Device for antagonistic artificial force gradient for an...

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 13/04 (2006.01) B64C 13/46 (2006.01) G05G 5/08 (2006.01) G05G 7/04 (2006.01) G09B 9/28 (2006.01)

Patent

CA 2572337

The invention concerns a device for antagonistic artificial force gradient for an aircraft control surface remote control device, comprising: an actuating member (1) pivoting about an axis (2) driving a rotary shaft (3); a stationary finger (8) parallel to said shaft (3) and supported at radial distance from the shaft; a fixed finger (8) parallel to said shaft (3) and supported at radial distance from the shaft; a mobile finger (5) secured to the shaft and supported at the same radial distance as the stationary finger, both fingers being parallel to the shaft; a platform (9) supported at the same radial distance as the fingers laterally thereto; a first spring (11) between the stationary finger and the platform and a second spring (10) between the mobile finger and the platform.

Dispositif de restitution artificielle d'effort antagoniste pour un dispositif de commande à distance de gouvernes d'un aéronef, comprenant : un organe d'actionnement (1) pivotant autour d'un axe (2) en entraînant un arbre rotatif (3) ; un doigt fixe (8) parallèle audit arbre (3) et supporté à distance radiale de l'arbre ; un doigt mobile (5) solidaire de l'arbre et supporté à même distance radiale que le doigt fixe, les deux doigts étant parallèles à l'arbre ; un plateau (9) supporté à la même distance radiale que les doigts latéralement à ceux-ci ; un premier ressort (11) entre le doigt fixe et le plateau et un second ressort (10) entre le doigt mobile et le plateau.

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