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Matches 1 - 50 out of 1,632

Document Document Title
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...  
WO/2018/066753A1
An unmanned aerial vehicle and an automatic charging device for the unmanned aerial vehicle are disclosed. In one embodiment, the unmanned aerial vehicle comprises a main body and a connection part. The main body includes: a battery; and...  
WO/2018/061823A1
An example of a control system shown in the present disclosure is a multi-copter control system provided with a plurality of motors for rotating a propeller, and a control unit for reading drive information of the motors, wherein said co...  
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/2018/058771A1
Disclosed are a battery clamping mechanism (100), a battery (200) and an unmanned aerial vehicle (300), and a charging device (400), wherein the battery clamping mechanism (100) comprises: a metallic elastic piece (110) and a plastic fas...  
WO/2018/057241A1
An aircraft is provided including a boundary layer ingestion fan mounted to an aft end of a fuselage. A stabilizer is mounted to the fuselage and extends between a root portion and a tip portion to define a span-wise length and extends b...  
WO/2018/057230A1
An aircraft is provided including a fuselage that extends along a longitudinal direction between a forward end and an aft end. A boundary layer ingestion fan is mounted to the fuselage at the aft end and is configured for ingesting bound...  
WO/2018/057229A1
An air injection assembly for an aircraft is provided. The aircraft includes a fuselage extending between a forward end and an aft end along a longitudinal direction and a boundary layer ingestion fan mounted to the fuselage at the aft e...  
WO/2018/054483A1
The invention relates to an aircraft turbine having counter-rotating propellers and a primary drive, the noise development of which is significantly reduced with respect to aircraft turbines which have a primary drive based on the intern...  
WO/2018/053873A1
An electronic governor (100, 100a), comprising an upper metal casing member (11); a lower metal casing member (12) engaged with the upper metal casing member (11) to form one casing (1); a control circuit board (5) mounted within the cas...  
WO/2018/057242A1
An aircraft is provided including a fuselage that extends along a longitudinal direction between a forward end and an aft end. A stabilizer assembly and a boundary layer ingestion fan is mounted to the fuselage at the aft end and is conf...  
WO/2018/045806A1
The present invention relates to a motor speed adjustment system for a multi-rotor aerial vehicle, and a multi-rotor aerial vehicle. The motor speed adjustment system comprises a flight control unit, and further comprises a motor speed a...  
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/2018/048565A1
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/2018/049163A1
A charging system for drones has a base structure connected to a power grid, a connector extendable from the base structure and ending in a charging interface compatible with a charging port of a drone, and a computerized controller at t...  
WO/2018/042676A1
The purpose of the present invention is to make the flight time of an unmanned flying body longer. This unmanned flying body comprises: a plurality of rotary blades; a plurality of control devices connected to the rotary blades; and a fl...  
WO/2018/038992A1
A gas turbine engine includes a compressor section and a turbine section together defining a core air flowpath. The rotary component is rotatable with the compressor section and the turbine section. The gas turbine engine additionally in...  
WO/2018/038909A1
An air intake system includes an exterior housing for a vehicle, the exterior housing including an outer surface including a recessed portion defined therein. The recessed portion includes an angled bottom member having a first end and a...  
WO/2018/039222A1
A propulsion system includes an electric propulsor and a gas turbine engine. The propulsion system also includes an electric machine coupled to a rotary component of the gas turbine engine generating a voltage at a baseline voltage magni...  
WO/2018/035206A1
A propulsion system for an aircraft includes a gas turbine engine and an electric propulsion engine defining a central axis. The electric propulsion engine includes an electric motor and a fan rotatable about the central axis of the elec...  
WO/2018/034295A1
Provided are a device for communicating with and controlling a small unmanned airplane, and a method therefor. In an information processing system to which the present invention is applied, a drone 2 is provided with: a converter module ...  
WO/2018/031548A1
Engine mounting systems and methods that reduce engine core bending provide a first forward mount (130) connectable to a forward part of an engine core of an aircraft, an aft mount (150) connectable to an aft part of the core, and in a v...  
WO/2018/029227A1
The invention relates to the supply of a helicopter training device with electrical energy. The helicopter training device comprises a rotatable rotor which is driven by a local electric motor. The electric motor is supplied with electri...  
WO/2018/027002A1
An aircraft where an engine creates mechanical energy. That energy is then converted into another transmittable form, e.g., electrical using a generator, or hydraulic using a pump, and is delivered to remotely-located motors and thruster...  

Matches 1 - 50 out of 1,632