| 摘要 |
<p>The invention pertains to the field of measurement devices for providing results other than an instantaneous value for a variable, and more particularly to an aircraft flight control assistance device comprising means (10) for detecting an instantaneous value of physical variables relating, for instance, to the aircraft propulsion system and to environmental conditions, characterized in that said device includes means (70) for displaying, at any point of a flight envelope using power and on the basis of said measured values, data representative of the difference between the power consumption of the propulsion system and a predetermined maximum power value, said means (70) having an on-board processor (80) in which a model of the flight mechanics and engines throughout the aircraft flight envelope has been input, as well as a display means (90).</p> |
