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Matches 1 - 50 out of 7,873

Document Document Title
WO/2019/072417A1
The aim of the invention is to achieve, by means of suitable design measures in connection with the electronics, a simple construction and mounting technology that ensures an economically efficient and robust product. This aim is achieve...  
WO/2017/162526A8
Method for managing and maintaining an aircraft (10) comprising an area with a high degree of security, a human machine interface of the aircraft being included in the area with a high degree of security and necessary for a maintenance o...  
WO/2019/071344A1
Apparatus and methods for assisting a flight crew with (e.g., pre-flight) functional testing of aircraft systems are disclosed. An aircraft condition can be used to select one or more functional tests that are applicable based on the air...  
WO/2019/071293A1
In an aspect there are disclosed examples systems (10, 110) for the landing and handling of a drone (1), the system (10, 100) may include a moveable platform (16, 116) on which the drone (1) is supportable in a landed state; a space (14,...  
WO/2019/069501A1
Provided are an aircraft soundness diagnostic device and an aircraft soundness diagnostic method that enable diagnosis of detachment and the progress or the like of detachment of an adhered structure in the body of an aircraft. An aircra...  
WO/2019/069057A1
An apparatus (1) for changing a power source of a drone, the apparatus (1) comprises an adaptor (2) for securing a power source (3) to a drone and comprising a first energy connection for supplying energy from the power source (3) and a ...  
WO/2019/068189A1
A lighting assembly for an aircraft includes a visible light source generating visible light and an ultraviolet light source generating ultraviolet light. The visible light source is disposed adjacent to the ultraviolet light source. The...  
WO/2019/070735A2
A tether guide system operable through a wide range of tether/fleeting angles while causing minimal wear to the tether. The tether guide system may include a series of rollers arranged in a curved path. Also disclosed are tether guides w...  
WO/2019/061776A1
An unmanned aerial vehicle test method and an unmanned aerial vehicle test apparatus, which relate to the technical field of unmanned aerial vehicles. The unmanned aerial vehicle test method is used for implementing impact testing on an ...  
WO/2019/064636A1
An operation management device acquires from a mobile terminal through a mobile phone line: a subscriber ID identifying a subscriber to a service relating to a use of the mobile phone line; position information that the mobile terminal h...  
WO/2019/058598A1
According to the present invention, a flying apparatus is provided with: an acquisition unit which acquires a planned flight time/date, a flight start-location, and a flight end-location; a specification unit which specifies a plurality ...  
WO/2019/060575A1
A cupola fairing (250) for reducing drag and increasing lift on an aircraft fuselage (210) and wings (220). The fairing includes a housing length extending along a longitudinal axis, and a variable width extending normal to the longitudi...  
WO/2019/060079A1
A wireless power initiated test system (100) can use an aircraft controller (160) to automatically initiate a test sequence to determine status of systems of the aircraft (101), based on the detection of receipt of the wireless power at ...  
WO/2019/025653A3
The invention relates to temperature control equipment for inside aircraft or similar, comprising a closed-cycle cooling circuit, said circuit including compression means, a condensation/evaporation exchanger, an expansion valve and an e...  
WO/2019/057346A1
Automated baggage handling facility at an airport site for handling and delivering said baggage, the baggage being transported along routes from a collection point to a delivery point. Baggage transportation is carried out by means of a ...  
WO/2019/052675A1
Demounting aid (2) for demounting a hoisting fitting (3) from a workpiece (4), preferably from an aircraft structural component, comprising a first connector (5) and a second connector (6), a force measurement device (7) for measuring th...  
WO/2019/055722A1
One variation of a tram system includes: a chassis; a latch configured to selectively engage a latch receiver mounted to an aircraft; an alignment feature adjacent the latch and configured to engage an alignment receiver mounted to the a...  
WO/2019/054027A1
An acquiring unit of the present invention acquires a flight plan containing first flight conditions. A setting unit sets a risk level for airspace in which an aircraft is flying. A determining unit determines second flight conditions. A...  
WO/2019/055702A1
Disclosed are transportable unmanned aerial vehicle (UAV) facilities. The facilities comprise a housing for holding a UAV, where the housing defines a landing area for the UAV. The facilities also comprise a structure for reducing wind s...  
WO/2019/051604A1
Systems and methods for a heat exchange system used to heat or cool a space. The system includes an airflow source for providing an airflow and at least one conduit that defines an airflow path for receiving the airflow. The system furth...  
WO/2019/055685A1
Disclosed are unmanned aerial vehicle (UAV) positioning mechanisms for moving a UAV across a surface. The positioning mechanisms comprise a first guide assembly arranged opposite to a second guide assembly. A drive system is arranged to ...  
WO/2019/056009A1
A pitot tube cover (10,120) for a pitot tube (100) operable to determine a speed of an aircraft based on an airstream impinging on the pitot tube (100). The pitot tube cover (10,120) has a body (12,122) and a sail (14) extending from the...  
WO/2019/054028A1
An acquisition unit acquires, by communicating with a server device, a flight plan that states a first flight condition. A state determination unit determines the state of communication. A condition determination unit determines a second...  
WO/2019/048896A1
The present invention relates to an aircraft stand baggage delivery system (1) for delivery baggage to an aircraft stand (10) comprising a medium duty underground transportation network (100) for the transportation of unit load devices (...  
WO/2019/047394A1
A device and a method for integrating hole drilling and interference-fit bolt insertion. The device comprises: a station conversion module (1), a spindle module (2) and a bolt-insertion module (3); the station conversion module (1) compr...  
