Document |
Document Title |
WO/2021/212345A1 |
Provided are an aircraft state management method, an aircraft state management apparatus, an aircraft state management system, a remote control terminal, and a storage medium. The aircraft state management method comprises the following ...
|
WO/2021/216407A1 |
Disclosed herein is a drone docking station for deposit of items/goods delivered by a drone to a secured receptacle. Items can be delivered to a receptacle at a curb, mailbox, post, porch, mobile units, and window for a multi-parcel rece...
|
WO/2021/216397A1 |
Disclosed herein is a drone docking station for deposit of items/goods delivered by a drone to a secured receptacle. Items can be delivered to a receptacle at a curb, mailbox, post, porch, in-ground vault, and window to a multi-parcel re...
|
WO/2021/217132A1 |
A vehicle escape ramp arresting system that includes a narrowed internal width and includes housing connection that limits the peak initial load that can be applied to a metal tape during a vehicle impact with a net and allows a housing ...
|
WO/2021/214401A1 |
The invention proposes a method for checking the tightening tension of at least one fastening bolt (114) for fastening at least two aeronautical parts, characterised in that it comprises the steps consisting in: mounting a centring devic...
|
WO/2021/210138A1 |
A take-off and landing facility (200) according to the present embodiment is where a flight vehicle (100) that is capable of autonomous flight lands. The take-off and landing facility (200) is provided with: a fence (201) that defines a ...
|
WO/2021/210985A1 |
A facility for subjecting a test object (3) to one or more electrostatically charged aerosol clouds (2; 2+, 2-), comprises one or more aerosol generators (1; 1b,1b; 100), each such generator comprising at least a steam inlet (7) and a hi...
|
WO/2021/210136A1 |
A landing facility (200) according to an embodiment of the present invention is a landing facility on which an aircraft (100) capable of autonomous flight lands. Provided are a landing platform (230) on which the aircraft lands, a landin...
|
WO/2021/211074A1 |
The present invention particularly relates to a carrier with movable fan blade holders (2) that can swivel independently in the vertical axis so as to carry and pile up the fan blades and mating parts to be removed from engines or to be ...
|
WO/2021/211283A1 |
The present invention is directed to multiple arrangements of a self-disengaging pitot tube cover, which can be triggered by a plurality of different environmental conditions while the cover admits to a plurality of different latching me...
|
WO/2021/211712A1 |
Aircraft handlers and related methods. The aircraft handlers include a plurality of undercarriage support assemblies. Each undercarriage support assembly includes a body, a translation assembly operably attached to the body, and a suppor...
|
WO/2021/205126A1 |
Removable closure member (50) configured to close a female portion (40) received in an external opening (16b) formed in the external surface (16) of a nacelle (10) for an aircraft engine, the female portion (40) comprising at least one a...
|
WO/2021/199117A1 |
Provided is a passenger boarding bridge capable of avoiding the mounting of a cab onto an aircraft due to the backward travel of traveling wheels. In an example, this passenger boarding bridge is provided with a rotunda (4) which is conn...
|
WO/2021/198073A1 |
The invention relates to a vehicle region comprising a roof section of a primary structure and two luggage compartments. One of the luggage compartments comprises a releasable luggage compartment hatch and a luggage compartment cover whi...
|
WO/2021/198964A1 |
An aircraft including a fuselage with one or more wings extending from the fuselage. The aircraft may include one or more apertures in a surface of at least one of the fuselage and the one or more wings. The one or more apertures may be ...
|
WO/2021/189518A1 |
An automatic charging device for an unmanned aerial vehicle, comprising a mounting base plate, a supporting column, a rotating platform, a rotating pillar, and a charging panel, wherein the mounting base plate is of a solid structure mad...
|
WO/2021/189101A1 |
Embodiments generally relate to systems, methods, and processes that may use touch-free document reading at self-service interaction stations. Some embodiments relate to a self service station for conducting a passenger interaction proce...
|
WO/2021/189099A1 |
Embodiments relate generally to systems, methods, and processes that may use touch-free interactions at self-service interaction stations. In particular, embodiments relate to use of such stations in transit environments, such as airport...
|
WO/2021/188085A1 |
This invention is related to a system used to facilitate the landing of unmanned aerial vehicles on any desired coordinates, and docking and retake-off of them.
|
WO/2021/188538A1 |
A maritime sulfur dioxide emissions switch monitoring system has an emissions sampling apparatus that is self-powered and requires a low power for operation. The emissions sampling apparatus has sensitive and selective chemical sensing t...
|
WO/2021/186106A1 |
A device for manufacturing a weave, comprising a winder (1) for reeling the manufactured weave to a rotating reel (14), wire spools (2) arranged to release longitudinal wires (6) to said winder (1), a wire spool carrier (3) comprising a ...
|
WO/2021/185761A1 |
The invention relates to a method for predicting the failure of an item of aircraft equipment, based on maintenance data collected during a plurality of flights of the aircraft, the method comprising: - a phase of generating a training s...
|
WO/2021/188353A1 |
A moveable wing gantry for servicing a wing of an aircraft is configured to be positioned around a wing of an aircraft to provide access to overwing and underwing surfaces of the wing of the aircraft. The wing gantry includes a service d...
|
WO/2021/184071A1 |
Embodiments relate generally to systems, methods, and processes that use thermal imaging at self-service interaction stations. In particular, embodiments may relate to a self-service station for conducting an interaction process, having ...
|
WO/2021/186940A1 |
A method of designing the airframe shape of a supersonic aircraft according to one aspect of the present technique involves: obtaining the equivalent cross-sectional area distribution of the initial shape of the airframe on the off-track...
