| 摘要 |
<p>The invention relates to a system for bleeding air on an aircraft, comprising: at least one air bleed valve (5, 5', 5") that can bleed a flow (F) of air on the aircraft, a first temperature information module (10), a second temperature information module (20), at least one control module (30), and at least one data processing module (40) coupled to the control module (30).</p> |
