About 45 results
https://drivepatents.com/patents/1071639 · 21 Dec 2005
The method involves determining a transition point on a low flying flight line, representing the start of an intermediate path between the flight line and another flight line starting at an initial point. The latter flight line corresponds to the point whe...
https://drivepatents.com/patents/1071973 · 7 Dec 2005
The method involves determining current flight conditions, and performing an autonomous and global monitoring function of a low altitude flight of an aircraft using the current flight conditions by a monitoring unit (6) to preserve integrity of the aircraf...
https://drivepatents.com/patents/1071974 · 7 Dec 2005
Low altitude flight path constructing method involves constructing lateral and vertical paths of a flight path. The vertical path having segments with preset minimum length is constructed on a profile section defined between two maximum heights of a ground...
https://drivepatents.com/patents/1072152 · 30 Nov 2005
The method involves automatically determining a decision point (5) which indicates a recent position of an aircraft (A) along a main trajectory (TP), where an optional trajectory (TO) can be activated to permit the aircraft to follow the trajectory (TO). T...
https://drivepatents.com/patents/1072153 · 30 Nov 2005
The method involves determining a change-over point (12) which is found on a flight trajectory (T0). The point (12) corresponds to a point where an aircraft (A) quits the trajectory (T0) for reaching a start point (8) of a flight trajectory (T1) of tactic ...
https://drivepatents.com/patents/1072299 · 23 Nov 2005
The indicator has a central processing unit (3) determining a trajectory change of an aircraft based on a vertical or lateral change. A display unit (5) presents, on a head up display (7), four indication units with two indicating a nearest vertical change...
https://drivepatents.com/patents/1072300 · 23 Nov 2005
The method involves determining a safety altitude from a sum of high altitude of an aircraft from ground and a protection height. A control surface defined laterally in the safety surface and vertically by the safety altitude, is determined. A location of ...
https://drivepatents.com/patents/1072297 · 23 Nov 2005
The indicator has a calculation unit determining, from information issued by an information source assembly, a total maximum gradient of an aircraft. A head-up display device (5) presents, on a visual display unit (7), indication units (8, 10). The indicat...
https://drivepatents.com/patents/1072298 · 23 Nov 2005
The method involves determining an auxiliary flight plan corresponding to a lateral revision of a current flight plan on a low altitude flight section. A decision point indicating last position of an aircraft along the current flight plan is automatically ...
https://drivepatents.com/patents/1072885 · 2 Nov 2005
The assembly has an air inlet structure with an inner wall (32) having a sound wave attenuating acoustic structure (36, 38, 40). The wall has a protrusion part (32`) extending backwards beyond a bond line (A) of a connecting flange (22) of an engine crankc...