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WO/2005/012837A1 |
An aircraft flight management system having a flight management computer that stores a pre-planned lateral route of flight of the aircraft comprising a plurality of successive waypoints to be overflown, the next proximate waypoint being ...
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WO/2005/010554A1 |
The invention relates to methods and devices for aircraft's safe operation and is embodied in the form of a method and system for informing a user, for example an aircraft crew and/or a flight controller, on the probable penetration of t...
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WO/2005/010555A1 |
The invention relates to systems for preventing off-normal situations when there is a possibility that an aircraft penetrates into a dangerous area of the vortex shedding of a vortex generator. The inventive system consists of informatio...
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WO/2005/003875A1 |
The invention relates to a method and a system for monitoring the location of a mining vehicle in a mine. The mine comprises a first and a second work area. At least one identifier (29) whose exact location is known is arranged in the fi...
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WO/2004/107291A1 |
A free flight obstacle avoidance system (OAS) (60) is a commanded obstacle resolution feedback system. The system employs insertion of hybridized elements to the existing designs of Adaptive Ground Collision Avoidance Systems and Midair ...
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WO/2004/102121A1 |
The invention relates to a system for flight management comprising a performance management computer which, during the flight preparation by the crew, plots a flight plan (20) with branches (203, 204, 206, 208) where diversion trajectori...
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WO/2004/102122A1 |
A cockpit configuration management apparatus, method and computer program product for enabling pilot configurations of display and non-display avionics devices to be saved to a storage device, retrieved from that storage device, and opti...
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WO/2004/090474A1 |
In an aircraft flight instrument display system having a display screen for displaying flight information, an airspeed indicator is displayed in a vertical tape format, and has a low speed range indicator with a low speed range identifie...
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WO/2004/087490A2 |
Disclosed is an electronic system for use on vehicles. Some embodiments of the system use an integrated power supply to power all of the electronic components of the electronic system. The electronic system may include various microproce...
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WO/2004/088249A2 |
Methods and apparatus are provided for indicating safe or potentially hazardous operating conditions of an aircraft in a required navigational performance (RNP) environment. The apparatus comprises a course deviation display field with f...
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WO/2004/085964A1 |
The invention relates to an on-board flight management system. According to the invention, the aircraft crew use an MCD console (20) to enter elements which enable the FMS flight management computer to plot a flight plan, and the courses...
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WO/2004/083935A1 |
Described is a heads-up display system for an aircraft having a rotating propeller within view of at least one occupant of the aircraft. The heads-up display system comprises a plurality of light-emitting elements disposed on a side of a...
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WO/2004/059252A1 |
Methods, apparatus and program product are provided to obtain a shortened holding pattern exit path for an aircraft from its current position (CP) in or entering a holding pattern to an allowed exit point (EP) of the holding pattern. The...
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WO2003048886B1 |
A taxi planning system (10) for aircraft provides an intuitive user interface for entering and selecting taxi plans quickly and easily. The system includes predefined reduced selection menus that prompt the pilot with feasible taxi choic...
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WO/2004/048892A1 |
A method for determining a track of a geographical trajectory which has a predetermined start location and a predetermined end location, said method comprising the steps of: moving a data collecting device from the start location to the ...
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WO/2004/048893A1 |
A method for determining a track of a geographical trajectory which has a predetermined start location and a predetermined end location. The method comprises the steps of: moving a data collecting device from the start location to the en...
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WO/2004/037643A1 |
The invention concerns equipment features of aircraft instrument panels. The invention is characterized in that it provides an instrument panel, besides a main attitude indicator display system (50, 52, 54) and necessary piloting paramet...
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WO/2004/034373A2 |
Systems and methods for providing an enhanced head up display to an aircraft pilot are disclosed. According to a first aspect of the present invention, a system for increasing pilot situational awareness is disclosed. The system (1800) i...
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WO/2004/031833A2 |
A method and apparatus is disclosed for displaying a dynamic parameter of an aircraft, the apparatus comprises a display unit receiving a display signal and displaying a scale that changes dynamically and non-linearly in accordance with ...
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WO2003048888B1 |
An airport map display system for an aircraft displays the airport paved surfaces and structures to a pilot or crew member. The system displays runways, taxiways, connectors, ramps, gates, and buildings. Hold and yield points may also be...
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WO/2004/027732A1 |
The MCP/FCU (30) interface for controlling the automatic pilot (13) and/or flight director (14) is provided with an access port which is linked to the ATN terminal (2) by means of a digital information transmission link (4) and provided ...
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WO2003048887B1 |
An airport map display system (10) provides situational awareness to a pilot of an airport's runways, taxiways, and other features relative to the pilot's aircraft. Data representative of an airport map is translated and communicated bet...
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WO/2004/005853A1 |
The invention concerns a method for an aircraft navigational aid, comprising the following steps which consist in: a) calculating on the basis of wind a pick-off, that is a ground track which the aircraft would follow if it were instantl...
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WO/2004/006203A1 |
A flat panel display (10) for presenting graphical renderings (16) of aircraft flight, operation and system status data to an aircraft pilot renders the data at various predetermined brightness levels depending on the category of data as...
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WO/2003/100608A2 |
A system having replaceable subsystems is operable in a certified configuration after installation of a replacement subsystem. The system includes several subsystems each installed at an interface. For each subsystem, the interface inclu...
