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WO/2008/064191A2 |
A visual display system includes a monitor for displaying a visual display; a memory having a user application definition file containing information related to the visual display; and a processor coupled to the monitor and the memory, t...
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WO/2008/060260A2 |
An improved system and method for increasing the visibility of critical flight information on aircraft displays, such as, for example, Primary Flight Displays are disclosed. For example, an aircraft display system is disclosed that inclu...
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WO/2008/051277A2 |
An electronic flight bag is disclosed which includes an electronic logbook module having an electronic logbook database. The electronic logbook module is configured to compile a list of deferred maintenance items including one or more ME...
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WO/2008/048949A2 |
Provided are systems and methods for operating an avionics component to a given level of certification. Steps of the method include receiving data from a sensor and, sending the data to at least two components, a data monitor and an inte...
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WO/2008/043763A1 |
The invention relates to the field of guiding and taxiing assistance optoelectronic devices for aircraft comprising a head-up display for presenting information in the visual field of the pilot. The invention is particularly intended for...
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WO/2008/035827A1 |
This invention concerns a pedestrian navigation system for using GIS in the area which is difficult to acquire GPS signal, which determines the user's position by calculating the horizontal and vertical displacement with the tilt angles ...
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WO/2008/031723A1 |
This system accompanies the alarms of TAWS type and in particular the alarms of 'avoid terrain' type telling the pilot that he has gone past the limit point of success of a standard vertical avoidance manoeuvre, of indications (32, 33) o...
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WO/2008/024130A2 |
A navigation procedure display (200) is described. The navigational procedure display includes a dynamic information area (204), positioned within the flight procedure display, for displaying a current procedure (240) instruction and at ...
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WO/2008/015102A2 |
The invention relates to a system comprising two combined instruments (ICS1, ICS2) mounted on board an aircraft, and means (10) of communication between the two combined instruments (ICS1, ICS2), each combined instrument (ICS1, ICS2) com...
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WO/2008/010841A1 |
An avionics system for a plane includes a plurality of nodes disposed throughout the plane, each node performing a function. The system includes an optical network in communication with the nodes and through which the nodes communicate. ...
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WO/2008/009133A1 |
An instrumented ball for collecting data in an industrial mill comprising a durable sphere defining an enclosed cavity and having a substantial thickness, the sphere manufactured from a resilient material able to withstand pressures exer...
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WO/2008/006798A2 |
The invention relates to the securing of aircraft handling information necessary for cockpits. More specifically, the invention relates to an aircraft head-up display characterised in that it includes means for calculating a PFD-type sym...
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WO/2008/003591A1 |
The invention relates to flight control systems for aircraft having large control loops delivering load factor commands and which are applied to flight controls more suited to the tracking by the pilot of a longitudinal attitude deviatio...
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WO/2008/000712A1 |
The invention relates to a method for managing the display of a rotary counter on a digital screen, the method enabling at least one value of the counter in the form of characters to be permanently displayed in a window (34), the values ...
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WO/2007/139495A1 |
The present invention relates to a device for, during traveling with a vehicle, classifying a distance of a way along which the vehicle is traveling. The device comprises means for dividing the distance into segments, means for determini...
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WO2007107001B1 |
This invention relates to a system and method to generate a private, auditable, evidentiary quality record of the location-history of an asset or person. This invention addresses ten critical improvements over existing systems that are p...
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WO/2007/123559A2 |
Systems and methods to accurately display lateral deviation symbology in offset approaches to runways is provided. A system for on-aircraft display of lateral deviation symbology for use in offset approaches comprises means for generatin...
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WO/2007/123558A2 |
A system and method for displaying obstacles in a conformal perspective view. The system comprises a display screen for graphical display of data, at least one obstacle data source, one or more graphics processors for receiving obstacle ...
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WO/2007/115359A1 |
A display system is disclosed for use in controlling aircraft traffic. The display system includes means for displaying a representation of a first aircraft relative to a second aircraft. The display system also includes means for displa...
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WO/2007/110503A1 |
The guidance system (1) comprises means (2, 6) for generating an alphanumeric identification characteristic, making it possible to identify a data item which must be used for a selected guidance mode of the aircraft, and display means (1...
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WO/2007/096501A1 |
Method and device for detecting a lateral dissymmetry of an aircraft. The detection device (1) comprises a means (7) for detecting a lateral dissymmetry, as a function of the current value of a control parameter which is representative o...
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WO/2007/096508A2 |
Method and device for automatically adjusting an image of an aircraft navigation screen. The device (1) comprises means (8, 9) for automatically determining, if necessary, a new display configuration making it possible to present on a na...
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WO/2007/094765A2 |
A method and apparatus for performing wide area terrain mapping. The system comprises a digital elevation map (DEM) and mosaic generation engine (430) that processes images that are simultaneously captured by an electro-optical camera (R...
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WO/2007/086822A2 |
Disclosed is an aircraft computing and display device (14) that includes a general purpose processor (30), a touch screen display (16) and a housing (26). The processor executes logical instructions in the form of computer software. The ...
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WO/2007/079556A1 |
A system to monitor ruptures of cables and anchoring lines (20) and others in oil extraction platforms (10) and vessels (11) is described, comprising a monitoring device (15) fastened to a given line at a given depth (20), so that any mo...
