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Patent Searching and Data


Matches 301 - 350 out of 1,567

Document Document Title
WO/2007/019133A3
An automated system collects information related to various factors that affect fuel costs, and determines an optimal amount of fuel to be loaded on an aircraft. Information related to an aircraft's fuel efficiency is collected from the ...  
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...  
WO/2007/019135A3
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...  
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...  
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...  
WO/2007/012199A3
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...  
WO/2007/010121A3
The invention concerns a system (1) comprising means (2) for determining the current position of the aircraft, a display device (4) displaying, on a viewing screen (7) an airport map, wherewith is associated a symbol illustrating the cur...  
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 ...  
WO/2007/006966A3
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 ...  
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 ...  
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...  
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...  
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 ...  
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...  
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...  
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...  
WO/2006/137859A3
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...  
WO2005123443A3
The invention relates to a method of indicating the lateral manoeuvre margins on either side of the flight plan path of an aircraft. The parts of the flight plan of an aircraft corresponding to low-altitude lateral paths can comprise pas...  
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...  
WO/2006/136687A3
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...  
WO/2006/134256A3
The system (1) comprises means (6) for determining a limit angle of climb corresponding to a climb angle of the aircraft for flying over the ground along an avoidance path and means (8) for displaying a characteristic sign representing s...  
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...  
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...  
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, ...  
WO/2006/120318A3
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, ...  
WO/2006/115873A3
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)...  
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)...  
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...  
WO/2006/116089A1
A method and a system is provided for displaying an unusual attitude of an aircraft in a head-up display system. The system comprises an LCD projection unit (14) configured to project the unusual attitude of the aircraft and a processor ...  
WO/2006/113105A1
An improved system and method are disclosed for facilitatin g target aiming and aircraft control by flight crews using electronic displays. For example, an aircraft display system is disclosed that includes a database for storing target ...  
WO2005013204A3
A flight situation presentation system (100) displays a large majority of the information required for piloting an aircraft in an enhanced manner to reduce potential for misinterpretation and instances of piloting error. Approaches inclu...  
WO/2006/106211A1
The invention relates to a system comprising a display device displaying, on a cockpit pilot display unit (7), a set of indications (10) containing an aeroplane symbol (8) which illustrates the position of the aeroplane and a map part (9...  
WO/2006/106206A1
The invention concerns a device (1) comprising means (7) for searching for elements of the airport which are displayed on a display field of a screen (9), means (10) for verifying, for each of said elements, whether it forms part of a fi...  
WO2006073669A3
An improved avionics display unit (36) graphically presents meteorological phenomena data to a pilot enroute utilizing conventional pilot report (PIREP) information which includes meteorological phenomena data including phenomena locatio...  
WO/2006/104552A1
A relative navigation system including a first unit responsive to the motion of a first position, a second unit responsive to the motion of a second position and a processing unit that generates a relative navigation solution as a functi...  
WO/2006/091228A2
An embedded digitization system (100) enables a military platform to receive, transmit and process a variety of types of information for a variety of purposes. An apparatus and method provides a means to ensure information interoperabili...  
WO/2006/091228A3
An embedded digitization system (100) enables a military platform to receive, transmit and process a variety of types of information for a variety of purposes. An apparatus and method provides a means to ensure information interoperabili...  
WO/2006/087276A1
The invention concerns the device, on board an aircraft, of data received or exchanged without any audio communication with the ground or with other aircraft by means of a data management device provided with display means showing, in a ...  
WO/2006/087709A1
There is provided a personal navigation system, including a head-mounted orientatio sensor, a coordinate position sensor, a head-mounted display, and a processor receiving a input from the head-mounted orientation sensor and an input fro...  
WO/2006/083408A1
An E-field sensing system (16, 18, 26, 28) is provided to detect the presence of obstacles (14), including wires, power lines or trip wires, as well as towers, guy wires, buildings and elevated terrain, in which a variation or tilt of th...  
WO/2006/078322A2
The present invention describes a drive system for an aircraft involving one or more nose wheel motors. Data regarding the nose wheel rotation is used to control the ground travel of the aircraft, to predict potential problems, to provid...  
WO/2006/076647A2
The present invention provides computer implemented methodology that permits the safe landing and recovery of rotorcraft following engine failure. With this invention successful autorotations may be performed from well within the unsafe ...  
WO/2006/074081A2
Disclosed is a programmable computing and display device (14) for upgrading a cockpit instrument panel (12) of an aircraft (8). The programmable computing and display device includes a plurality of processing units; a network backbone (5...  
WO/2006/074081A3
Disclosed is a programmable computing and display device (14) for upgrading a cockpit instrument panel (12) of an aircraft (8). The programmable computing and display device includes a plurality of processing units; a network backbone (5...  
WO/2006/073669A2
An improved avionics display unit (36) graphically presents meteorological phenomena data to a pilot enroute utilizing conventional pilot report (PIREP) information which includes meteorological phenomena data including phenomena locatio...  
WO/2006/068962A2
A system and method for operating an aircraft such that any hostile persons taking over the cockpit, for instance, terrorists or a disgruntled pilot, cannot control the flight path of the aircraft to enter restricted airspace, such as 'n...  
WO/2006/065782A1
Systems and methods for automatically switching to a track view mode on a vertical view display. The system determines aircraft position relative to a leg of a flight plan and switches display mode for a navigation vertical display to tr...  
WO/2006/061072A1
The inventive timepiece, in particular a wristwatch (1) is used in the form of a navigation aid for pilots and navigators and is characterised in that it comprises at least two concentric bezels (38, 46) one of which (46) is at least rot...  
WO2006032549A3
The invention concerns the signalling, to a pilot of a moving craft, for example an aircraft, of lateral maneuver margins taking into account obstacles placed in the maneuvering zone. Said device determines the maneuvering zone of the ve...  
WO2006042098A3
A vertical situation display ("VSD") system (300) according to the invention generates a terrain image (216) that represents a profile view of terrain elevation relative to the position of an aircraft traveling above the terrain. The VSD...  

Matches 301 - 350 out of 1,567