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WO2002041131A9 |
The present invention provides systems, apparatus and methods for entering data into a flight plan entry field (114a) which facilitates the display (114) and editing of aircraft flight-plan data. In one embodiment, the present invention ...
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WO/2003/087727A1 |
The computation and data load for producing a flight plan and terrain display for a flight management system is reduced through the use of intelligent level of detail control which computes and displays flight plan areas and related terr...
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WO/2003/083414A1 |
An apparatus and method are provided for reducing display clutter and improving the readability of a display by eliminating the necessity of providing multifunction control/display units and other similar radio/audio/etc. subsystem CDUs ...
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WO/2003/079040A2 |
A system and method compares combinations of vehicle variable values against known combinations of potentially dangerous vehicle input signal values. Alarms and error messages are selectively generated based on such comparisons. An aircr...
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WO/2003/071228A2 |
A method and system for providing taxiway navigational information to a crewmember of an airplane taxiing at an airport. An airport taxiway navigation system ('ATNS') that executes on an onboard computer system that displays a map of the...
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WO/2003/071371A1 |
Embodiments provide a method and apparatus for indicating aircraft (12) height relative to an obstruction in a terrain awareness warning system. The method includes receiving data indicative of geographic features of an obstruction, late...
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WO/2003/071236A2 |
A display system having a display screen for graphical display of data, a graphics processor for receiving data from at least a terrain data base and data from a weather radar and for converting the received data into a single data strea...
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WO/2003/069279A2 |
A compact, lightweight, cost effective, self-contained standby electronic navigation system (100) with high signal-to-noise ratio and good dynamic stability is provided. The system includes a first sensor module (122) for providing a plu...
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WO/2003/064976A2 |
The attitude indicator comprises a display device (11) with a screen (110), generating a three-dimensional silhouette of an aircraft (3) on the background of a screen (4,5) which is divided up into two areas a lower area (4) symbolizing ...
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WO/2003/062754A1 |
Apparatus and methods are provided for flight instruments in an electronic format. The flight instruments may appear in a standard configuration, including both primary flight instruments and secondary flight instruments. The apparatus a...
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WO/2003/062752A1 |
Method and apparatus are provided for assembling a flight plan. The apparatus comprises a memory configured to store data associated with a plurality of waypoints that can be used in the flight plan and a processor coupled to the memory,...
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WO/2003/048687A1 |
An airport feature display system for aircraft provides visual guidance cues and awareness to track the specified taxi path on a HUD (14). The guidance cues include symbology representative of the position of selected airport features su...
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WO/2003/031915A1 |
A predictive flight path symbology system for increasing pilot situational awareness of an aircraft. The system includes a pilot display, and a precision pathway flight guidance (PPFG) symbology set displayed on the pilot display. The PP...
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WO/2003/025511A1 |
The invention relates to an instrument panel for the operating state of a land, air or water vehicle, in particular for the cockpit of an airplane, comprising a number of display fields (13) for representing information, whereby, in orde...
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WO/2003/023734A1 |
Methods and apparatus are provided for generating a vertical situational image of a vehicle. The apparatus for generating a vertical situational image of the vehicle is comprised of an input device configured to receive flight plan data ...
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WO/2003/021291A1 |
A wide field scanning laser obstacle awareness system (LOAS) comprises: a plurality of first optical elements configured to directa portion of a pulsed laser beam generated by a light source to a light detector, and to direct the pulsed ...
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WO/2003/021290A2 |
A combined system of a LOAS and a LIDAR system comprises: a LIDAR arrangement of optical elements for generating a first coherent beam of light at a first predetermined wavelength; a LOAS arrangement of optical elements for generating a ...
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WO/2003/019115A1 |
Pilot error is reduced and auto pilot operation is improved by the addition of capture information (e.g., 420, 410) to the information provided on a cockpit display (100). The capture information (e.g., 420, 410), such as, for example, c...
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WO/2003/005305A1 |
A synthetic rendering of the terrain within a selected field of view is created from raw terrain elevation data, and the resolution of the rendering is proportioned to the altitude above ground level (altitude AGL) of the aircraft. All t...
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WO/2003/005326A1 |
A system and method for displaying a three-dimensional image of airspace includes a series of translucent, horitontal 'pavers' that lie like stepping stones marking the selected flight path. In addition, the display includes a series of ...
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WO/2003/002944A1 |
The invention relates to methods for the display of cartographic information on an aeroplane screen. Said method concerns the display of several windows (2D5, 3D, PV, PH) on an aircraft screen, each representing a distinct aspect of the ...
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WO/2002/103292A1 |
A flat panel display system (10A, 10B) for an aircraft display includes a graphics rendering computer (34) for rendering of anti-aliased graphical imaging data derived from aircraft sensors for full-field imaging on a cockpit display scr...
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WO/2002/090890A1 |
This invention concerns a display device for aircraft comprising a display surface (15) that has a punctual marking (11) arranged so as to represent the pilot's own airplane and one or more threat markings, each of which is arranged so a...
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WO/2002/084219A2 |
Methods and apparatus (20) are provided for displaying multiple data categories (22). The apparatus (20) is comprised of a display (24) that is configured to produce visual representations of the plurality of data categories (22) and a p...
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WO2002025212A9 |
A display system according to various aspects of the present invention provides systems and methods for an integrated graphical user interface which facilitates the interactive and dynamic display aircraft data. In accordance with variou...
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