|
WO/2021/183968A1 |
Described herein are systems and methods for baggage or parcel handling. The system (10) includes an automated bag unloading cell (26), a container roller deck (70) positioned in the automated unloading cell. The container roller deck in...
|
WO/2021/180561A1 |
The invention relates to a system for the ground power supply of aircraft (1), the system comprising at least one mobile transformer unit (4) which comprises a first chassis (15) and a voltage transformer (8) mounted on the first chassis...
|
WO/2021/183958A1 |
A system (10) for sequential loading of objects (14) into a container (18), the system comprising: a first robot (22) including an engaging end effector (40), the engaging end effector (40) operable to apply a vacuum force to engage an o...
|
WO/2021/181635A1 |
This status notification device 10 acquires face image data of an aircraft passenger 55 acquired at the arrival and departure airports 61, 62 of the aircraft, and acquires identification information and arrival destination information co...
|
WO/2021/176914A1 |
[Problem] To provide: a passive guidance mechanism that enables smooth guiding to a desired position; and a flying object landing system that enables smooth guiding to and landing at a desired position. [Solution] A pair of guide rails 2...
|
WO/2021/175417A1 |
Control system (1) for a cargo inspection system (2), said control system (1) comprising one or more first sensors (3) for determining the position and/or the shape and/or the size of a cargo item (5), which cargo item (5) is to be proce...
|
WO/2021/173065A1 |
Passenger bridge (100), comprising a proximal end (110), comprising a passenger passage opening (111); a distal end (120), comprising a bridge head (121); at least one first bridge segments (130), a proximal one (131) of which comprises,...
|
WO/2021/172367A1 |
A container deck 20 of a trailer 10 includes a central lift floor 40 that allows loading and unloading of a container 14 from the left and right of a vehicle body, a rear lift floor 60 that allows loading and unloading of the container 1...
|
WO/2021/173737A1 |
A drone docking port (DDP) mounted on a pole and having an openable and closable convertible top (CT), a docking plate having integrated battery wired or wireless recharging pads, and a control module. The control module (CM) is adapted ...
|
WO/2021/173450A1 |
Unmanned aerial vehicle (UAV) systems, including autonomous UAV operational containment systems, and associated systems, devices, and methods are disclosed herein. In one embodiment, a UAV operational containment system includes a cloud-...
|
WO/2021/165268A1 |
The invention relates to a method for manufacturing an aerodynamic structure (34) comprising a first panel (42) having an aerodynamic face (F34) as well as a second reinforced panel (44), characterised in that the manufacturing method co...
|
WO/2021/166610A1 |
The purpose of the present invention is to provide an aircraft landing guidance support system that is accurate and can be incorporated at a lower cost, and an aircraft landing integrated support system including the same, and to enable,...
|
WO/2021/167863A1 |
A gantry for servicing an aircraft is configured to be positioned adjacent an aircraft to provide access to a perimeter of the aircraft. A platform is moveably attached to the gantry and operable to move along the gantry between a lowere...
|
WO/2021/160402A1 |
Method for operating a passenger boarding bridge (7) of an airport (1), wherein operating the passenger boarding bridge (7) comprises the step of moving the passenger boarding bridge from a retracted position into a docking position or f...
|
WO/2021/160661A1 |
The invention relates to a versatile system for the secure handling of an aircraft (1) for vertical take-off and landing, which is provided with a skid-type landing gear comprising means (6) which form a motorized trolley for handling th...
|
WO/2021/157167A1 |
A crewless aircraft (10m) comprises: an airframe body (1912) having a first length (N1) in a first direction longer than a second length (N2) in a second direction orthogonal to the first direction; a plurality of propellers (22) that ro...
|
WO/2021/153445A1 |
The present invention provides a heat input reducing structure for an aircraft, an aircraft, and an aircraft manufacturing method with which, even if there is a limit to natural ventilation due to heat dissipation from a compartment in t...
|
WO/2021/152427A1 |
The invention is designed for the organization of landing of unmanned vertical take-off and landing aerial vehicles (UAV VTOL) on the landing platform of a ground station, (including) for the purposes of automatic servicing their payload...
|
WO/2021/152275A1 |
A device (500) for controlling the ground clearance of an airship (200), the airship being provided with two lateral anchoring points (212), said device comprising: a frame (502), on which a weight (504) is fixed; two (rigid) arms (506),...
|
WO/2021/148338A1 |
An apparatus attached near the tip end of a cantilevered aircraft wing for controlling the loads on the wing. The apparatus comprises a first body having a mass rotatable about a first axis by an actuator device; and a second body adjace...
|
WO/2021/149059A1 |
An aircraft management system and method of use are presented. The system comprises an application server, an application programming interface, a database and a graphical user interface. The interface comprises a dashboard and a plurali...
|
WO/2021/150759A1 |
The present application generally relates to aircraft water management. The disclosed system provides an initial step of verifying the amount of available water on board and dynamically regulating water usage during flight based on proje...
|
WO/2021/148520A1 |
The invention relates to a landing zone arrangement (1) for aircraft (19), in particular aircraft capable of vertical take-off, said arrangement comprising: a plurality of segments (3) which together form a landing zone in an operating s...
|
WO/2021/148774A1 |
An airframe or a part thereof 3, for example a skin assembly or a profile such as a structural profile, comprises: a wall W having an aperture A therethrough, wherein the wall W provides a frame F surrounding, at least in part, the apert...
|
WO/2021/150126A1 |
A mobile adjustable stairway which has a first frame section which is adapted to be mobile and has fixed steps and a second frame section coupled to the first frame section such that relative movement there between can take place whereby...
|