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WO/2017/221859A1 |
[Problem] The present invention addresses the problem that functional components for causing multiple moving bodies to operate in a coordinated manner have to be designed individually in conformity to functional components for causing th...
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WO/2017/208179A1 |
The present disclosure describes displaying on a flight deck (12) graphical presentations indicative of performance limitations of an aircraft (10) resulting from an in-flight aircraft reconfiguration. The graphical presentations are co-...
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WO/2017/191543A1 |
Systems, devices and methods for alerting a crew of an aircraft or other mobile platform of a relevant condition associated with the aircraft are disclosed. One exemplary method comprises receiving data indicative of an existence of the ...
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WO/2017/162862A1 |
The invention concerns an aircraft probe for resisting formation and propagation of ice comprising: • a base that is intended to be attached to an aircraft; • a housing extending from the base, said housing comprising: a body ext...
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WO/2017/138049A1 |
The control system (100) includes a flying body (10) and a base station (50). The base station is equipped with a light source unit which irradiates guide light of a predetermined wavelength. The flying body is equipped with: a propulsio...
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WO/2017/073241A1 |
Provided is a technique with which it is possible to measure the airspeed of a low-speed flight vehicle along a horizontal direction. An airspeed measurement system for a low-speed flight vehicle, wherein the airspeed measurement system ...
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WO/2017/055975A1 |
A method of and a system for presenting an operating status of an aircraft engine. The method comprises accessing a first indication indicative of a position of an aircraft engine start switch and accessing a second indication indicative...
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WO/2017/053913A1 |
A truss-reinforced radome crown structure (TRRCS) that functions in combination with an aircraft and a communication radome or antenna. The TRRCS maintains and protects a radome and antenna located on an aircraft's fuselage. The TRRCS in...
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WO/2017/021414A1 |
A display management system 10 is provided for displaying a graphical representation of flight envelope information of an aircraft. Included in the display management system is a control module 20 being coupled to the display management ...
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WO/2017/002055A2 |
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WO/2016/209225A1 |
Examples disclosed herein relate to control of a drone. In one example, aerial movement of the drone is controlled. In the example, it is determined, based on a plurality of devices, whether the drone is within a line- of-sight with at l...
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WO/2016/204843A2 |
Systems, apparatuses and methods for landing an unmanned aircraft on a mobile structure are presented. Sensors on the aircraft identify a predetermined landing area on a mobile structure. The aircraft monitors the sensor data to maintain...
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WO/2016/195816A2 |
An avionics display for rotorcraft provides a depiction of 360 degrees of terrain and obstacles about the rotorcraft using a top plan view at above a predetermined altitude that transitions to an angle perspective view as the altitude dr...
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WO/2016/190933A2 |
Vehicle navigation methods, systems and computer program products are provided that create a composite video image of a scene from video images of the scene generated by a plurality of video image sensors. The video image from each image...
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WO/2016/164624A1 |
A system for and method of indicating an angle of attack of an aircraft is provided. The system utilizes measurements from existing aircraft sensors so that a dedicated angle of attack sensor is not required. The system enables and benef...
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WO/2016/130716A2 |
A method of unmanned aerial vehicle (UAV) operation, including: receiving from a customer a first data request (400), the first data request (400) having: a first geographic coverage area, and a refresh rate for the first geographic cove...
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WO/2016/130721A2 |
A method of migrating unmanned aerial vehicle (UAV) operations between geographic survey areas, including: uploading a first plurality of flight missions (604) into a first UAV pod; deploying the UAV pod (606); autonomously launching the...
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WO/2016/125139A2 |
A device, system and method is provided for obtaining and processing turbulence data via communication devices located on-board airplanes. Turbulence data obtained by a plurality of communication devices may be received during flights on...
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WO/2016/105324A1 |
The group of inventions relates to means for enhancing vehicle safety. An autonomous modular device contains means for recording, controlling and reacting, signaling means, an electronic module, a cluster module, and at least one membran...
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WO/2016/084000A1 |
An auxiliary safety system for controlling the attitude of an aircraft (1) provides sensors placed on the aircraft (1) which identify stalling and/or other critical flying conditions that are imminent and/or have occurred, an electronic ...
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WO/2016/053452A1 |
A method of controlling noise of an aircraft includes storing a plurality of predefined noise modes; receiving a selection of a selected noise mode from the plurality of predefined noise modes, the selected noise mode identifying at leas...
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WO/2016/037035A1 |
An airspeed estimation system of an aircraft includes an electronic airspeed rate modeler unit configured to output an estimated airspeed rate signal indicating an estimated airspeed rate of the aircraft. The estimated airspeed rate sign...
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WO/2015/126513A2 |
Peripheral vision hover drift cueing methods, systems and computer readable media are disclosed. For example, a system can include one or more sensors, and a peripheral vision hover drift cueing controller coupled to the one or more sens...
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WO/2015/079155A1 |
The invention relates to a system (2) for generating non-propulsive energy in an aircraft, including: an auxiliary power unit (20) including a gas turbine (21) and a fuel cell (22); a pathway (23) for the intake of outside air into the a...
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WO/2015/059085A1 |
Air data sensing apparatus (10) comprising: an aircraft panel; a blister (12) arranged on a surface (8) of the aircraft panel, the blister (12) comprising an upstream portion (12a) and a downstream portion (12b), the upstream portion (12...
