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WO/2020/210800A1 |
An aircraft engine mounting system to retrofit an aircraft engine from one aircraft type to another in a manner suitable for approved flight. The system includes a circular member having longitudinal securement members extending therefro...
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WO/2020/201639A1 |
The invention relates to a hybrid propulsion unit (100) for an aircraft with multi-rotor rotary wings: an electrical generator (114) driven by an internal combustion engine (112), a rectifier (116) configured to convert an AC current sen...
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WO/2020/200853A1 |
A method for controlling a non-propulsive power generation turbine engine (T) configured to supply power to a plurality of propulsion rotors (R1-R4) of an aircraft, each propulsion rotor (R1-R4) being connected to a power distribution mo...
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WO/2020/195004A1 |
A motor according to an aspect of the present invention is provided with: a rotor rotatable about a center axis; a stator radially facing the rotor with a gap therebetween; and a stator holding member that holds the stator. The stator ho...
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WO/2020/187345A1 |
The invention relates to an aircraft (3) having at least one wing (32) on which an aircraft propulsion device is arranged which has at least one heat engine (I), in particular a gas turbine (10), and an exhaust gas passage (21) for guidi...
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WO/2020/190382A1 |
In an embodiment, one or more computer-readable storage medium comprising a plurality of instructions to cause an apparatus, in response to execution by one or more processors of the apparatus, to receive sounds emanating from one or mor...
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WO/2020/189493A1 |
A wind information storage unit 101 acquires and stores wind information indicating the wind speed and wind direction of wind blowing at a plurality of locations near a facility being inspected. A wind prediction unit 102 predicts, on th...
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WO/2020/190344A2 |
A hybrid propulsion system includes a heat engine configured to drive a heat engine shaft An electric motor is configured to drive an electric motor shaft. A transmission system includes at least one gearbox. The transmission system is c...
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WO/2020/184934A1 |
A vertical take-off and landing aircraft using a hybrid electric propulsion system, according to an embodiment of the present invention, includes: a first control step (S1) of changing a destination when an engine (10), a power generator...
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WO/2020/180376A2 |
An aircraft includes a fuselage defining a longitudinal axis between a forward end and a aft end. At least one airfoil is laterally extending from the fuselage defining an airfoil axis. An electrical system has an electric storage. The e...
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WO/2020/180380A1 |
A hybrid propulsion system includes a heat engine configured to drive a heat engine shaft. An electric motor is configured to drive a motor shaft. A transmission system includes at least one gear box. The transmission system is configure...
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WO/2020/180370A1 |
An aircraft propulsion system having dual powerplants is disclosed that includes a combustion powerplant on one wing of the aircraft and a hybrid-electric powerplant on the other wing of the aircraft, wherein the combustion powerplant in...
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WO/2020/180377A1 |
A cooling system for an engine of an aircraft of a having hybrid-electric propulsion system including a nacelle body including a bottom cooling air intake disposed below a propeller hub for supplying air to an oil-air cooler, wherein the...
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WO/2020/180366A1 |
A hybrid propulsion system includes a heat engine configured to drive a heat engine shaft. An electric motor configured to drive a motor shaft. A transmission system is connected to receive rotational input power from each of the heat en...
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WO/2020/180375A1 |
A power plant a for an aircraft having a hybrid-electric propulsion system including a nacelle body including therein an electric motor directly connected to a gearbox for driving a propeller, wherein the gearbox is connected directly to...
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WO/2020/180374A1 |
An aircraft propulsion system is disclosed that includes at least one hybrid-electric powerplant for delivering power to an air mover for propelling the aircraft, wherein the at least one hybrid-electric powerplant includes a heat engine...
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WO/2020/180367A1 |
A hybrid electric engine control module (ECU) configured to be operatively connected to a hybrid electric aircraft powerplant having a heat engine system and an electric motor system to control a torque output from each of the heat engin...
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WO/2020/180368A2 |
An aircraft includes a fuselage defining a longitudinal axis between a forward end and an aft end. The aircraft includes an electrical system having an electric storage. The electric storage is positioned within the fuselage.
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WO/2020/180371A2 |
An electrical power system is disclosed for an aircraft having a hybrid-electric propulsion system, which includes a battery assembly for storing energy, an electric motor controller operatively connected to the battery assembly for cond...
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WO/2020/180381A1 |
An indicator for a hybrid electric powerplant for an aircraft can be configured to indicate at least an amount or percentage of a total power and/or total torque, and an amount or percentage of an electric motor power and/or electric mot...
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WO/2020/174165A1 |
Disclosed is a hybrid/electric propulsion architecture (100) for a multi-rotor rotary wing aircraft, comprising: an electricity generator (114) driven by an internal combustion engine (112), and configured to operate in motor mode, a rec...
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WO/2020/169497A1 |
The invention relates to an electric propulsion unit (P) for an aircraft comprising at least one first propulsion member (1), a second propulsion member (2) and a single electric motor (6) configured to drive the first propulsion member ...
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WO/2020/166250A1 |
A motor-integrated fan having an intake port and a blow-out port comprises a rotary part 12 that is rotatably supported by a shaft, and a motor 14 that rotates the rotary part 12. The motor 14 is an outer periphery drive motor that rotat...
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WO/2020/166337A1 |
This electric actuator device for a flying object comprises: an inner rotor motor that is mounted on the flying object and generates thrust for the flying object; a motor driver that supplies a drive signal to the inner rotor motor; a fl...
