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Matches 1 - 50 out of 1,294

Document Document Title
WO/2017/025288A1
The invention seeks to get around the problems of mass and complexity of pylons made up of assembled box sections. In order to do so, the invention effectively proposes organizing the engine - wing interface around a substantially unifor...  
WO/2017/021918A1
The invention concerns a convertible aircraft comprising a fuselage (F), a pair of wings (A1, A2) disposed to either side of the fuselage (F), at least one ducted rotor (1) installed in a horizontal position at one of the ends of the fus...  
WO/2017/022806A1
The present invention establishes a technology for accurately landing an in-flight small aircraft at a destination. A landing guide port device 2 is provided with a port ID storage unit 422 and a guiding radio wave transmission control u...  
WO/2017/013363A1
The present invention relates to an aircraft comprising a fuselage (1) and a thruster downstream of the fuselage. The thruster includes a power turbine (7), located inside a main flow jet, and at least one fan (9), located inside a secon...  
WO/2017/014508A1
A vertical take-off and landing aircraft using a hybrid electric propulsion system is disclosed. A hybrid vertical take-off and landing aircraft according to one embodiment comprises: an engine; a generator which generates electric power...  
WO/2017/013366A1
The invention relates to an aircraft comprising a fuselage (1), which is propelled by a turbine engine with two coaxial fans, namely an upstream fan (7) and a downstream fan (8), driven by two contra-rotating rotors (5, 6) of a power tur...  
WO/2017/013858A1
An information processing system for a mobile object is provided with: a mobile object manipulation license (1); a mobile object (2) having a first IC tag; an information communication terminal (3) configured to communicate with the mobi...  
WO/2017/013059A1
The invention relates to a propeller drive (20') which is, in particular, an aircraft drive and comprises a propeller machine (100) as well as an electric drive (30, 50) that is connected without a converter to said propeller machine (10...  
WO/2017/013842A1
This unmanned flight vehicle (10) comprises: a remaining battery capacity acquisition unit (112) that acquires the remaining capacity of a battery (106); an arrival determination unit (114) that determines, when the unmanned flight vehic...  
WO/2017/013077A1
The invention relates to a drive device for an aircraft, comprising a shaft turbine coupled to an impeller by means of a shaft. The impeller comprises a suction side and a thrust side. The shaft turbine is arranged in the region of the s...  
WO/2017/015551A1
An internal combustion engine for use with a propeller driven aircraft includes a camshaft adapted to function as an output shaft that rotates a propeller to provide propulsive thrust. A gear set is configured to transfer rotational powe...  
WO/2017/013361A1
The invention relates to an aircraft comprising a fuselage (1) and a propulsion assembly, said propulsion assembly comprising at least one fan rotor (7, 8) located at the rear of the fuselage (1) in the extension thereof along a longitud...  
WO/2017/013364A1
The invention relates to an aircraft including a fuselage (1) and a propulsion assembly. Said propulsion assembly includes at least one fan rotor (7, 8) placed behind the fuselage (1) as an extension thereof along a longitudinal axis (XX...  
WO2017009037A1
The invention relates to the redundant supply of kinetic energy to a drive system of an aircraft in order to ensure in each case largely safe operation of the aircraft during normal operation of the system and also in various emergency s...  
WO/2017/002298A1
The screen device of the present disclosure is provided with: a screen that has a plurality of photoelectric conversion elements and that receives video light from a video projection device; a power supply unit that supplies electric pow...  
WO/2017/000528A1
A driving device assembly including multiple driving devices (05) and an aircraft. The driving devices (05) are triangularly arranged to form a triangular driving device module (01). The combination method is that the spatial distances b...  
WO/2016/209331A3
An extremely quiet short take-off and landing (STOL) aircraft includes: two wings (203), wherein each wing comprises an engine system (220); a fuselage (206) structurally connected to each wing; and a ducted fan thruster (210) positioned...  
WO/2016/203015A1
The present invention belongs to the field of aeronautics and relates to an aeroplane with reduced installation noise, and specifically to an aeroplane wing and jet engine system including an aeroplane wing and at least one jet engine wi...  
WO/2016/200915A1
An airplane is provided. The airplane includes a pressurized compartment and an environmental control system. The environmental control system includes a compressing device. The compressing device includes a compressor and a turbine. The...  
WO/2016/195537A1
The group of inventions relates to methods and means for moving aircraft (including spacecraft) of various purpose. It is proposed to generate a lifting (moving) force of said craft by accelerating a liquid in radial curved channels (...  
WO/2016/188833A1
The invention relates to a drive unit (20) for an aircraft (10), having at least one electric motor and a propeller (14) driven by the electric motor , the electric motor being an electric motor (22) in the form of a double-coil actuator...  
WO/2016/188836A1
The invention relates to a fixed-wing aircraft (10) having a fuselage section (12) and a first and second wing section (14, 16) on both sides of the fuselage section (12), at least one drive unit (24) being mounted below and/or above the...  
WO/2016/181420A1
A mount mechanism (3) for mounting an accessory gearbox (11) to the engine case of an aircraft engine comprises: a pair of first brackets (4) affixed to either the engine case or the accessory gearbox (11) and located at a distance from ...  
WO/2016/181051A1
The invention relates to a device for controlling the orientation of the fan blades of an unducted fan turbomachine, comprising at least one set of adjustable pitch fan blades (26), said set rotating as one with a rotary ring (20) centre...  
WO/2016/178008A1
The disclosure relates to an unmanned aerial vehicle, wherein the fuel cell provides a structural component of the vehicle.  