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WO/2014/168566A1 |
The invention relates to a distributed display device (40, 45, 50, 55) for a vehicle comprising a set of subsystems, wherein said display device comprises at least one operator station (10; 20; 30), comprising at least one display unit (...
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WO/2014/155446A1 |
The purpose of the invention is to suppress variations in brightness degradation in a display. A display device (1) according to the invention displays information using self-illuminating type display elements and is provided with a disp...
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WO/2014/136068A1 |
A method provides alert information, regarding an aircraft wheel braking system, to an operator of an aircraft during an aircraft landing. An input of a target deceleration rate for the landing aircraft is received prior to the aircraft ...
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WO/2014/133598A1 |
A method and apparatus for displaying an energy state (121) of an aircraft (100). The energy state of the aircraft is identified by a processor unit based on a speed (112) of the aircraft and an altitude (114) of the aircraft. An indicat...
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WO/2014/133250A1 |
The present invention relates to a brightness adjusting system for an illumination panel of an aircraft operation console, the system comprising: a controller for controlling voltage; a power IC for outputting power; a digital potentiome...
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WO/2014/081337A1 |
The invention relates to aviation technology. The system for depicting information for controlling an aircraft comprises an orientation sensor, making it possible to determine three angular coordinates of the position of a line of observ...
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WO/2014/047578A1 |
The flight of an aircraft is represented in terms of Earth-based reference system data for a first position and a second position of the aircraft that are separated by a time increment. A centripetal acceleration of the aircraft is deter...
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WO/2014/023989A1 |
The present disclosure relates to a checklist display system (100), a method, a graphical interface (120) and a computer program product. The checklist display system, method, graphical interface and computer program product display in a...
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WO/2013/144157A1 |
The invention relates to a method for determining a credibility state of measurements from an incidence sensor of an aircraft, including at least one test (90, 100) of the consistency between the incidence measurements from said sensor a...
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WO/2013/144126A2 |
This method for determining a state of credibility of measurements made by static and total pressure sensors and incidence sensors of an aircraft comprises the following steps: - determining (31) a speed of the aircraft, from static and ...
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WO/2013/045861A1 |
The present invention relates to a novel design of the front portion of an aircraft cockpit. The invention provides a viewing device which comprises a screen pivotably mounted on a mounting that allows height adjustment. The invention al...
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WO/2012/161608A1 |
The group of inventions relates to aircraft and watercraft, and also to signalling devices. The method for preventing flow separation over the wing of an aerohydrodynamic device consists in that, during movement of the wing, a wing part ...
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WO/2012/148232A2 |
The present invention relates to an aircraft, and more specifically, to an aircraft instrument display system which automatically recognizes the facial image of a pilot to verify the identity of the pilot, and then displays and memorizes...
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WO/2012/112090A1 |
The invention pertains to a display method, a computer program for performing steps of the display method and a display system. The display system (1) comprising: display means (2) comprising: a physical display unit (13)operable to disp...
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WO/2012/107613A1 |
An aeronautical safety device having a casing with a first light indicator (1) to indicate landing or take off permission, with a second light indicator (2) to indicate if the cabin is ready, with first light indicator operating/repositi...
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WO/2012/095605A1 |
The invention relates to an overhead panel capable of being arranged in an aircraft cockpit, which includes a set of independent sub-modules (67) each associated with a specific system or a specific function of the aircraft, built into a...
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WO/2012/091819A1 |
According to one embodiment, a center pedestal display (10) includes a plurality of mounting faces (352) and a high - resolution screen (310). The plurality of mounting faces (352a) include a first mounting face that is substantially par...
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WO/2012/080280A1 |
The general field of the invention is that of aircraft cockpit display systems requiring enhanced alertness for certain nighttime missions or flights. The system according to the invention comprises strictly blue-colored lighting means: ...
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WO/2012/047846A1 |
A system (1) for monitoring aerodynamic flow conditions over an aerodynamic member is provided. The system (1) includes a cantilevered arm (16) having a first conductive lead (18) configured for movement relative to a second conductive l...
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WO/2012/025695A1 |
The invention relates to a bracket (4, 6) for display devices (8a) for an aircraft cockpit (2), such as an instrument panel or glare shield, comprising a panel including a core (10) having a cellular structure and two skins (12) covering...
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WO/2012/022891A1 |
The invention belongs to the field of the installation of systems in aircraft. More specifically, the invention relates to the installation of avionics furniture, electrical master boxes and IFE bays. Compared with the arrangements known...
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WO/2012/010496A1 |
The invention relates to a monitoring device (30) for a repair patch (10) that can be placed on or in a wall of an aircraft for repairing a defect, having a sensor device (36) for capturing properties of the repair patch (10) placed in t...
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WO/2011/154249A1 |
The invention relates to a method and device for protecting an aircraft during the flight phase, the aircraft having a plurality of slat and flap configurations. The method comprises the following steps: determining (201), for at least o...
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WO/2011/114278A2 |
The application discloses an aeronautical input/output device (70) for flight task management which comprises a display unit (90) with a housing (97), and a keyboard unit (91) which is adapted to communicate with the display unit (90). T...
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WO/2011/064263A2 |
The invention relates to a structural element made of a layered composite material in the form of an elongate profile section and comprising, in a thickness of the layering, three cores consisting of an electrically conductive material c...
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