| Document |
Document Title |
|
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/2016/094067A1 |
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...
|
|
WO/2016/016604A1 |
A ground level illumination system such as a road stud comprises a light source (12) positioned below ground level (8). An optics block (9) and a top block (2) transmit light from the source (12) to the exterior, the light rising at a sh...
|
|
WO/2016/015546A1 |
A system and method for aircraft docking guidance and aircraft type identification. The method is executed in the system for aircraft docking guidance and aircraft type identification comprising a machine vision sub-system, a laser scann...
|
|
WO/2016/017883A1 |
An active airfield lighting apparatus is disclosed. The active airfield lighting apparatus may comprise: a plurality of lighting units arranged along a preconfigured movement position of a moving object and capable of lighting up in mult...
|
|
WO/2016/015547A1 |
A machine vision-based method and system for aircraft docking guidance and aircraft type identification, the method comprising: S1, an aircraft berthing scenario setting step: a monitoring scenario is divided into different information p...
|
|
WO/2016/011389A1 |
A safety net support system is provided. The system includes a plurality of support members having a material positioned there between to create a barrier between neighboring support members. The system further includes a pneumatic ancho...
|
