Login| Sign Up| Help| Contact|

Patent Searching and Data


Matches 1 - 50 out of 1,591

Document Document Title
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...  
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...  
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...  
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...  
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...  
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 ...  
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...  
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...  
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...  
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...  
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...  
WO/2018/000913A1
A robot wing assembly device, comprising: a wing support (13), an electric machine (14), an encoding disk (10), a photoelectric sensor (7), a wing casing, and a wing (6). The wing casing is divided into a left wing casing (8) and a right...  
WO/2018/002855A1
Apparatus and method for conditioning engine-heated air onboard an aircraft including a heat exchanger (140) at least partially disposed in a pylon structure (118) for supporting an engine (134) of the aircraft. The pylon heat exchanger ...  
WO/2017/214934A1
A frame assembly (20), comprising a frame (21) and arms (22); each of the arms (22) is connected to one end of the frame (21), the frame (21) is connected to the arms (22) by means of joint portions (30, 60), the joint portions (30, 60) ...  
WO/2017/207666A2
The invention relates to an air ship having a supporting structure (12) and a shell (10) that can be filled with a gas and which is tensioned by the supporting structure (12). According to the invention, said supporting structure (12) co...  
WO/2017/207666A3
The invention relates to an air ship having a supporting structure (12) and a shell (10) that can be filled with a gas and which is tensioned by the supporting structure (12). According to the invention, said supporting structure (12) co...  
WO/2017/207968A1
A battery arrangement and a method of operating a battery arrangement for a solar powered aerial vehicle. The battery arrangement has a plurality of batteries arranged in a plurality of groups, the groups including a first battery group,...  
WO/2017/203793A1
According to the present invention, a body part is provided with: a plurality of motors; and a plurality of rotors corresponding to the motors. The rotors are driven by output from the corresponding motors. The rotational speed of each o...  
WO/2017/200277A1
A battery of a vehicle such as a car, an electric aircraft, an electric ship, an electric submarine or the like is formed inside a bag or the like of a carrier. The carrier bag is formed in such a manner that a handle thereof is pulled o...  
WO/2017/197232A1
Aircraft isolator devices, systems, and methods for isolating a structural component within an aircraft can include an engine interface, airframe, and one or more (e.g., a plurality of) isolator devices attached to the engine interface a...  
WO/2017/197325A1
An unmanned aerial vehicle includes at least one rotor motor configured to drive at least one propeller to rotate. The unmanned aerial vehicle includes a data center including a processor; a data storage component; and a wireless communi...  
WO/2017/197245A1
A solar power system comprising a solar panel, a load, and a battery pack group. The load comprising an electric motor operatively coupled with a propeller. The battery pack group comprises one or more voltage controllable battery packs,...  
WO/2017/185487A1
A battery fixing and mounting structure for a battery self-dismounting unmanned aerial vehicle comprises an unmanned aerial vehicle mainly body (1) and a battery cover (2). A battery chamber (10) used for accommodating a battery (4) is f...  
WO/2017/188699A1
A discharge device according to an embodiment of the present invention comprises: a housing having an inlet for introducing a fluid to a central region thereof, an outlet at an edge thereof, and a stator; a mouth composed of an outer wal...  
WO/2017/180392A1
The modular aircraft system includes a single fuselage (10) having a permanently installed empennage (12) and plural sets of wing modules (46a, 46b, 66a, 66b, 68a, 68b) and engine modules (56, 60, 64), with each wing and engine module op...  
WO/2017/178853A1
The air flow which this invention itself makes on its surface makes lift by the Bernoulli effect. This invention utilizes the difference of the pressure of one side of the surface on which air flows and that of the other side of the surf...  
WO/2017/176174A1
The present invention relates to flying scooter comprising a base made of fibreglass, 20 fans with 20 motors connected to a power system with components comprising capacitors, batteries, photovoltaic solar cells, an oxygen generator, a r...  

Matches 1 - 50 out of 1,591