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Matches 51 - 100 out of 2,721

Document Document Title
WO/2020/240198A1
A vehicle (10), preferably an unmanned and/or autonomous vehicle for example an unmanned aerial vehicle, UAV, is described. The vehicle (10) comprises: a set of structural components (100), arranged to provide, at least in part, a struct...  
WO/2020/240957A1
This flight object which is long and can be suspended is configured to be provided with: a drive unit for driving a propeller with less power consumption when the flight object is suspended than when the flight object flies without being...  
WO/2020/237082A1
A vertical take-off and landing aircraft which uses fixed rotors for both VTOL and forward flight operations. The rotors form a synthetic wing and are positioned to achieve a high span efficiency. The rotors are positioned to even out th...  
WO/2020/229287A1
Disclosed is an aircraft assembly comprising: a first aircraft structure, a second aircraft structure, first and second tension bolts arranged to suspend the first aircraft structure below the second aircraft structure, the first and sec...  
WO/2020/180368A3
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.  
WO/2020/185274A3
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...  
WO/2020/227837A1
An electric propulsion system for an aircraft includes a nacelle and an electric machine. The electric machine includes a stator positioned in the nacelle, and a rotor and fan assembly positioned in a primary flow path through the nacell...  
WO/2020/190344A3
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...  
WO/2020/225510A1
The invention relates to a hybrid propulsion system (10) for a vertical take-off and landing (VTOL) aircraft comprising at least one combustion engine (120, 140) driving an electricity generator (122, 142), at least one electrical energy...  
WO/2020/180376A3
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...  
WO/2020/222674A1
The group of inventions relates to the field of aviation. An aircraft train consisting of an aircraft having a nuclear power plant and an additional aircraft comprises an aircraft having a nuclear power plant that includes a nuclear reac...  
WO/2020/223115A2
Systems, devices, and methods including: at least one unmanned aerial vehicle (UAV) (108A,B); at least one battery pack (114) comprising at least one battery (120); and at least one motor (112) of the at least one UAV, where the at least...  
WO/2020/217624A1
Provided is a control device that controls a flying body including a double-sided light-receiving solar battery panel provided on a main wing, the control device comprising: a positional relationship acquisition unit that acquires the po...  
WO/2020/219112A1
An aircraft navigational system for a multiengine aircraft can include a flight planning module configured to receive two or more navigational points defining a route and determine if a first degraded operation ceiling is high enough to ...  
WO/2020/217623A1
Provided is a control device for controlling an aerial vehicle having a double-sided light receiving type solar cell panel disposed on a main wing, the control device comprising: a positional relationship acquisition unit that acquires t...  
WO/2020/219994A1
In one embodiment, a solar powered high altitude long endurance aircraft power bus architecture is provided which includes a main DC power bus, with a battery connected to the main DC power bus. This embodiment includes a plurality of so...  
WO/2020/219111A1
A control system for a hybrid electric powerplant of an aircraft can include a master controller configured to receive one or more power settings and to output a heat engine setting and an electric motor setting and a heat engine control...  
WO/2020/217058A1
The present disclosure pertains to an unmanned aerial vehicle system. Some exemplary implementations may include: a mounting frame (110) onto which at least a payload (30) is affixed; a plurality of fuel cell stacks (50) operable in a pr...  
WO/2020/213831A1
The present invention directly drives an electric motor (115) through the power of power generators (100, 102) that produce electric power by means of the driving of a gasoline engine (103), so as to drive propellers (116), provides a po...  
WO/2020/212656A1
The invention relates to a hybrid propulsion system (100) for a multi-rotor rotary-wing aircraft, comprising: an internal combustion engine (12), an electric machine (14) coupled to the internal combustion engine, a rectifier (16) connec...  
WO/2020/212966A1
A system comprising: an Unmanned Aerial Vehicle (UAV) carrier comprising a power supply, the UAV carrier connected, via respective wires, to one or more UVs, wherein: (a) each of the UVs is capable of performing maneuvers irrespective of...  
WO/2020/180372A3
A hybrid electric engine control module (ECU) can be 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 hea...  
WO/2020/209255A1
[Problem] To provide a drone system for safely executing a task by using a plurality of drones. [Solution] A drone system (500) comprising at least a plurality of drones (100) that fly within a task area (403a) and execute a task, and a ...  
WO/2020/208527A1
An electric power system (300) with integrated fire relief channels for an electric vehicle (100), the electric power system comprising: a power source (104, 180) configured to power a motor (160) that propels a vehicle housing (101), th...  
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...  
WO/2020/208318A1
The invention concerns a hybrid propulsion installation (100) for an aircraft, comprising: an internal combustion engine comprising at least one combustion chamber (114); at least one electricity generator (134a, 134n); an electrical pro...  
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...  
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...  
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...  
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...  
WO/2020/149907A3
An aircraft includes a fuselage, an engine, a pylon, a nacelle cowling, and a gearbox assembly. The engine is spaced apart from the fuselage and the pylon is disposed between the fuselage and the engine. The accessory gearbox is fixed to...  
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...  
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...  
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...  
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...  
WO/2020/121067A3
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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.  
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...  
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...  
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...  
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 ...  
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...  

Matches 51 - 100 out of 2,721