Login| Sign Up| Help| Contact|

Patent Searching and Data


Matches 1 - 50 out of 1,189

Document Document Title
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/2016/083720A1
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...  
WO/2015/134234A1
A pylon structure (10) for mounting an aircraft engine to a wing. The pylon structure comprises a torque box (12) having a wing mount (14) on the aft portion, a first engine mount (16) on the fore portion and second engine mount (18) on ...  
WO/2015/115927A1
The claimed group of inventions relates to power engineering and can be used for locating faults in overhead power transmission lines. A method for locating faults in overhead power transmission lines comprises installing, on a lightn...  
WO/2015/116260A1
A method of protecting fuel hardware for a gas turbine engine in an aircraft is disclosed. The method may include determining a current altitude of the aircraft, and controlling a temperature of fuel for the gas turbine engine based at l...  
WO/2015/110749A1
The invention relates to a turbomachine casing (1) comprising: a hub (2), an outer shroud (3), and yokes (11) projecting from the outer shroud (3), for attaching the housing (1), characterised in that it comprises at least one stiffener ...  
WO/2015/108578A3
A VTOL aircraft includes at least one puller rotor and at least one pusher rotor. The VTOL aircraft, for example, may include three puller rotors and one pusher rotor. The combination of static puller and pusher rotors allows the rotors ...  
WO/2015/108578A2
A VTOL aircraft includes at least one puller rotor and at least one pusher rotor. The VTOL aircraft, for example, may include three puller rotors and one pusher rotor. The combination of static puller and pusher rotors allows the rotors ...  
WO/2015/104494A1
The invention relates to a structure (100) for the suspension of a turboprop engine (10) having two unducted propellers on a structural element of an aircraft, comprising a suspension frame (102) which is to be fastened to a structural e...  
WO/2015/096842A3
According to the invention, the assembly of the half-sphere airplane wing made it possible to create another form of flight (vertical flight), controlling air flow only on the top surface of the circular wing, said assembly being a perfe...  
WO/2015/094003A1
The invention relates to air transport and can be used in aircraft of various designs. The aircraft wing comprises a lifting surface and a turbojet engine (1). The lifting surface is the combination of a conventional aerodynamic wing (3)...  
WO/2015/089404A2
Redundant active vibration and noise control systems and methods are provided, which include safety-critical systems and methods. In one embodiment, a safety-critical active vibration control system (SCAVCS) is provided, which includes a...  
WO/2015/082854A1
The invention relates to a method for mounting an engine module (1) in a mount comprising a first structure (3) and a second structure (2) that is offset relative to the first structure (3), which method is intended to position at least ...  
WO/2015/076882A2
A turbine engine fan case (48) comprises a composite body member (300) circumscribing an axis (500) and having an annular mounting portion (310, 410), a segmented polymer member (320, 330, 420, 440) along the annular mounting portion, an...  
WO/2015/076882A3
A turbine engine fan case (48) comprises a composite body member (300) circumscribing an axis (500) and having an annular mounting portion (310, 410), a segmented polymer member (320, 330, 420, 440) along the annular mounting portion, an...  
WO/2015/074043A3
An engine attachment system (EAS) includes a forward collar (202), an aft collar(204), at least one truss subassembly (216) disposed between the forward collar and the aft collar for supporting an engine, and at least one vibration isola...  
WO/2015/074043A2
Engine attachment systems (EASs) and methods are provided. In one aspect, an EAS includes a forward collar, an aft collar, at least one truss subassembly disposed between the forward collar and the aft collar for supporting an engine, an...  
WO/2015/067891A3
The invention provides, in order to allow a fan engine (10) to be placed as close as possible to the lower surface of a wing box (21), an assembly (1) for an aircraft including means (8) for attaching a rigid structure (6) of an engine s...  
WO/2015/067906A1
The invention relates to a turbine engine, comprising two structural annular casings (16, 22) connected to one another by means (40, 54) for absorbing stresses from the thrust of the engine, which include connecting rods (54), characteri...  
WO/2015/064767A1
 Provided is a technology which, in vertical lift, oblique lift, vertical descent, oblique descent, horizontal flight and hovering for example, enables the maintenance of a stable and secure attitude of an airframe, using a single wing...  
WO/2015/057544A1
A compressor impeller for an Auxiliary Power Unit (APU) includes a hub including a plurality of splitter blades interposed between a plurality of main blades. Each of the plurality of splitter blades and the plurality of main blades incl...  
WO/2015/050652A1
An exhaust system for an aircraft includes an exhaust duct configured to be inserted within a plurality of leaf springs of an aircraft. The exhaust duct is configured to be in fluid communication with the auxiliary power unit for conveyi...  

Matches 1 - 50 out of 1,189