Control system (1) comprising a control rod (5) extending between a first zone (2) situated in a hydraulic chamber delimited by a chamber wall (3) and a second zone (4) situated outside the hydraulic chamber. The control system (1) further comprising a seal (6) arranged around and against this control rod (5) to oppose the passage of fluid between the first and second zones (2, 4). The system further comprises a guide piece (7) assembled removably with respect to the chamber wall (3), the seal (6) is assembled inside the guide piece (7) so as to allow relative movement of the rod (5) with respect to the guide piece (7) while at the same time achieving sealing between the first and second zones (2, 4).
ACTIONNEUR D'ATTERRISSEUR D'AÉRONEF COMPRENANT UN SYSTÈME DE COMMANDE COMPORTANT UNE TIGE DE COMMANDE
AIRCRAFT LANDING ACTUATOR INCLUDING A CONTROL SYSTEM COMPRISING A CONTROL ROD
FLUGZEUGLANDINGAKTUATOR BEINHALTEND EINES STEUERUNGSSYSTEMS, DAS EIN SCHALTGESTÄNGE UMFASST
2021-06-02
Patent
Electronic Resource
French
SYSTEME DE PEDALE POUR COMMANDE D’UN ACTIONNEUR AUTOMATISE, COMPORTANT UNE HYSTERESIS
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