Process to counter the vibrations in aircraft caused by the...

Details Process to counter the vibrations in aircraft caused by the... Process to counter the vibrations in aircraft caused by the...

B - Operations, Transporting

64

C

B64C 17/00 (2006.01) B64C 13/16 (2006.01) B64C 19/00 (2006.01) G05D 19/02 (2006.01)

Patent

CA 2460610

- Selon l'invention, en cas de détection de vibrations induites : .cndot. on calcule un ordre électrique de commande additionnel (.delta.Z, .delta.Y) qui, appliqué à la servocommande d'au moins une gouverne, permet à celle-ci de s'opposer auxdites vibrations induites ; .cndot. on somme l'ordre électrique de commande de vol (dZ, dY) concernant ladite gouverne et ledit ordre électrique de commande additionnel (.delta.Z, .delta.Y) pour obtenir un ordre de commande global pour ladite gouverne ; et .cndot. on asservit temporairement ladite servocommande audit ordre de commande global, en permettant le fonctionnement de ladite servocommande dans une bande de fréquences élargie.

Affiliated with

Also associated with

Rating

Process to counter the vibrations in aircraft caused by the... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Process to counter the vibrations in aircraft caused by the..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Process to counter the vibrations in aircraft caused by the... will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1756309