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Patent Searching and Data


Matches 151 - 200 out of 1,555

Document Document Title
WO/2011/070536A3
The application provides a component flight-hour updating module (10) of an aircraft. The module comprises at least one Radio Frequency Identifier (RFID) tag (16; 54) being attached to at least one component (15) and a component flight-h...  
WO/2011/067419A1
Digital recording and replay system (100) for an aircraft, comprising a Mission Computer (MC) with an Operational Flight Program (OFP) for generating instrument data (ID) for onboard instruments of the aircraft; a Mission Data Recorder (...  
WO/2011/066920A1
The invention relates to an information display device (2) comprising a first processing unit (6.1) and a second processing unit (6.2) connected to at least one information source (3, 4, 5), the first processing unit being further connec...  
WO/2011/053552A1
A method and system for displaying three dimensional images of runways and terrain, as well as additional information, on one or more screens of an avionics display system is provided. The system merges elevation information for terrain ...  
WO/2011/027357A3
A system and method for dynamically computing an equi-distance point (EDP) for aircrafts is disclosed. In one embodiment, a method for dynamically computing an EDP for an aircraft includes receiving at least two reference points for land...  
WO/2011/015752A1
The invention relates to a digital display device (10), comprising a display (12) for a scene (14), a means for displaying a virtual tool (18) for selecting at least one point (20) of the scene (14), and a touch-sensitive means for contr...  
WO/2011/012156A1
An aircraft avionics system (10) for an aircraft, comprising a mission system (2), controlled by an open systems mission computer (OSMC) with a tactical communications system (320) and a tactical navigation system (220); a civil system (...  
WO/2011/012102A1
The invention relates to a method for producing a sensor-supported, synthetic vision for landing support of helicopters (H) under brown-out or white-out conditions, wherein a virtual 3-D representation of the intended landing zone (L) is...  
WO/2010/132133A1
A display system for a parachutist is provided based on navigation data and calculations of locations where the parachutist should steer the parachute to increase likelihood of reaching a target. A two-dimensional representation of a nav...  
WO/2010/132133A4
A display system for a parachutist is provided based on navigation data and calculations of locations where the parachutist should steer the parachute to increase likelihood of reaching a target. A two-dimensional representation of a nav...  
WO/2010/132133A9
A display system for a parachutist is provided based on navigation data and calculations of locations where the parachutist should steer the parachute to increase likelihood of reaching a target. A two-dimensional representation of a nav...  
WO/2010/112877A3
A device for indicating a direction or axis in three dimensions to a user, comprises an indicator member (10, 11) configured to indicate a direction in any three dimensional direction,- a static member (12) for mounting the indicator mem...  
WO/2010/080656A1
A monitoring system is disclosed for use with a mobile platform being operated by an operator. The system may make use of a database for containing operational information and procedures relating to the operation of the mobile platform b...  
WO/2010/063821A1
A navigational database (BD) includes: a first set of elements that includes airports, tags, and waypoints; a second set of elements that includes procedures; and a third set of elements that includes routes. The method is characterized ...  
WO/2010/060792A1
The invention relates to a navigation assistance instrument for an aircraft pilot, including: a first display means (R3) extending horizontally, the centre of the display means marking the longitudinal axis (X) of the aircraft; a mobile ...  
WO/2010/059570A1
In one embodiment, a method for aligning a vehicle includes providing an optical instrument, mounted in the vehicle, the optical instrument providing an image viewable from the vehicle's standard operating position by an operator and the...  
WO/2010/056508A1
A method and system for a required time of arrival (RTA) performance graphic display is provided. The system includes a processor programmed to receive a required time of arrival and a first visual display communicatively coupled to the ...  
WO/2010/027620A3
A flight data recorder includes an enclosure and electronic interface within the enclosure. The electronic interface is coupled for receiving data. A crash survivable memory unit is disposed within the enclosure. The crash survivable mem...  
WO/2010/027620A2
A flight data recorder includes an enclosure and electronic interface within the enclosure. The electronic interface is coupled for receiving data. A crash survivable memory unit is disposed within the enclosure. The crash survivable mem...  
WO/2010/020751A2
A visual aid for the pilot of an aircraft approaching to land on an aircraft carrier comprises a series of lights (9) embedded along the landing deck and controlled in response to pitch and heave of the vessel so that the light(s) illumi...  
WO/2010/003824A2
The invention relates to an autonomous system for determining information representative of the movement of an articulated chain (CA_1, CA_2, CA_3) comprising at least two solid elements (ES1_1, ES2_1, ES1_2, ES2_2, ES3_2, ES1_3, ES2_3, ...  
WO/2010/001402A1
A number of apparatuses are provided, for sensing and/or emitting energy along one or more desired apparatus line of sights (LOS) with respect to the respective apparatus. In at least one embodiment, the apparatus includes an assembly th...  
WO/2009/155176A2
A flight recorder includes an enclosure having a notch formed on one side or corner of the enclosure. An electronic interface is disposed within the enclosure. The electronic interface is coupled for receiving flight data, video data, an...  
WO/2009/155176A3
A flight recorder includes an enclosure having a notch formed on one side or corner of the enclosure. An electronic interface is disposed within the enclosure. The electronic interface is coupled for receiving flight data, video data, an...  
WO/2009/141519A8
Device for aiding the navigation and guidance of an aircraft, and system comprising such a device. The device (1) comprises at least three independent channels and it comprises at least one computer (2) which contains means (4) for stori...  
