| 摘要 |
<p>On an aircraft having spoilers (21) on the wing (20), the spoilers are converted, according to this invention, following the ACT philosophy, for use in countering gust effects. Accordingly, a sensor of gusts (23) is arranged to transmit warning of the arrival of a significant gustto a spoiler operator which, taking into account airspeed, deploys the spoilers in a mode so that a phase of spoiler generated lift decrement is time to coincide with effective arrival of the gust.</p> |
