Login| Sign Up| Help| Contact|

Patent Searching and Data


Matches 201 - 250 out of 7,060

Document Document Title
WO/2016/108015A1
Apparatus for supporting a nacelle of an aircraft engine. The invention relates to an apparatus (1) for supporting a nacelle (2) of an aircraft turbojet, comprising: a frame (10); a supporting structure (11) extending upwards from the fr...  
WO/2016/100676A1
Embodiments of the present invention relate to composite materials for use as a vehicle arresting system (also referred to as an Engineered Material Arresting System (EMAS). Specific embodiments may use modified polymeric foams composite...  
WO/2016/094981A1
Magnetic table jig assemblies and methods allow workpieces (e.g., aircraft components to be fabricated) on a table top of the table jig assembly to be accurately indexed relative to a robotically operated tool (e.g., a robotically operat...  
WO/2016/099285A1
A control system (16) and a method for manoeuvring an elongated element (1) which projects in a pivotable manner from a foundation (13) are described, wherein the landing place (2) is provided with a camera-readable pattern (22); the pro...  
WO/2016/093701A1
Helipad and helipad illumination system The invention relates to a dynamic helipad illumination system (2) for dynamically illuminating a floor surface or supporting deck of helipad (1) at least partly in order to enable communication of...  
WO/2016/094543A2
A UAV support vehicle carries a UAV support apparatus for launching and/or recovering a UAV while the UAV support vehicle is moving. The UAV support apparatus releases the UAV during launch and receives the UAV during recovery. An active...  
WO/2016/094543A3
A UAV support vehicle carries a UAV support apparatus for launching and/or recovering a UAV while the UAV support vehicle is moving. The UAV support apparatus releases the UAV during launch and receives the UAV during recovery. An active...  
WO/2016/094543A4
A UAV support vehicle carries a UAV support apparatus for launching and/or recovering a UAV while the UAV support vehicle is moving. The UAV support apparatus releases the UAV during launch and receives the UAV during recovery. An active...  
WO/2016/094067A1
Disclosed herein is a system and device for a drone docking station for deposit of items delivered by drone. Items may include but not be limited to food items, groceries and parcels. A secure porch, roof, window or otherwise building mo...  
WO/2016/089066A1
The present invention relates to a taking-off and landing system for a drone and, more specifically, to: a system in which a product is transported by a drone, in an unmanned way, to a device, possessed by a user, for enabling the drone ...  
WO/2016/088221A1
The present invention addresses the problem of providing a durable aircraft body cover which can be easily put on and taken off by one person and is easy to put away after being taken off. The inner side of the body cover 1 has a plurali...  
WO/2016/085404A1
An apparatus for launch and recovery of an Unmanned Aerial Vehicle (UAV), a method for launching a UAV, a method for recovering a UAV and a kit of parts for launch and recovery of a UAV are disclosed. The apparatus comprises a boom havin...  
WO/2016/078093A1
A base station for automated battery pack or payload exchange and methods for using the same. The base station provides a landing surface for receiving a mobile platform and includes a manipulator controlled by a manipulator compartment ...  
WO/2016/078025A1
Disclosed are a positioning mechanism, a UAV base station using the positioning mechanism, and a UAV replenishment method. The positioning mechanism comprises a base provided with a landing area, on which a positioning part is provided; ...  
WO/2016/075409A1
The present invention relates to method for monitoring an engine (1) of an aircraft (2) operating in a given environment. The invention is characterized in that it comprises the implementation, via means for data processing (31), of the ...  
WO/2016/076696A1
The present invention relates in general to a coupling mechanism, specifically to a connecting cabin that can be adapted to passenger transfer mechanisms in the aviation sector, particularly for passenger boarding and/or disembarkation b...  
WO/2016/076704A1
The invention relates toa method for inspecting and/or repairing surface damage of a component in a device via an access opening, using fluorescent penetrant inspection (FPI), with a borescope inspection kit comprising flexible conduits,...  
WO/2016/076695A1
The invention relates to a mechanical system for the transfer of people between places located at different heights, as is the case in facilities that are temporary, under construction, or where at least one of the places is mobile, such...  
WO/2016/071633A1
The invention concerns a system for the local surface treatment of an aeronautical part (1) to be treated. Said system is characterised in that it comprises a plurality of reservoirs (18, 19, 20, 21} each comprising a treatment product (...  
WO/2016/071103A1
The invention relates to a sealing device (1; 2) for sealing a duct (3; 4) in a gas turbine (5) in order to prevent downtime corrosion, characterized in that the sealing device (1; 2) comprises a vapor-impermeable membrane (9; 15) and at...  
WO/2016/072239A1
Provided is a device whereby a balloon can be filled with gas outdoors and the balloon can be anchored without directly fixing a mooring line to the ground, e.g., by an anchor. This balloon storage box 203 has: a balloon anchoring device...  
WO/2016/071639A1
The invention relates to a device (1) for transporting a passenger (V) from door to door, characterised in that it comprises: a platform (2) equipped with means for moving along the ground; at least one private seat (3) comprising a powe...  
WO/2016/068452A1
The present invention relates to an integrated landing reception device for landing an aircraft and a control method therefor. The integrated landing reception device for landing the aircraft, according to the present invention, comprise...  
WO/2016/064038A1
The movable dehumidification apparatus for an aircraft according to the present invention comprises: a dehumidification unit comprising a first air inlet for introducing external air, a dehumidification rotor for performing dehumidificat...  
WO/2016/063112A1
