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Matches 1 - 50 out of 1,246

Document Document Title
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) etâ„¢ 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...  
WO/2016/046482A1
The invention relates to a turbine engine provided with an element (3), comprising a wall (11) and at least one load-bearing member (17) extending substantially perpendicularly relative to the wall (11). Said member (17) is to be attache...  
WO/2016/042264A1
The invention relates to a method for mounting an engine (1) on an aircraft pylon (3) comprising engine suspension members (31) secured to the pylon, the engine being secured to a suspension cradle (6) via which it is suspended from the ...  
WO/2016/030168A1
A fault tolerant, optically or electrically managed, EMP resilient electromagnetic distributed direct drive powertrain applied to provide lift and/or propulsion and/or attitude control to an aircraft. The electromagnetic distributed dire...  
WO/2016/025784A1
In one aspect, a method is described. The method may include operating a plurality of circuit elements, and operating a plurality of magnetically-coupled power-balancing circuits. Each individual power-balancing circuit may be electrical...  
WO/2016/022726A1
An airframe is provided that includes a forward lifting wing, tail control surfaces, a propeller mounted between the wing and the tail control surfaces, a motor driving the propeller, a fuselage supporting the motor and the wing, and an ...  
WO/2016/019562A1
Systems and methods are provided for swapping the battery on an unmanned aerial vehicle (UAV) while providing continuous power to at least one system on the UAV. The UAV may be able to identify and land on an energy provision station aut...  
WO/2016/018486A3
A vertical takeoff and landing aircraft includes a pair of ducted lift/thrust fans that are rotatably movable between a first vertical lift position and a second horizontal thrust position. The lift/thrust fans are disposed within curvil...  
WO/2016/018486A2
A vertical takeoff and landing aircraft includes a pair of ducted lift/thrust fans that are rotatably movable between a first vertical lift position and a second horizontal thrust position. The lift/thrust fans are disposed within curvil...  
WO/2016/009824A1
[Problem] To ensure safety demanded of an aircraft while suppressing an increase in the total weight of the drive system. [Solution] Disclosed is a motorized aircraft controlled by a drive control means (120) that rotates and drives prop...  
WO/2016/008125A1
Disclosed is an intelligent electric quantity protection method for an electric unmanned aerial vehicle. The method comprises the steps of: acquiring the current remaining electric quantity of a battery in real time; acquiring coordinate...  
WO/2016/003534A3
A method for securing an engine using an adjustable mounting assembly is provided including adjusting an extendible element of the adjustable mounted assembly from a first position to a second position. Another extendible element of the ...  
WO/2016/001581A1
The invention relates to an aircraft propulsion assembly comprising a turbofan engine (2) equipped with a nacelle (3), the turbojet comprising a structure defining a first part of the secondary flow path (54) for channelling the secondar...  
WO/2015/196276A1
A Pulsed Locomotor (120), for propelling media, fluids and crafts, in fluids and on land, comprising a blade (124) securely connected to a drive shaft (122). Upon reciprocation, the ambient medium is forced towards the trailing edge of t...  
WO/2015/191017A1
Invention is about an electrical jet motor system with super conductive technology which can be used as a throttle power in all kind of air vehicles. Special designed electrical motor (1) has no axis shaft. Super conductive wires (2.5) w...  
WO/2015/178091A1
[Problem] To provide a highly safe flying device taking into consideration the influence on a user using the flying device and the flight environment. [Solution] The present disclosure provides a flying device provided with a flying mech...  
WO/2015/177431A1
A ball joint device (10) for suspension of a turbine machine to a pylon or suspension of a device on the body of a turbine engine. The device comprises a first member (12) one end of which carries a ball (14) and which is inserted betwee...  
WO/2015/169276A1
The invention relates to a drive (1) for an autonomously acting mobile device (2), comprising an input shaft (4), an internal combustion engine (5) which is connected to the input shaft (4) and an actuating drive (6) for influencing torq...  
WO/2015/157114A1
Modular nacelles to provide vertical takeoff and landing (VTOL) capabilities to fixed-wing aerial vehicles, and associated systems and methods are disclosed. A representative system includes a nacelle, a power source carried by the nacel...  
WO/2015/146608A1
[Problem] To provide electrified aircraft such that the path angle and rate of descent can be controlled independently of speed and with high response by operating the drag of a propulsion drive system whereby electric power generated du...  
WO/2015/138217A1
UAV configurations and battery augmentation for UAV internal combustion engines, and associated systems and methods are disclosed. A representative configuration includes a fuselage, first and second wings coupled to and pivotable relati...  

Matches 1 - 50 out of 1,246