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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...
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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...
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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 ...
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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...
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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...
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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...
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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...
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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 ...
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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...
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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...
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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...
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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)...
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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...
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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...
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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...
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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...
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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...
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WO/2017/041018A9 |
A vehicle includes a main body and a gas generator producing a gas stream. At least one fore conduit and tail conduit are fluidly coupled to the generator. First and second fore ejectors are fluidly coupled to the at least one fore condu...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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 ...
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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...
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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...
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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...
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WO/2018/027017A1 |
A propulsion system for an aircraft includes an engine (e.g., piston engine, or turbine) having an axis made to be nonparallel with the longitudinal axis of the aircraft. This is enabled using an electrical, hydraulic, or other system to...
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WO/2018/020112A1 |
The invention relates to a cradle (10) for an aircraft turbopropeller engine (12) of a substantially axial orientation, comprising a front arch (16) and a rear arch (18) extending transversely relative to said axial direction (A), said a...
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WO/2018/018634A1 |
A cradle head (100), comprising: a bracket assembly (30), a function module (50), a control board (500) and a connection structure (70); the function module (50) is disposed on the bracket assembly (30); the function module (50) comprise...
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WO/2018/019074A1 |
An escape aircraft in an air crash. Key points of the technical solution of the escape aircraft are as follows: the escape aircraft comprises a fuselage (1) and wings (2) disposed on the left side and the right side of the fuselage, main...
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WO/2018/019152A1 |
A motor mounting base for an electronic speed controller of a multi-rotor plant-protection aircraft, and the motor-mounting base comprising: a mounting base (10) and a connecting tube (20); a motor mounting position (100) is formed at a ...
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WO/2018/014336A1 |
A system for supplying power to an unmanned aerial vehicle (UAV), and methods for making and using same. Heat generated by at least one energy component of the UAV can be converted into electrical power. The electrical power can be suppl...
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WO/2018/011519A1 |
The invention concerns a propulsion device (1) comprising a torque generator (2) driving an output shaft (3) via a power transmission gearbox (4), the output shaft (3) being rotatably coupled to a propeller (5), said power transmission g...
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WO/2018/009260A1 |
A propulsion system for an aircraft is provided having a propulsion engine configured to be mounted to the aircraft. The propulsion engine includes an electric machine defining an electric machine tip speed during operation. The propulsi...
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WO/2018/008675A1 |
Provided are a gas detection system and a gas detection method utilizing a plurality of aerial vehicles, which enable precise detection in a short time. The gas detection system includes: a sending aerial vehicle in which a light-emittin...
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WO/2018/006439A1 |
An integrated power multi-axis unmanned aerial vehicle, which comprises an internal combustion engine, an electric motor, an electricity storage unit, and an electric drive unit. The internal combustion engine is employed to drive an ele...
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