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Patent Searching and Data


Matches 1 - 50 out of 55,505

Document Document Title
WO/2017/046573A1
A method of repairing damage to a composite material (12) comprising a composite substrate (14) and at least one layer of shielding material (16). The method comprises the following steps: a) removing damage to the at least one layer of ...  
WO/2017/045475A1
A magnetic-fluid momentum sphere is used for satellite attitude adjustment. The magnetic-fluid momentum sphere comprises stators and a spherical shell. The stators are classified into three groups, axes of the three groups of stators are...  
WO/2017/048122A1
Described is a laminate, comprising a stack of mutually bonded adhesive layers and metal sheets. The laminate comprises abutting and/or overlapping metal sheet edges that extend along a length direction within a splicing region. A splice...  
WO/2017/047520A1
This flying device (10) has a plurality of connected flying units (11, 12, 70). Each of the plurality of flying units (11, 12, 70) is provided with a thruster (24-27) for generating thrust. The flying units (11, 12, 70) are provided inte...  
WO/2017/049297A1
Systems and methods are described herein for mounting a thruster onto a vehicle. A thruster mounting structure may comprise a first, second, and third rotational joint, a boom, and thruster pallet, and a thruster attached to the thruster...  
WO/2017/046231A1
The invention relates to a method for identification of an electronically controlled aircraft in the form of a remote-controlled or autonomously controlled, unmanned aircraft (6), wherein data are stored in a memory (16) of the aircraft ...  
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/2017/046279A1
The present invention relates to a method (50) for estimating the attitude of a satellite (20), said satellite being configured to generate and transmit a first reference signal on a downlink by means of a first transmitting antenna (21)...  
WO/2017/045020A1
Disclosed herein is a propulsion system comprising: a solid conductive or semiconductive cathode (130); an anode (110) having a potential difference relative to said cathode (130), said potential difference creating an electric field bet...  
WO/2017/046497A1
The invention relates to a space vehicle (1, 100), such as a satellite, the vehicle (1, 100) comprising: at least one equipment-carrying module (2) for carrying equipment of the vehicle (1); at least three posts (12) extending at least p...  
WO/2017/049183A1
Stowable and deployable unmanned aerial vehicles (UAVs), and associated systems and methods are disclosed. A UAV in accordance with a particular embodiment includes a main body, frames carried by the main body, and motors carried by the ...  
WO/2017/048336A2
A hybrid VTOL/high speed aircraft may comprise systems and functions for in flight configuration changes from high lift helicopter or VTOL mode to fixed or swing-wing high speed aircraft mode to accommodate a variety of functions or miss...  
WO/2017/048683A1
A blade includes a blade body having a surface and a hole extending through the surface of the blade body. The hole defines a hole axis and a plane perpendicular to the hole axis. The hole has an elongated hole perimeter within the plane...  
WO/2017/049135A1
In an embodiment, a ducted fan propulsion system comprises an outer cowling, adapted to form a duct. The duct houses one or more fan blades rotating about a central axis. One or more motors are in communication with the fan blades and in...  
WO/2017/048543A1
Methods and apparatus for monitoring and controlling wellsite emissions. A mobile emissions monitoring device is operated in airspace above a wellsite to generate and transmit a monitor signal related to emissions in the airspace. The em...  
WO/2017/045006A1
Overhead luggage compartment (1) for an aircraft, having an upper luggage compartment element (2), having a lower luggage compartment element (3) which is movable between an open and a closed position, having a first holding device (9) f...  
WO/2017/046536A1
The invention relates to the field of supporting interfaces, and particularly a supporting interface (30a, 30b) of this kind for an engine crankcase (90) and including a coupling part (50), a first plurality of bolts (80) and a plurality...  
WO/2017/047281A1
Provided are: a functional film; and an aircraft window structure. This functional film (100) is sequentially provided, on a first main surface of a transparent film base (10), with a functional thin film (20) that is composed of a lamin...  
WO/2017/048464A1
Noises that are to be emitted by an aerial vehicle (1210) during operations may be predicted using one or more machine learning systems, algorithms or techniques. Anti-noises having equal or similar intensities and equal but out-of-phase...  
WO/2017/047546A1
The present invention is a method for controlling a multicopter by transmitting a first control signal and a second control signal from a controller operated by the operator toward a multicopter that performs an unmanned flight with a pl...  
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/2017/048289A1
The ground-based recovery system for aircraft with disabled landing gear includes an in-ground recovery vehicle channel (10) in which an aircraft recovery vehicle (12) travels. Additional lateral slots (20a, 20b) contain lateral wheel tr...  
WO/2017/046195A1
The invention relates to a transmission device (1) including: - a housing (2), - an input shaft (3) rotatably mounted relative to the housing (2), - an output shaft (4) rotatably mounted relative to the housing (2), - a brake (12) betwee...  
WO/2017/048319A1
A tray table assembly includes a table body and a support. The support can include a first end and a second end distal from the first end. The second end of the support can be pivotably attached to the table body. The support can define ...  
WO/2017/045145A1
System and method can support photography. A controller can configure a carrier to move an imaging device along a moving path. Furthermore, the controller can apply a time-dependent configuration on the imaging device, and use the imagin...  
