| DASSAULT AVIATION Patent applications |
| Patent application number | Title | Published |
|---|
| 20120095623 | DEVICE FOR ASSISTING AIRCRAFT CREW WHEN PERFORMING FLIGHT LEVEL CHANGES - This device providing assistance to aircraft crew for a flight level change of the aircraft in air traffic, comprising means for viewing the position of the aircraft in the vertical plane, is wherein the viewing means comprise: display means capable of displaying an image comprising at least one zone corresponding to a target altitude (FL) for the aircraft, and in that it comprises: selection means for selecting said zone in the image. | 04-19-2012 |
| 20120078921 | METHOD AND SYSTEM FOR AUTOMATIC ANALYSIS OF FAILURE OR STATE MESSAGES - This method for automatic analysis of failure or state messages generated by at least one complex system is characterized in that it comprises the steps for integrating said messages to a database of failure or state messages, and for determining with a computer, for each of said messages, an index of overall interest characterizing a degree of relevance of said message, on the basis of at least one parameter representative of a frequency of occurrence of similar messages in said database, and a correlation between said or each representative parameter and a predefined number of indexes of overall interest. A corresponding analysis system is also provided. | 03-29-2012 |
| 20110315820 | AIRCRAFT STRUCTURAL ASSEMBLY AND ASSOCIATED ASSEMBLING METHOD - An assembly includes a structural wall and a composite wall extending in the extension of the structural wall and defining a second section positioned facing a first section of the wall. The assembly includes an elongated traction element received in a first passage made in the structural wall, the first passage opening out into the first section and into a cell made in the structural wall. The composite wall defines a second passage opening out into the second section and receiving the elongated element, The assembly includes a locking member added onto the elongated element. The composite wall delimits an access cavity connecting an outer surface of the composite wall to the second passage. The locking member is received into the access cavity. | 12-29-2011 |
