Aircraft controls

B - Operations – Transporting – 64 – C

Patent

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B64C 13/16 (2006.01) G05D 1/00 (2006.01)

Patent

CA 1253239

ABSTRACT On an aircraft having spoilers on the wing, the spoilers are converted, according to this invention, following the ACT philosophy, for use in countering gust effects. Accordingly, a sensor of gusts is arranged to transmit warning of the arrival of a significant gust to 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.

454808

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