WO/2017/048365A1
Methods, devices, and circuits are disclosed for managing a high energy density battery (BATT1 151) and a high power density battery (BATT2 153) during operational modes in an autonomous vehicle. A power input (VIN 451) may be provided f...  
WO/2017/045089A1
A main rotor shaft 5 is mounted on each of the two sides of a rotorcraft body 1, comprising a rotor head, a total torque control device and a blade 4. The two rotor disks rotate in opposite directions. When the rotorcraft takes off, the ...  
WO/2017/046637A1
Tailed parachute-paraglider (10) comprising a first portion (A) of a substantially squared/rectangular shape with sides (11, 13) two by two substantially parallel and opposed, and a second portion (B) with trapezoidal shape, comprising a...  
WO/2017/049057A1
A light ball apparatus and method includes a remote controller device configured for transmitting and receiving data. A programmable ball is provided with an exterior shell with a top and a bottom and an interior. Two light sources are a...  
WO/2017/046634A1
The present invention provides a seating system with dynamic space optimization mechanism and design. The system comprises a spatially staggered seating arrangement, an artificial neural network, a central control module, an actuator mod...  
WO/2017/041145A1
An access controlled cabinet (10) has a front face (12) and a rear face (14). A plurality of individual compartments (16) is provided in the cabinet (10). Each compartment (16) has a respective compartment door (18) on the front face (12...  
WO/2017/044148A1
A system for generating force is provided. The system includes a rotating disk with a plurality of recesses, and bearings disposed within each recess. The system further includes at least one guide, disposed adjacent to the disk, which c...  
WO/2017/041912A1
The invention relates to escape path markings for aircraft and to an assembly consisting of an escape path marking and a floor fitting. The escape path marking (1) for aircraft comprises a lighting element (3), which luminesces in the da...  
WO/2017/044184A2
A carbon nanotube-based thermal gasket for space vehicle applications, and process for making the same, is disclosed. A thermal gasket is created that includes one or more free-standing carbon nanotube (CNT) sheets formed of a CNT compos...  
WO/2017/041220A1
A locking device (140, 210, 310) of a battery module (13) is disposed on a housing (130, 200, 300) of the battery module (13) and configured to lock the battery module (13) to an electrical apparatus. The locking device (140, 210, 310) c...  
WO/2017/043177A1
Provided is a waste bin device for an aircraft lavatory unit, which is advantageous in having a reduced number of components and for reducing the weight of the lavatory unit. A chute 30A, a waste flap 32, and a waste container 34A are ma...  
WO/2017/042251A1
The invention relates to a device (1) for handling containers and/or packagings, comprising a first handling unit (2) which handles the containers and/or packagings in a first predetermined manner, and a second handling unit (6) which ha...  
WO/2017/042685A1
A device is disclosed; said device is capable of floating in the sky by means of the interaction of its surface with the wind, as in the case of a kite. The device features a plurality of cylinders linked together, with valves at their f...  
WO/2017/044784A1
An arm rest support includes a support element. A reinforcing element is disposed on the support element. The support element is chemically compatible with the reinforcing element. A homogeneous chemical bond is formed between the suppor...  
WO/2017/044786A1
An apparatus for bending metal beams and methods of using the same are provided herein.  
WO/2017/042354A1
A VTOL (vertical take-off and landing) aerial flying vehicle comprising an inner frame, a gimbal system and an outer frame, the inner frame comprising a propulsion system and a control system, the propulsion system being able to generate...  
WO/2017/044798A1
A docking station for an aircraft includes a base portion and an alignment system disposed on the base portion configured to orient the aircraft relative to the base portion. The alignment system can include a plurality of outer protrusi...  
WO/2017/044683A1
A composite has a) a PMC layer, and b) a tile layer comprising a plurality of Ox/Ox CMC tiles each has: i) a central portion, ii) an outer portion disposed surrounding the central portion, the bottom surface of the outer portion is dispo...  
WO/2017/042291A1
The invention relates to a vertical take-off and vertical landing aircraft (1,1b) configured for flying in a first flight mode (200) and a second flight mode (201), wherein the aircraft (1,1b) comprises: -a front section (2) comprising t...  
WO/2017/042165A1
The invention aims to achieve an emergency opening of a vehicle closing element with a minimum of operations and in a minimum of time, without substantially increasing the space requirement or the weight. To do this, a near-instantaneous...  
WO/2017/044169A1
Described is a breakover mechanism for a passenger seat that includes a frame member with a rear portion attached to two opposing sides of a seat back of the passenger seat wherein the frame member is at least partially disposed under a ...  
WO/2017/041302A1
An apparatus and methods for stabilizing a payload device such as an imaging device are provided. The apparatus includes a carrier for controlling torque delivery to a payload (1804). The carrier comprises at least one carrier component ...  
WO/2017/043687A1
Disclosed is an L-V-C operation system for providing an L-V-C-based unmanned air vehicle training/experimental environment. The L-V-C operation system of the present application may comprise a synthesis environment control unit which exc...  
WO/2017/043980A1
A rotor assembly for a multirotor aircraft, and a multirotor aircraft, are disclosed herein. The rotor assembly has a first motor having a first axis of rotation and a first propeller connected to the first motor. The rotor assembly has ...  
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...  

Matches 1 - 50 out of 55,505