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WO/2020/162584A1 |
The present invention provides a drone system for safely and efficiently carrying out a task using a plurality of drones. Specifically provided is a drone system 500 containing at least a plurality of drones 100 which carry out a task by...
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WO/2020/155459A1 |
A method for flying on Mars, using the medium of the surface of Mars and a medium acceleration unit; the medium acceleration unit operates under the action of electricity to deliver medium to the medium acceleration unit, and the medium ...
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WO/2020/158361A1 |
This motor-integrated fan has a suction port and a blowing port, and is provided with: a rotating part rotatably supported on a shaft part; and a motor that rotates the rotating part. The motor is a peripheral drive motor that rotates th...
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WO/2020/152613A1 |
An electrical drive system for an electrically driven aircraft comprising:a power source (130);at least one motor (110);a main motor controller (222A) using at least one sensor (115) for controlling said at least one motor based on param...
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WO/2020/153373A1 |
[Problem] To make it possible, in a system for managing the process for charging a drone battery, to efficiently charge the drone even when the amount of stored power in the battery of the drone becomes depleted while the drone is workin...
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WO/2020/153316A1 |
[Problem] To make it possible, in a system for managing the process for charging a drone battery, to efficiently charge the drone even when the amount of stored power in the battery of the drone becomes depleted while the drone is workin...
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WO/2020/149495A1 |
A jet engine according to an embodiment of the present invention has four lift nozzles and one main nozzle for vertical takeoff and landing. Therefore, cruising, vertical takeoff and landing, transition flight and the like of an aircraft...
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WO/2020/145820A1 |
A liquid propelled unmanned aerial vehicle (1) comprises a carrier (2) and a nozzle assembly (3) mounted to the carrier (2). The nozzle assembly (3) comprises a nozzle (4) adapted to eject a liquid propulsion jet (5), and a liquid inlet ...
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WO/2020/145488A1 |
According to one embodiment of the present invention, disclosed is a system for detecting defect of a solar panel, comprising: a central server for receiving sensing data of a plurality of solar panels from a sensor provided in relation ...
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WO/2020/142332A1 |
Technologies are described herein for a drag recovery scheme. In various examples, a recovery engine is placed within a vortex flow of air caused by the impingement of air upon a nacelle of a main engine. The propeller of the recovery en...
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WO/2020/141053A1 |
The invention provides a circuit arrangement (1) and comprises: a first cooling body (10) having at least one first cooling channel (101) which is at least partially open at the top; at least one electrical power module (12) arranged in ...
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WO/2020/137105A1 |
In a flying object (10), a PCU (32) has a plurality of operation modes in which an engine (16) and/or a motor generator (18) is used as a driving source for a pusher propeller (12). In accordance with the state of the flying object (10),...
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WO/2020/135637A1 |
A logistics unmanned aerial vehicle comprises a fuselage (1) and four rotary blade shafts (2) extending through the fuselage (1) and arranged in a criss cross fashion. Two ends of the rotary blade shaft (2) respectively extend out of the...
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WO/2020/136424A2 |
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WO/2020/135793A1 |
Provided is an aerial vehicle, comprising: a fuselage (1), comprising an accommodating cavity with an opening; a motor assembly, comprising a motor (2) with an opening installed in the accommodating cavity and a rotor (5) connected to th...
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WO/2020/136425A2 |
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WO/2020/137104A1 |
In a flying object (10), a PCU (32) has a plurality of operation modes in which an engine (16) and/or a motor generator (18) is used as a driving source for a pusher propeller (12). In accordance with the state of the flying object (10),...
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WO/2020/137103A1 |
In a flying object (10), a PCU (32) has a plurality of operation modes in which at least one of an engine (16), a first motor generator (17), and a second motor generator (19) is used as a driving source for a pusher propeller (12). In a...
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WO/2020/130333A1 |
The present invention relates to a vertical take-off and landing type hybrid drone comprising: a pair of front rotary rotors, which are formed on a fixed blade, perform a vertical rotation operation so that vertical taking-off and landin...
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WO/2020/129344A1 |
The purpose of the present invention is to provide a cable used to at least moor a moving body to be moored and supply power thereto, such that weight of the whole cable can be reduced. This cable (1) is a cable used to at least connect ...
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WO/2020/121671A1 |
A motor-integrated fan 1 including one or more motors integrated therein comprises: a shaft part 11 which serves as a supporting system disposed at the center of a rotational axis; a rotation part 12 which is a rotating system rotating a...
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WO/2020/122056A1 |
The present invention provides a motor-integrated fan that suctions air through a suction port and blows out the suctioned air through a blow-out port, wherein: the motor-integrated fan comprises a shaft part provided in the center of a ...
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WO/2020/121582A1 |
[Problem] To provide a flight body comprising a multicopter mechanism, the flight body having both a vertical takeoff and landing function and a horizontal circling function, and also having exceptional circling capability. [Solution] In...
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WO/2020/122077A1 |
[Problem] To provide a motor cooling structure capable of improving cooling efficiency when cooling a motor that has reached a high temperature. [Solution] In the motor cooling structure equipped with a motor disposed on a board and a pr...
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WO/2020/121067A2 |
A metal air battery electrolyte replenishment system comprised of a base station with docking receptor apparatus and matching docking probe on a flying drone. The probe onboard the drone has a sensor that guides the drone to connect with...
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WO/2020/122433A1 |
The present invention relates to a drone provided with a foldable rotary wing and, more specifically, to a drone (an unmanned aerial vehicle) provided with a foldable rotary wing, wherein the wing of the drone can be folded through a sim...
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