes a fuselage having an upper surface and a lower surface and a plurality of planetary modules housed in the fuselage, an individual planetary module having a first jet engine directed outward of the upper surface of th...  
WO/2018/133511A1
The present invention relates to the technical field of unmanned vehicles. Provided is a hybrid-powered unmanned vehicle. The vehicle comprises: a fuel-combusting generator (10), a permanent magnet brushless DC motor (20), a chargeable b...  
WO/2018/126536A1
Disclosed is a motor (100). The motor (100) comprises a motor body (10), a cover (40), a base (60), and an electronic speed controller (80). The motor body (10) comprises a mount (12), a stator (14) fixed on the mount (12), and a rotor (...  
WO/2018/127603A1
The invention relates to a transport carrier system (1), having at least one elongate take-off and landing ramp (2) and at least one flying object (3), which is designed to take off and land on the take-off and landing ramp (2), wherein ...  
WO/2018/121804A1
An electric drive system of a gyroplane (28) comprising a support rotor (11), a primary engine (7) connected with a pusher propeller (8) for movement in air, and an electric motor (1) for movement on road, wherein the primary engine (7) ...  
WO/2018/122297A1
The invention relates to an electrical drive system for an aircraft. The drive system has electrical components which are operated at relatively high operating voltages. In order to compensate for negative effects of Paschen's law on the...  
WO/2018/120001A1
A power device, comprising a motor (1) and a propeller (2); the motor (1) is used for driving the propeller (2) to rotate; the motor (1) has a hollow cavity (11) that is open at two ends; the hollow cavity (11) extends from the top of th...  
WO/2018/116083A1
An assembly for connecting an engine to an aircraft, including a first support configured to be structurally connected to the engine, a second support configured to be structurally connected to the aircraft, and a thrust link. The thrust...  
WO/2018/108834A1
A propulsion system for a vehicle (10) includes a propulsor (102) for generating a thrust for the vehicle, a motor (104) operable with the propulsor for driving the propulsor, a motor mount (164) for mounting the motor in or to the vehic...  
WO/2018/110650A1
A moving body (2) is provided with a main body (21), a propulsion engine (22), and an energy supply unit (3). The propulsion engine (22) propels the main body (21). The energy supply unit (3) supplies energy to the propulsion engine (22)...  
WO/2018/110088A1
An unmanned aircraft 1 according to one embodiment of the present invention is able to properly make an emergency landing in case of an abnormality. The unmanned aircraft 1 is configured as a multicopter which flies with the lift and thr...  
WO/2018/103203A1
Disclosed is a ducted unmanned aerial vehicle, comprising: an aerial vehicle body (9), a first duct (1), a second duct (2), a third duct (3), a fourth duct (4), a front landing gear, and a rear landing gear. The first duct (1) is connect...  
WO/2018/106331A1
An electric machine is provided which includes a rotor disk extending along a radial direction and having a rotor flange attached to or formed integrally with the rotor disk and extending substantially along the axial direction. A plural...  
WO/2018/106359A1
An aircraft has a gas turbine engine including a compressor section that includes at least one compressor bleed. An environmental control system has an air input configured to receive pressurized cabin air. An intercooler has an input an...  
WO/2018/102913A1
An unmanned aerial vehicle ("UAV") is provided for the lifting and carrying payloads of up to 100 kg. The UAV can include a pair of counter-rotating propellers enclosed in a cage with attitude control motors for providing directional thr...  
WO/2018/103576A1
Disclosed is an unmanned aerial vehicle, comprising: a fuselage (11); a battery accommodating cavity (12) provided on the fuselage (11); a battery pack comprising at least two battery blocks, the battery pack being mounted in the battery...  
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/2018/101614A1
A drone according to one embodiment includes: a body frame; an internal combustion engine mounted on the body frame; a plurality of injection ports formed so as to be arranged at intervals along the edge of the body frame, and injecting ...  
WO/2018/099377A1
An aircraft, and over-voltage protection method and device for an electronic governor thereof. An electronic governor is used to control a motor. The method comprises the following steps: acquiring a direct current busbar voltage of an e...  