WO/2016/171120A1
Provided is a multicopter which is equipped with a fall prevention device capable of preventing the aircraft from falling even when normal flight has become unsustainable due to various reasons. The multicopter has: a multicopter fuselag...  
WO/2016/171222A1
The purpose of the present invention is to provide a safety management system which can be easily installed in an existing aircraft in order to prevent unauthorized use, accidents, resale, theft, etc. This aircraft safety management syst...  
WO/2016/166344A1
The invention relates to an electric drive for a hybrid aircraft system. Said electric drive comprises a rotor and a stator, the stator being connectible to a structure of an aircraft, and the rotor comprising an annular flange with a sh...  
WO/2016/164649A1
A. turbine assembly system and apparatus for a Hyper) et™ and method for making same is provided. Specifically, the turbine assembly provides a power generation system for a turbine engine and includes a plurality of stages. Each stage...  
WO/2016/147032A1
Abstract: An ultra-high rpm rotatory turbine system for propulsion in the vacuum of space. The system attains ultra high angular velocities and uses sparse gas molecules, electrons, photons as well as radiation as ejectory material to pr...  
WO/2016/142573A1
The object of the invention is a method to replace the control signal of an operation organ of a remote controlled flying apparatus with another signal. The signal to be replaced (a, b, etc., y, z, etc.) is a signal to be sent from the s...  
WO/2016/138173A1
Methods of manufacturing and operating a solar powered aircraft having segmented wings that can be reconfigured during flight to optimize collection of solar energy are described. The aircraft have rigid construction that is resistant to...  
WO/2016/134433A1
Propeller-driven craft (e.g., aircraft) are provided with at least one propulsion system having at least one engine and at least one aerial tractor propeller which generates a propeller propwash airflow when driven by the engine. At leas...  
WO/2016/138139A1
A solar powered aircraft having segmented wings that can be reconfigured during flight to optimize collection of solar energy are described. The aircraft have rigid construction that is resistant to inclement weather and is configured to...  
WO/2016/136770A1
This thrust force generation device (1) is provided with: a turbo fan engine unit (2) that is provided with a generator (7) for generating power using a rotation force of a drive shaft, and drives a fan (5) provided on the drive shaft us...  
WO/2016/134366A1
A propeller (70) for an aircraft (20) having a fuselage (22) and a pair of fixed wings (50a, 50b) includes a mounting member (76) secured to at least one wing. At least one blade (72) is rotatably connected to each mounting member (76) a...  
WO/2016/131148A1
A compound engine assembly with an engine core including at least one internal combustion engine, a turbine section, and a compressor having an outlet in fluid communication with an inlet of the engine core. A casing is connected to the ...  
WO/2016/132073A1
The invention relates to an aircraft propulsion unit comprising: a turbine engine (1) having at least one unducted propulsion fan (4a), and an attachment pylon (3) intended to attach the turbine engine to a structural element (2) of the ...  
WO/2016/126231A1
In accordance with the present invention, an embodiment of a rotational ducted fan motor comprises a monolithic rotational ducted fan rotor, an electric propulsion system, a static aft-shroud comprising electrochemical-energy-storage, an...  
WO/2016/114851A1
A vertical take-off and landing (VTOL) aircraft is provided and includes wings, first and second nacelles supported on each of the wings, each of the first and second nacelles including a propeller drivable to generate aircraft thrust, a...  
WO/2016/112187A2
An engine mount system having failsafe securement points. The engine mount system includes a forward mount carrying a coat hanger shackle having a spherical bearing and a cylindrical bearing. Securement of the engine mount to a support u...  
WO/2016/112187A3
An engine mount system having failsafe securement points. The engine mount system includes a forward mount carrying a coat hanger shackle (51) having a spherical bearing (54) and a cylindrical bearing (53). Securement of the engine mount...  
WO/2016/083720A1
The invention relates to a propulsion unit (10), notably for an aircraft, comprising - a turbomachine (12); - a propeller (14) that can be selectively coupled to said turbomachine (12); - a rotary electrical machine (16) able to drive at...  
WO/2016/074134A1
A battery (100, 200, 300), a heat management apparatus (101, 301) thereof and a UAV (10) having the battery. The heat management apparatus (101, 301) comprises: a heat conduction shell (110, 210, 220, 310) having an accommodation cavity ...  
WO/2016/071040A1
The present invention relates to an optimized propulsion system comprising at least one turbomachine (2) and a supercharged internal combustion engine (1) which are mechanically coupled. According to the invention, the propulsion system ...  
WO/2016/067488A1
A multicopter (100) that has a plurality of propellers (1) and that is provided with an electric motor (2), at least one main battery (3), a generator (4), and an engine (5). The electric motor (2) drives the propellers (1). The main bat...  
WO/2016/067489A1
An electric multicopter (100) that has a plurality of propellers (1). The multicopter (100) is provided with an electric motor (2), at least one main battery (3), a generator (4), an engine (5), and a battery status detection unit (71). ...  
WO/2016/065343A1
An unmanned aerial vehicle (UAV) that includes a light and a cooling system is described. The light fitted to the UAV may be bright since heat it generates will be cooled by thermal conduction, convection and/or heat absorption. The ligh...  
WO/2016/062921A1
An electrically powered vertical takeoff and vertical landing (VTOL) aircraft, which comprises at least two main propellers (101a, 101b), wherein the main propellers are adapted to generate at least 70% of the aircraft propulsion. The ai...  
WO/2016/059953A1
[Problem] To provide an electric power supply system capable of providing a moving body with electric power by which the moving body is able to operate, without imposing any limitations to movement of the moving body. [Solution] Provided...  

Matches 1 - 50 out of 1,294