The invention provides a method of sampling de-icing fluid (2) from an airplane de-icer (10) having a spraying nozzle (16) for spraying the de-icing fluid (2) onto a surface of an airplane (4), the de-icing fluid (2) preferably being pro...  
WO/2016/061000A1
An Airborne Wind Turbine ("AWT") may be used to facilitate conversion of kinetic energy to eiectrieai energy. An AWT may include an aerial vehicle ihai flies in a path to convert kinetic wind energy to electrical energy. The aerial vehic...  
WO/2016/059555A1
An unmanned aerial vehicle (UAV) system provides for UAV deployment and remote, unattended operation with reduced logistics requirements. The system includes a launcher that can include one or more containers, or hangars, configured to h...  
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/2016/057155A1
The invention relates to a mobile ground power unit (1) for supplying power to an air-craft parked on the ground, the ground power unit (1) comprising an engine (10), which is preferably a combustion engine, and - an electric generator (...  
WO/2016/057154A1
The invention relates to a mobile ground power unit (1) for supplying power to an air-craft parked on the ground, the ground power unit (1) comprising an engine (10), which is preferably a combustion engine, and - an electric generator (...  
WO/2016/055964A1
A process for assembling aircraft control surfaces (1, 1'), in particular high-lift devices and wing portions, allows implementing smooth control surfaces in short times, wherein the control surface is defined by an upper skin (2) and by...  
WO/2016/057153A1
The invention relates to a Mobile ground power unit (1) for supplying power to an air-craft parked on the ground, the ground power unit (1) comprising - an engine (10) and - an electric generator (20), whereby the electric generator (20)...  
WO/2016/050987A1
The present invention is concerned with an aircraft environmental control system for temporary engagement with an aircraft fuselage in order to permit conditioning, most preferably dehumidification, of the air within one or more enclosur...  
WO/2016/046185A1
The invention relates to a processing system for aircraft structural components (2), comprising at least one processing station (3, 4) wherein the processing station (3, 4) has a clamping frame (7, 8), extending along a longitudinal axis...  
WO/2016/044794A2
A Runway Incursion Prevention System (RIPS) involves a Runway Incursion Barrier System (RIBS) and Interface Vector Imaging (IVI), with an emphasis on positively controlling ground movement to prevent runway incursions in the aviation/aer...  
WO/2016/043581A1
The invention relates to a mobile airline kiosk (1) for use at an airport, comprising a man-transportable structure (2) having, in an operational state: -communication means (3) for providing a wireless data connection (4) to an airline ...  
WO/2016/038760A1
This passenger boarding bridge (100) is provided with a cab (20) that is disposed at the leading end of a tunnel portion (10) and is mounted to a boarding portion (202) of an aircraft (200) so as to form a walkway (21). The cab (20) is p...  
WO/2016/038761A1
This passenger boarding bridge (100) is provided with a cab (20) that is disposed at the leading end of a tunnel portion (10) and mounted to a boarding portion (202) of an aircraft (200) so as to form a walkway (21). The cab (20) is prov...  
WO/2016/038037A1
The invention relates to a repair unit (10) for a pod (11), especially a laser designation pod, comprising: a transportable casing (14); a bubble (18) attached to the casing (14), having a retracted state and a deployed state, the bubble...  
WO/2016/035963A1
Disclosed is a height adjustment device for a rotunda of a boarding bridge. A height adjustment device for a rotunda of a boarding bridge can comprise: an outer column which fixes a rotunda and ascends and descends; an inner column which...  
WO/2016/035962A1
Disclosed are a system and a method for arrival. A system for arrival can have: an air control radar unit for calculating the expected traveling time of an aircraft, before landing, to a runway and displaying same on a screen; a parking ...  
WO/2016/026315A1
A guiding system of three-dimensional high-directivity infrared light for aircraft landing and an aircraft landing guide method using same. The system comprises a low divergent infrared laser source (2) emitting at an optimal landing ang...  
WO/2016/028736A1
Described embodiments include an unmanned aerial vehicle and a method. The unmanned aerial vehicle includes an airframe and a rotary wing system coupled with the airframe and configured to aerodynamically lift the vehicle in the air. The...  
WO/2016/023088A1
Testing apparatus, systems (10) and methods are provided to obtain measurements pertaining to aircraft control surfaces (ACS) mounted to stationary aircraft structures (AAS) for displacements about a hinge axis (HA). A support structure ...  
WO/2016/023125A1
A counter module system is provided, which may allow for partial or full self check-in by a passenger at a transportation facility, such as an airport. The system may comprise a counter module having multiple bays each for receiving an e...  
WO/2016/024031A1
The invention relates to a halting system in walkways of three or more tunnels for boarding aircraft and watercraft, said walkways being formed by: a first tunnel (1); one or more intermediate tunnels (2, 2.1); a last tunnel (3); and tra...  
WO/2016/019567A1
Systems and methods are provided for swapping the battery on an unmanned aerial vehicle (UAV) (201). The UAV (201) may be able to identify and land on an energy provision station (202) autonomously. The UAV (201) may take off and/or land...  
WO/2016/019814A1
A vacuum energy-storing type take-off ejector for a fixed wing aircraft is formed by connecting an electric winch (1), a trailer wagon (2), a speed variator, a disc cable wheel, a large diameter piston (7), a large diameter vacuum cylind...  
WO/2016/019564A1
A multi-zone battery station is provided, comprising a plurality of landing areas configured to support a UAV. The battery station may permit battery life to be reloaded onto a UAV, which may include recharging a battery of the UAV or ex...  
WO/2016/015354A1
Disclosed are an unmanned aerial vehicle dock and a battery replacement device thereof. The battery replacement device (10b) comprises: a grabbing device (14) for grabbing a battery, a first translation mechanism (11) for driving the gra...  

Matches 201 - 250 out of 7,060