Electric control system for aircraft rudder

Details Electric control system for aircraft rudder Electric control system for aircraft rudder

B - Operations, Transporting

64

C

B64C 13/04 (2006.01) B64C 13/50 (2006.01) G05D 1/08 (2006.01) G05D 1/10 (2006.01)

Patent

CA 2349770

- Selon l'invention : .cndot. ledit système comporte, entre le palonnier (7) et l'actionneur (9) de la gouverne (1), des moyens de filtrage (12) du type passe-bas recevant l'ordre de pilotage (y) et engendrant un ordre de commande (yf) pour ledit actionneur (9) ; et .cndot. la constante de temps desdits moyens de filtrage (12) est d'autant plus élevée que l'amplitude dudit ordre de pilotage (y) correspond à une fraction plus grande de la valeur maximale de débattement de ladite gouverne (1).

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