| Patent application number | Description | Published |
|---|
| 20080243316 | Method For Setting an Aircraft Barometric Altitude - The invention relates to a method for aiding the setting of the barometric altitude of an aircraft equipped with a means ( | 10-02-2008 |
| 20080300737 | METHOD AND DEVICE FOR CALCULATING A FLIGHT PLAN - The invention relates to a method for calculating a diversion flight plan making it possible to define at least one diversion airport to have the associated predictions on the corresponding diversion flight plan. The invention also relates to a device comprising means implementing the method according to the invention. The device according to the invention makes it possible to change, in the course of the flight, the said waypoint from which the diversion flight plan is calculated. The method according to the invention furthermore calculates the last possible diversion point on the flight plan, based on the fuel predictions. | 12-04-2008 |
| 20080312779 | FLIGHT MANAGEMENT COMPUTER WITH CONSIDERATION OF APPROACH SPEED CONSTRAINT - The flight management computer discloses and carried onboard an aircraft can be programmed with a newly apparent speed constraint while it ensures the guidance of the aircraft in the course of a landing runway approach. It then takes account of the speed constraint by using it as target speed, when it is greater than an instruction speed which depends on the number of extended flap settings and which corresponds to the addition of a further flap setting. If appropriate, the speed constraint may be bounded below, thus making it possible to remain within the limits of the flight domain of the aircraft in its configuration at the time. | 12-18-2008 |
| 20090005918 | METHOD FOR OPTIMIZING THE EXIT OF AN AIRCRAFT IN A HOLDING CIRCUIT - The method of optimizing the exit of an aircraft traversing for a known duration (D) a holding circuit forming a racecourse comprising two parallel branches of the same distance, the branches being traversed in a first time (t | 01-01-2009 |
| 20090076721 | NAVIGATION AID METHOD - The invention relates to a navigation aid method and device for an aircraft. The aircraft occupies a position PPOS outside its flight plan and seeks to rejoin the flight plan. The flight plan includes a succession of waypoints. A waypoint WPT | 03-19-2009 |
| 20090082955 | METHOD OF PLOTTING A PORTION OF TRAJECTORY OF AN AIRCRAFT COMPRISING A CIRCULAR ARC OF CONSTANT RADIUS - A method is disclosed for plotting a trajectory portion ( | 03-26-2009 |
| 20100152927 | METHOD AND DEVICE FOR OPTIMIZING THE FLIGHT OF AN AIRCRAFT - The invention relates to a method for optimizing the flight of an aircraft comprising a flight management system, the said flight management system using a first cost index (CI | 06-17-2010 |
| 20100161156 | DEVICE FOR ASSISTING IN THE CHOICE OF A DIVERSION AIRPORT - The invention relates to a device for assisting in the choice of a diversion airport for an aircraft piloted by a crew ( | 06-24-2010 |
| 20100168936 | Method of Constructing a Vertical Profile in the Event of Depressurization in an Area with Risks and Associated Devices - The method of generating a secure flight plan portion in the event of depressurization corresponding to a time-conditioned descent profile that may include a succession of levels, comprises:
| 07-01-2010 |
| 20100198433 | Flight Management System with Optimization of the Lateral Flight Plan - Flight management system for aircraft comprising computation means capable of determining a gain or a loss in terms of flight time remaining to a point of arrival, and in terms of fuel consumption, following the input by an operator of a modification of an initial flight plan using the Direct To function. The computation means are capable of suggesting to the operator a modification of the lateral flight plan that procures an optimum gain. The flight management system also comprises a display interface capable of presenting to the operator the information concerning the gain or the loss in time and/or consumption, and of prompting the operator to accept or refuse the modification. | 08-05-2010 |
| 20100324812 | Method of short-term rejoining of a flight plan by radar guidance of an aircraft - Method of formulating a lateral flight trajectory for the rejoining by an aircraft ( | 12-23-2010 |
| 20110082605 | AIRCRAFT PILOTING ASSISTANCE METHOD AND CORRESPONDING DEVICE - An aircraft piloting assistance method and system including determining at least one flyable slope with which the aircraft is assumed to be able to fly, based on a value of at least one flight parameter including the weight of the aircraft. The step for determining said slope or slopes with which the aircraft is able to fly, called flyable slopes is performed by a computer, and presenting the flyable slope to a decision-maker. | 04-07-2011 |
| 20110087428 | DEVICE FOR AIDING THE FLIGHT MANAGEMENT OF AN AIRCRAFT - A device for aiding the flight management of an aircraft includes a navigation display, a personalized database capable of storing navigation-aid data, each datum comprising a classification type representative of a family or of one or more categories of navigation-aid data, one or more periods of validity of the said datum, information relating to at least one geographic zone of the said datum, one graphic and/or textual representation of the said datum, selection means allowing an operator to choose one (or more) type(s) of classification, called selected type(s), extraction means capable of extracting from the personalized database the navigation-aid datum or data called extracted data of which the type is equal to at least one selected type, of which at least one geographic zone is situated at a distance, from the flight plan or from the aircraft, that is less than a predetermined maximum distance and of which at least one period of validity verifies a predefined display time criterion, the said extraction means transmitting the said extracted datum or data to the said navigation display capable of displaying the representations of the said extracted data. | 04-14-2011 |
