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Matches 1 - 50 out of 1,340

Document Document Title
WO/2017/065858A2
A propulsion system coupled to a vehicle. The system includes an ejector having an outlet structure out of which propulsive fluid flows at a predetermined adjustable velocity. A control surface having a leading edge is located directly d...  
WO/2017/065859A2
A propulsion system coupled to a vehicle. The system includes a convex surface, a diffusing structure coupled to the convex surface, and at least one conduit coupled to the convex surface. The conduit is configured to introduce to the co...  
WO/2017/065107A1
Provided is an information transmission device that can project an image from a moving body to the outside thereof and that can widely and conveniently present arbitrary information to people passing through the surroundings of the movin...  
WO/2017/060584A1
The present invention relates to an aircraft comprising a fuselage (1), a propulsion unit (7) at the rear tip of the fuselage and at least two engines (3, 5) each driving an engine shaft (32, 52), the propulsion unit including at least o...  
WO/2017/060581A1
The invention relates to a system for suspending two modules of a propulsion unit, such as two fan modules, said system comprising a pylon (28) and a rudder bar (30). One part (30') of the rudder bar is hinged to the pylon, while the opp...  
WO/2017/060585A1
The present invention relates to an aircraft comprising a fuselage, a lateral support wing (1) and a propulsion assembly (100) mounted under the wing, the wing comprising at least two structural spars (1lba, 1lbf) extending from the fuse...  
WO/2017/060628A1
The present invention relates to an aircraft propulsion assembly comprising at least a main turbine (5) mounted along a longitudinal axis (XX), at least one main fan (8) arranged upstream of the main turbine (5) along the longitudinal ax...  
WO/2017/060629A1
The present invention relates to an aircraft propulsion assembly comprising at least one twin-spool gas generator (30) of longitudinal axis (XX), at least one main fan (8) arranged upstream of the gas generator along the longitudinal axi...  
WO/2017/057795A1
The present invention relates to an insect-mimicking ornithopter, which comprises: a pair of wings (110) symmetrically arranged at the right and left sides of a body of the ornithopter; a direct current motor (120) installed in the body;...  
WO/2017/051111A1
The invention relates to a shock absorber assembly (200) for a non-streamlined blower comprising: an extension collar (210) having a first interface (201) suitable for being rigidly attached on a first module of the blower; a connector s...  
WO/2017/053634A1
A motor mount assembly (320) is provided for coupling a propeller motor (310) to a body of an unmanned aerial vehicle (UAV). The motor mount assembly includes a floating portion (330) and acts to attenuate frequencies of vibration from t...  
WO/2017/048627A1
Aircraft support structures, systems, and methods are disclosed. In one embodiment, an aircraft system includes a rotating component and a support (e.g. strut) that supports the rotating component. The support includes a locking assembly...  
WO/2017/048016A1
A wired air vehicle energy supply system according to the present invention comprises: an air vehicle comprising a fuel cell and an air vehicle electric device; a fuel cell fuel supply device positioned outside the air vehicle; and a tra...  
WO/2017/042774A1
A novel, portable electric generator and energy conversion method for using small- sized or model vehicles. The portable electric generator is composed of a liquid fuel tank, a glow spark plug-type internal combustion motor, a dynamo and...  
WO/2017/040565A1
Aft-mounting systems, devices, and methods for turboprop and turboshaft engines include two or more coupling elements 201, 211, 221 that are configured to couple an aft portion of an engine of an aircraft to a support structure of the ai...  
WO/2017/041018A1
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...  
WO/2017/035841A1
An unmanned aerial vehicle (20) comprises a monitoring device, a wireless communication device, and a flight control device. The monitoring device is configured to generate a supply demand signal when detecting that the unmanned aerial v...  
WO/2017/038809A1
Provided is a flight position control device that can cause a drone having a plurality of rotary wings to quickly move to a prescribed position in a space, and cause the airframe to hover stably in that position. The flight position cont...  
WO/2017/030034A1
The problem addressed by the present invention is to provide a power-generating device with which it is possible to efficiently and safely charge a storage cell of an unmanned air vehicle during flight, and an unmanned air vehicle provid...  
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...  

Matches 1 - 50 out of 1,340