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WO/2023/095022A1 |
In an aircraft component where the aircraft component comprises a metal sheet (1.1, 1.2, 1.3, 1.4, 1.5, 1.6), the metal sheet (1.1, 1.2, 1.3, 1.4, 1.5, 1.6) comprises a normal region (5.1, 5.2, 5.3, 5.4) and a first surface milling regio...
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WO/2023/092174A1 |
The present invention relates to a conveyor controlling apparatus and a conveyor controlling method for controlling a conveyor in accordance with environment parameters with respect to the conveyor. The conveyor controlling apparatus (Ba...
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WO/2023/091991A1 |
A system, method and apparatus are proposed to assist in assembling the frame, attaching the skin, and performing other tasks in manufacturing an airship and constructing other structures that are otherwise challenging, inefficient, or u...
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WO/2023/091132A1 |
Features for in-flight recovery of an unmanned aerial vehicle (UAV). A towline may be deployed by a host aircraft in-flight to recover an in-flight target UAV. The towline or portion thereof may be oriented nearly vertical. The towline m...
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WO/2023/091114A1 |
The present invention relates to a body (2) located at an air vehicle; at least one control stick (3) extending outward from the body (2) and enabling the pilot to control tasks such as position and speed of the air vehicle; at least one...
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WO/2023/089532A1 |
An automated container (1 ) for receiving objects (0), in particular parcels or the like, delivered by means of aerial vehicles (Va), in particular by means of drones (D). Said automated container (1 ) comprises a box-like structure (2) ...
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WO/2023/090209A1 |
The purpose of the present invention is to suppress the occurrence of biases in ground support equipment to be used and to reduce working time when allocating ground support equipment in an airport. An automatic allocation system 10 comp...
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WO/2023/091133A1 |
Features for in-flight recovery of an unmanned aerial vehicle (UAV). A towline may be deployed by a host aircraft in-flight to recover an in-flight target UAV. The towline or portion thereof may be oriented nearly vertical. The towline m...
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WO/2023/091788A1 |
The methods and systems provide for increasing the accuracy of aircraft (1) weight and center of gravity determination through the use of filtered strut pressure measurements. Aircraft (1) vertical and horizontal accelerations are determ...
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WO/2023/085198A1 |
The present invention provides a blade in which the specific rigidity of a flap part is further increased. This blade has a thick body part and a thin flap part integrally formed in the rear end of the body part. The flap part has a skin...
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WO/2023/084018A1 |
The security inspection system according to the invention consists substantially of • a luggage loading region for loading luggage of a person into at least one load carrier, • a luggage inspection station for an imaging examination ...
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WO/2023/084019A1 |
The invention relates to a security inspection system substantially consisting of • a baggage delivery area (1) having one or more delivery stations (1a, 1b, 1c) for delivering baggage belonging to a person into a load carrier (2), •...
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WO/2023/083990A1 |
An aerodrome structure comprising a core and a peripheral portion, wherein the peripheral portion is radially outside the core. The core comprises an upstanding structure, a platform located within the upstanding structure and a lift mec...
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WO/2023/084017A1 |
The invention relates to a follow-up inspection region of a security inspection system, comprising at least one follow-up inspection station accessible from two sides for the manual follow-up inspection of luggage objected to in a luggag...
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WO/2023/086757A1 |
In an aspect, a method for monitoring recurrent aircraft faults is disclosed. The method comprises (a) retrieving a plurality of data entries from an aircraft. The plurality of data entries may comprise semantic information about a plura...
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WO/2023/083901A1 |
The invention relates, according to one aspect, to a method for monitoring the configuration of an aircraft engine (300) comprising a plurality of pieces of equipment (301) each having a radio-identification device (3010) associated with...
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WO/2023/084167A1 |
The invention relates to a platform (28) for the take-off and landing of an aircraft (12) for generating electric power by means of a generator (24) and comprising: - a stationary support (30); - a receiving structure (32) that is intend...
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WO/2023/077855A1 |
An unmanned aerial vehicle electrostatic spraying test platform, comprising a test platform supporting movable frame (1), a sliding guide rail device (2), a fixed plate (3), an unmanned aerial vehicle flight angle adjustment device (4), ...
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WO/2023/079225A1 |
The invention relates to a method for producing a fibrous preform for part of a blade or propeller of a turbomachine, comprising at least one attachment root extended by a portion for mounting an airfoil, the method comprising at least t...
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WO/2023/081042A1 |
The present disclosure provides a ground support equipment for servicing an aircraft on the ground. The ground support equipment comprises a pre-conditioned air, PCA, unit configured to provide pre-conditioned air to an aircraft on the g...
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WO/2023/074357A1 |
This power supply device is for an unmanned mobile body. The power supply device has a drive mechanism and control unit. The drive mechanism moves on water. The control unit controls the drive mechanism so that a positional relationship ...
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WO/2023/076056A1 |
The present disclosure provides a preconditioned air (PCA) unit for supplying preconditioned air to an aircraft parked on the ground. The PCA unit comprises an air duct with an air inlet and an air outlet connectable to a hose for convey...
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WO/2023/073710A1 |
Stowing systems and methods to disassemble, store, and/or protect an aircraft, and in particular a VTOL aircraft, for transportation along standard public roadways. A stowing system attaches to the aircraft in a flight- ready state, and ...
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WO/2023/067005A1 |
The invention relates to a device (1) for handling and transferring an aircraft engine (2) having a receiving cradle (10) comprising at least two holding elements (30), and at least three support modules (20) suitable for supporting the ...