WO/2009/141519A2
Device for aiding the navigation and guidance of an aircraft, and system comprising such a device. The device (1) comprises at least three independent channels and it comprises at least one computer (2) which contains means (4) for stori...  
WO/2009/141519A3
Device for aiding the navigation and guidance of an aircraft, and system comprising such a device. The device (1) comprises at least three independent channels and it comprises at least one computer (2) which contains means (4) for stori...  
WO/2009/138989A3
Apparatus for forward looking terrain avoidance (FLTA) in an aircraft, including a processor and at least one sensor, each sensor being coupled with the processor, the processor for executing at least one neural network based algorithm, ...  
WO/2009/134556A2
Techniques for representing a holding pattern on a vertical situation display are described. The vertical situation display has a first screen area to depict the holding pattern and second screen area to show a flight path after the hold...  
WO/2009/134556A3
Techniques for representing a holding pattern on a vertical situation display are described. The vertical situation display has a first screen area to depict the holding pattern and second screen area to show a flight path after the hold...  
WO/2009/118566A1
Operational data (214), such as data that is used to generate aircraft Head Down Displays, is recorded using a first type of processor (120) located onboard a vehicle. The system converts the operational data so that it is useable remote...  
WO/2009/081177A2
An aircraft (160) approaches a landing point (162) following a flight path (164) to a designation point (166), thepilot sightsthe landing point (162) and activates the apparatus. A first calculation ofcoordinates for the landing point (1...  
WO/2009/081177A3
An aircraft (160) approaches a landing point (162) following a flight path (164) to a designation point (166), thepilot sightsthe landing point (162) and activates the apparatus. A first calculation ofcoordinates for the landing point (1...  
WO/2009/059932A1
A display module for displaying passenger-specific display information in an aircraft, said module comprising: a display unit, a controller, a memory, and a first interface, said first interface being connected to said controller, and sa...  
WO/2009/058442A1
A computer implemented method, apparatus, and computer usable program product for cross checking required navigation performance procedures. A required navigation performance procedure in a flight management system is executed in an airc...  
WO/2009/058784A1
A method and system for determining right of way for a plurality of mobile units at an intersection. The method and system include collecting position and movement information about the plurality of mobile units approaching the intersect...  
WO/2009/057292A1
A travel data acquisition terminal (20) transmits travel data on a particular vehicle to a travel data processing server (30). The travel data processing server (30) receives the travel data and stores it in a travel data storage unit (3...  
WO/2009/053556A1
The invention relates to a device (1) for transmitting to a user system (3) geographical data that is stored, using a unit-surface sorting, in the database (4) of a provider system (2).  
WO/2009/053964A2
A method for presenting an advised action for recovering an aircraft from an unusual flight attitude, the method including the procedures of: retrieving real-time flight parameters; retrieving aircraft aerodynamic characteristics; determ...  
WO/2009/053964A3
A method for presenting an advised action for recovering an aircraft from an unusual flight attitude, the method including the procedures of: retrieving real-time flight parameters; retrieving aircraft aerodynamic characteristics; determ...  
WO/2009/050393A3
The invention relates to a crossed monitoring device for a head-up display (500-1) that can be used for displaying the representation of at least one first datum. The device includes means (505-1) for generating at least one image from s...  
WO/2009/050393A2
The invention relates to a crossed monitoring device for a head-up display (500-1) that can be used for displaying the representation of at least one first datum. The device includes means (505-1) for generating at least one image from s...  
WO/2009/052404A1
Hybrid-heuristic optimization of competing portfolios of flight paths for flights through one or more sectors of an airspace represented by an air traffic system. In one embodiment, a hybrid-heuristic optimization process includes one or...  
WO/2009/043806A1
The invention relates to a backup instrument (4) that can be fitted in the dashboard of an aircraft. The backup instrument (4) includes means (11, 25, 28) for calculating and displaying backup flight information from backup signals provi...  
WO/2009/037248A1
The invention generally pertains to the field of display devices for managing systems comprising at least a means for generating and displaying information about the system and a designator. The devices of the invention are such that: th...  
WO/2009/037083A1
The general field of the invention is that of viewing devices used for managing complex systems. The viewing device comprises the following functionalities: - the information of one and the same type is disposed in a given plane (L1, L2 ...  
WO/2009/033940A1
The invention relates to a method of managing an anti-collision system for an aircraft, said system comprising means for detecting collision with a threat and at least one Head-Up viewing device. The symbology comprises two display modes...  
WO/2009/032091A1
An instrument mounting device includes a first component having a flexible band configured to clamp about an instrument for mounting within an instrument panel. A second component is configured to couple with the first component and incl...  
WO/2009/027498A1
The invention pertains to the field of displaying, onboard an aircraft, geostationary members of the navigation database onto a screen having different display resolutions for data display, and relates to a method for simplifying the dis...  
WO/2009/022080A1
The invention relates to a data processing and display system that comprises processing and display means adapted for displaying, from a more secured domain (A) and on a same screen (5) of a display processing device, information data (1...  

Matches 151 - 200 out of 1,555