WO/2018/097359A1
The present technique relates to a drone and, more specifically, to a drone which flies by jetting compressed gas. According to one embodiment, a turbojet drone is disclosed. The turbojet drone comprises an engine part for intaking and d...  
WO/2018/094792A1
A battery housing (100), a battery (102), and an unmanned aerial vehicle. The battery housing (100) is used for the battery (102). The battery housing (100) comprises an outer housing (10) and damping elements (20). Edge portions (11) an...  
WO/2018/093552A1
An electric machine is provided which includes a rotor disk extending along a radial direction and having a rotor flange attached to or formed integrally with the rotor disk and extending substantially along the axial direction. A plural...  
WO/2018/086202A1
An unmanned aerial vehicle battery compartment (100), and unmanned aerial vehicle (200) having the unmanned aerial vehicle battery compartment (100). The unmanned aerial vehicle battery compartment (100) is used to accommodate an unmanne...  
WO/2018/086132A1
A detection device (100) and an unmanned aerial vehicle (200). The detection device (100) comprises a battery (10), a battery mounting base (20), a circuit (70), and a sliding member (30). The battery (10) is provided with at least one g...  
WO/2018/086227A1
An unmanned aerial vehicle (100), comprising a fuselage (1) and a powered component (7). The fuselage (1) is provided with a battery compartment (22) configured to accommodate a battery (2). The battery compartment (22) is provided with ...  
WO/2018/087213A1
The present invention relates to an aircraft (100) comprising: a fuselage (101) comprising a plurality of panels (105) adapted to define an aerodynamic shape for a cockpit or a cargo hold of the aircraft (100);at least one wing (103) str...  
WO/2018/089934A1
Commercial supersonic aircraft and associated systems and methods. A representative commercial supersonic aircraft includes a fuselage configured to carry a crew and between 20 and 60 passengers, a delta wing mounted to the fuselage, and...  
WO/2018/084261A1
A vertical take-off and landing aircraft equipped with: an airframe main section; a frame (11) which defines a quadrant center inside the airframe main section in a planar pattern, and supports the airframe main section so as to generate...  
WO/2018/081904A1
An aircraft comprising a hydrogen-containing envelope, a water-collection system for collecting water from the envelope, an electrolyser to convert the water collected using the water-collection system into hydrogen, and a hydrogen-reple...  
WO/2018/083942A1
[Problem] To provide a framework by which the safety of an autonomous mobile device in an emergency situation can be further improved. [Solution] A circuit provided with: a notification unit for notifying a base station of operable time ...  
WO/2018/083839A1
A vertical take-off and landing aircraft equipped with: an airframe main section; a frame which defines a quadrant center inside the airframe main section in a planar pattern, and supports the airframe main section so as to generate inde...  
WO/2018/079290A1
This flying device comprises: a plurality of rotary blades; an electric motor element which is a drive source for each of the plurality of rotary blades and which rotatably drives a main shaft of the rotary blades; and a drive circuit. T...  
WO/2018/076149A1
Disclosed is a flight control method for a multi-rotor aircraft (10). The multi-rotor aircraft (10) comprises a plurality of rotor assemblies (11-14), wherein each of the rotor assemblies (11-14) comprises an electric motor (111, 121, 13...  
WO/2018/076535A1
A battery compartment (32), a battery compartment assembly (30), and an unmanned aerial vehicle (100). The battery compartment (32) comprises a body (34) provided with an installation cavity, and multiple groups of installation arms (36)...  
WO/2018/076047A1
A hybrid aircraft comprises at least three independent electric motors each arranged to drive a respective rotor; and an internal combustion engine arranged to drive at least two rotor, which are preferably horizontally spaced apart. The...  
WO/2018/072693A1
A method for controlling an aerial vehicle comprises: obtaining flight control information for controlling the flight of an aerial vehicle; and determining a control signal of at least one motor according to the flight control informatio...  
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/2018/068979A1
The invention relates to a drive system (9) for a vehicle, in particular an airplane (1), comprising the following components: - an internal combustion engine (15) for converting chemical energy stored in a liquid fuel (12) into mechanic...  

Matches 1 - 50 out of 1,716