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WO/2023/066934A1 |
The present invention relates to a thermal protection system (10) for an aircraft comprising a cockpit, the cockpit comprising a plurality of transparent surfaces (12, 14, 16), at least two transparent surfaces (14) being openable. The p...
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WO/2023/067289A1 |
The invention relates to a method for mounting an axle (12) in a bore (14) of a bogie (16) mounted on an aircraft landing gear (18), the landing gear (18) being in a gear-down position, the bore (14) extending in a substantially horizont...
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WO/2023/067010A1 |
The invention relates to a method and a system for determining the temperature in a mounted aircraft tyre. The system is characterized in that it comprises two temperature sensors installed inside the tyre.
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WO/2023/060326A1 |
The present application to a utility model pertains to the sector of devices and accessories for operating unmanned aerial vehicles, more specifically those designated as "drones"; the solution provides an extremely versatile platform en...
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WO/2023/060712A1 |
The present invention relates to the technical field of aircraft deicing, and in particular, to a novel steam jet multifunctional aircraft deicing vehicle, comprising a vehicle body. A steam generation assembly is provided in the vehicle...
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WO/2023/062439A1 |
The present disclosure relates to conveyance means for aerial vehicles, and discloses a cable-powered conveyance system (100) for an aerial vehicle. The system (100) comprises a structure (20) defined by a plurality of columns having ele...
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WO/2023/064713A1 |
An aircraft skin coating assembly for an aircraft. The coating assembly includes a primer layer (34) deposited on the aircraft skin (32), an optical stop-etch layer (52) deposited on the primer layer (34) that is reflective at a predeter...
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WO/2023/063680A1 |
A catapult is disclosed. The catapult according to an embodiment of the present invention, comprises: a take-off assisting member contacting an aircraft to push the aircraft; a power source coupled to the take-off assisting member to dri...
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WO/2023/059650A1 |
Methods and systems for testing an aircraft in-flight are described herein. The method can include receiving a test deck including one or more test cards, with an individual test card including an ordered list of points. For an individua...
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WO/2023/057377A1 |
The present invention relates to a method for manufacturing a connection part (10) between a wing box (20) and a leading edge module (30). The method comprises the steps of carrying out a three-dimensional digitization of a first part re...
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WO/2023/058329A1 |
Provided is a wall surface work device 1 comprising: a travelling body 2 which can travel with respect to a wall surface W; an ascending/descending support device 3 which is provided with support columns 3a that are installed to the left...
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WO/2023/056516A1 |
A drone system and method for deploying and autonomously refuelling. The drone system includes a base station and a drone. The base station and drone are configured for autonomous refuelling when the drone has landed in the base station....
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WO/2023/057450A1 |
An aerodrome structure (10) comprising a plurality of modules including a plurality of lift structure modules (100), each lift structure module of the plurality of lift structure modules comprising an upstanding structure (130); a platfo...
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WO/2023/055550A1 |
An air hose, the air hose comprising a first component and a second, elastic component. The second component is fastened to the first component at a plurality of fastening positions along the axial direction of the air hose. The air hose...
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WO/2023/055325A1 |
The present invention relates to a body (2) located on an air vehicle; at least one useful load (F) located on the body (2); at least one launcher (3) located on the body (2), which enables the launch and/or release of the useful loads (...
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WO/2023/055878A1 |
A smart landing platform system includes a flat and rigid platform for landing a drone and having a geometrical center, a center of gravity and a weight, a digital scale disposed beneath the platform for providing measurements of a weigh...
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WO/2023/045498A1 |
The present disclosure relates to an unmanned aerial vehicle (UAV) landing platform and a UAV landing system. The UAV landing platform comprises: a positioning board, which is provided with an identification code for a UAV to identify a ...
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WO/2023/047025A1 |
A system (1) for docking an airship (2) on a receiving structure (3) comprising at least one unmanned aerial vehicle (4) that can be controlled so as to move between the airship (2) and the receiving structure (3), carrying a first end (...
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WO/2020/206473A9 |
A system for recovering an aircraft, having at least one recovery dolly (4) which has a transport surface (7) for receiving an undercarriage (3) of the aircraft, wherein the system comprises at least one axle-lifting device (1), at least...
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WO/2023/043414A1 |
The invention relates to a test assembly (10) for testing the performance of said thrust system components (27), comprising a body (1) connected with the thrust system components (27); at least one detector unit (18) for measuring the ph...
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WO/2023/042067A1 |
The present invention concerns an apparatus (100) for non-destructive inspection of structural elements (10) having a wing profile, comprising a base (20), a positioning module (300) associated with the base (20) in correspondence with i...
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WO/2023/041677A1 |
The invention relates to a mobile structure for dispatching and accommodating drones, comprising a landing platform, a lifting unit for adjusting the height of the landing platform, and a storage unit. The lifting unit allows lifting and...
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WO/2023/041679A1 |
The invention relates to a landing platform for a drone (6), comprising a landing surface comprising two conveyor belts (2) which are arranged parallel in the same horizontal plane and which are spaced apart such that a drone (6) standin...
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WO/2023/035342A1 |
A cam type airplane cabin door load simulation device and simulation method. The device comprises n cam groups, an input shaft (7), 3n couplers (8), and a friction disc (41) load device; the n cam groups and the friction disc (41) load d...
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WO/2023/036202A1 |
The present invention relates to the technical field of airport ground equipment, in particular to an automatic leveling device for a conveying platform, and a loader. The automatic leveling device for a conveying platform comprises a ma...
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WO/2023/033228A1 |
A drone control system for forest fire monitoring is provided. A drone control system for forest fire monitoring, according to an embodiment of the present invention, comprises: a base station which is disposed in at least one position o...
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