WO/2019/048874A1
A system for handling an aircraft on a nautical vessel includes a plurality of winches each associated with a corresponding one of a plurality of electromotors and a plurality of cables associated with the plurality of winches. Each of t...  
WO/2019/043306A1
Method for circulating fuel in a filling line (2) of a tank of an aircraft. The method according to the invention involves automatically and mechanically varying the cross-section for passage of the fuel until the fuel reaches a threshol...  
WO/2019/042504A1
The invention relates to a carriage (101) for transporting and positioning an aircraft component, in particular a fuselage partial segment, comprising a chassis (102) and a first aircraft component holder (103) arranged on the chassis, w...  
WO/2019/039171A1
This tire management system for aeroplanes is provided with: a management device (40) with which a tire manufacturer (10), a maintenance repair overhaul (MRO) provision company (20), and an airline company (30) can communicate over a net...  
WO/2019/039988A1
An aircraft cleaning robot comprises a robot arm (14); a brush (34) rotatably attached to the robot arm (14) to be rotated about a brush rotation axis (R); and a controller (56) configured to control the position of the cleaning head (32...  
WO/2019/035011A1
An airfield light includes a light assembly mounted on a base (26) and a transparent cover (30) disposed over the light assembly and secured to the base. The light assembly includes a curved LED (light emitting diode) assembly having a c...  
WO/2019/035080A1
A system and method for distributing power to racing aircraft systems is provided. The system includes a race course, a power transmitter directed towards a power delivery section of the race course, the power transmitter configured to r...  
WO/2019/030116A1
The invention relates to a safety system for an unmanned flying object (1), flown by a user on the ground, the safety system making it possible to reduce the risks of the flying object (1) falling in the event of failure. The safety syst...  
WO/2019/030303A1
A system and a manner of handling luggage items, such as in an airport, where the luggage items are stored in a plurality of buffers, where the luggage items of one buffer are provided into one container which is configured for loading i...  
WO/2019/025653A2
The invention relates to temperature control equipment for inside aircraft or similar, comprising a closed-cycle cooling circuit, said circuit including compression means, a condensation/evaporation exchanger, an expansion valve and an e...  
WO/2019/025251A1
Device for providing utilities to an aircraft on the ground, comprising an electrical unit suitable for delivering AC electric current at a frequency of 400 Hz to an aircraft on the ground and a module for supplying preconditioned air, w...  
WO/2019/027371A1
According to various embodiments, there is provided a method for facilitating movement of a deadload during ramp operations comprising: identifying a current location of a deadload; identifying a desired location of the deadload; and hig...  
WO/2019/020158A1
What is proposed is a ground handling facility (1) for passenger-transporting aircraft (100), in particular vertical takeoff and landing multicopters, comprising: at least one first platform (2) which is designed as a landing platform (2...  
WO/2019/020162A1
The invention relates to take-off/landing equipment (1) for passenger (P, P')-carrying aircraft (100), in particular vertically taking-off and landing multicopters, comprising: at least one platform (2, 2') configured as a landing platfo...  
WO/2019/020227A1
The invention relates to a processing system for aircraft structural components (2), having a processing station (3) comprising a clamping frame (4) for receiving each particular aircraft structural component (2) to be processed, wherein...  
WO/2019/021084A1
The invention relates to a device for deflecting and decelerating a flow, comprising a deflecting surface, a support structure connected behind the deflecting surface and a vortex generator connected on the deflecting surface. The vortex...  
WO/2019/021538A1
An ultrasonic-inspection-system manufacturing method according to an embodiment comprises a step for creating ultrasonic-inspection-system design information including ultrasonic sensor and ultrasonic transducer counts, positions, and or...  
WO/2019/022636A1
The invention relates to airfield equipment. An aircraft short takeoff method includes fueling a launcher and mechanically connecting an aircraft and a launcher. The horizontal component of mechanical loads is transferred from the launch...  
WO/2019/019152A1
A reliability testing method and device for a cradle head, the reliability testing method for a cradle head comprising: inputting a control parameter such that the cradle head adjusts posture according to the control parameter (S202); ac...  
WO/2019/020226A1
The invention relates to a machining facility for aircraft structural components (2), comprising a machining station (3) having a mounting frame (4) for receiving each aircraft structural component (2) to be machined, the mounting frame ...  
WO/2019/020228A1
The invention relates to a machining system for aircraft structural components (2), having a machining station (3), which comprises a clamping frame (4) for holding the aircraft structural component (2) to be machined, the clamping frame...  
WO/2019/023512A1
Disclosed is a collapsible heated elastomeric bladder tool (100) for repairing damage to composite structures. The elastomeric bladder tool can be used to repair composite structures in difficult to reach areas, such as under stringers (...  
WO/2019/018857A1
Provided is a system including a platform to receive unmanned air vehicles (UAVs) thereon for launching and retrieving the UAVs. The system can include a pair of gantry arms that move to any location along the platform to position a UAV ...  
WO/2019/010581A1
In an aspect, a test platform for testing an embedded control system having a plurality of interconnected components is operable to: receive, at run time, configuration data for configuring a system under test ("SUT") representing the em...  
WO/2019/012298A1
Methods for drone-assisted inspection of aircraft and other large, mobile structures are disclosed. The drone's camera identifies the mobile structure to be inspected and an inspection routine for a portion of the mobile structure is sel...  

Matches 1 - 50 out of 7,873