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WO/2007/080313A1 |
The invention relates to a method and a device for assisting the flying of an aircraft, said method and device being used to determine an approach path and comprising a guidance system for helping to guide the aircraft along this approac...
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WO/2007/078707A2 |
Methods and systems for a displaying a moving map display for an aircraft is provided. The method includes determining a route of intended travel of the aircraft on the moving map display, determining a rank of relative importance of a p...
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WO/2007/078708A2 |
Methods and systems for displaying an en-route visible terrain display for an aircraft are provided. The method includes representing each pixel of a terrain display using a geographical location and an elevation above the location, each...
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WO/2007/078709A2 |
Methods and systems for a display system for an aircraft are provided. The system includes a moving map display screen configured to display a shaded-relief terrain display representative of an area being traversed by the aircraft, and a...
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WO/2007/075327A2 |
Methods and systems for a position indicating display system for an aircraft are provided. The system includes a moving map display representative of an area being traversed by the aircraft such that a current relative position of the ai...
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WO/2007/044694A2 |
An aircraft service information handling system comprises an input module operable to collect field service narrative data. A natural language data extraction module extracts problem data and related solution data from the narrative data...
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WO/2007/034079A1 |
The inventive device (1) comprises at least one rudder (2A, 2B, 2n), a control unit (4) for applying a deflexion instruction to the rudder, means (6) for measuring recovery characteristic displaying the evolution of the aircraft movement...
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WO/2007/028675A1 |
The invention concerns a method for homogenizing measurement units used for displaying communication messages containing encrypted data, in particular messages exchanged by an aircraft with an air traffic control authority. The method in...
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WO/2007/019135A2 |
An automated system tracks and records factors that affect fuel consumption. Configuration factors such as the actual engine(s) used in the airplane, weight, weight distribution, engine pressure, engine rotation speeds, etc.; environment...
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WO/2007/012747A1 |
The invention concerns a method for processing data representing an interaction between a user (12) and his/her work environment (14), characterized in that it includes the following steps: acquiring (E1) data representing the position i...
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WO/2007/012199A2 |
The present invention provides a system for coordinating multiple vehicles in a passageway environment (e.g., in underground mines). The system includes methods and apparatus for determining the global position and orientation of a vehic...
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WO/2007/010120A1 |
The invention concerns a device (1) comprising means (2) for determining the current position of the aircraft, a mapping database (3), a navigation system (4), means (9) for determining the current heading of the aircraft, and a display ...
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WO/2007/006966A2 |
The invention concerns an approach assisting device (1) comprising a flight management system (2) which determines an approach path, an inertial reference system (3) which prepares inertial position data, which receives position data of ...
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WO/2007/005033A2 |
A system and method of guiding an aircraft is disclosed. The aircraft includes at least one non-rigidly attached sensor for providing a signal indicative of the angular rate of turn of the aircraft. The signal includes an oscillation com...
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WO/2007/005658A2 |
One embodiment of the present invention includes an aircraft instrumentation system for a cockpit instrument panel having a first device associated with a first pilot of an aircraft and positioned on the instrument panel substantially in...
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WO/2007/002864A1 |
A display system and method are provided for a vehicle that includes a processor (104) and a display. The processor (104) is adapted to receive terrain data (106) and navigation data (108) operable, in response thereto, to supply one or ...
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WO/2007/002916A1 |
A system and method are disclosed for enhancing the visibility and ensuring the correctness of terrain and navigation information on aircraft displays, such as, for example, continuous, three-dimensional perspective view aircraft display...
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WO/2007/001306A1 |
Systems and methods for displaying a map onboard an aircraft are disclosed. A method in accordance with one embodiment of the invention includes displaying a map of an area at least proximate to an aircraft at an aircraft flight deck dur...
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WO/2006/136687A2 |
A device comprises means for computing the aircraft (A) current position, means for determining at least one maximum permitted deviation (E1) around a set position of the flight path of the flight plan according to accuracy and integrity...
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WO/2006/137859A2 |
A method of accounting for errors in the altitude reporting of a terrain alert and warning system (TAWS) is disclosed wherein errors due to non-standard atmospheric conditions, incorrect altimeter setting and air data computer (ADC) sens...
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WO/2006/132713A2 |
A flight control system 100 includes a primary flight display 118 having a hover display 114 which facilitates operations in DVE conditions. The hover display 114 includes a radar altitude display 122, heading drift symbology 134 and lat...
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WO/2006/125725A1 |
The invention relates to a method consisting in collecting information relating to an aircraft's situation in the airport site, during the landing, take-off or pre-take-off phases, said information being supplied by equipment that is nor...
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WO/2006/120318A2 |
The inventive flight controll assisting device comprises first means (4) for determining the actual aircraft flight conditions, second means (5) for determining, with the aid of said actual flight conditions and a predetermined pattern, ...
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WO/2006/115873A2 |
A display system (100) and method for an aircraft displays, in real-time, the protected airspace (302) associated with a CTL maneuver. The system (100) processes aircraft approach category data and determines the protected airspace (302)...
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WO/2006/115884A1 |
Systems and methods for displaying ground obstructions on a visual display are disclosed. In an embodiment, a ground proximity warning system includes at least one aircraft sensor system operable to acquire aircraft data and a ground pro...
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