Patent ID: 11884379
Assignee: DASSAULT AVIATION
Field: Mechanical elements (Mechanical engineering)
Classification: CPC B  G | IPC B  G

Claim 10:
11. The control system according to claim 1, wherein the high lift assembly is configured to be controlled into at least three different aerodynamic configurations of increasing lift;
the manual control device being configured, when the movable member reaches the first position from the rest position, to output at least one signal representative of the reaching of the first position to change the high lift assembly from a current one of the aerodynamic configurations to another of the aerodynamic configurations having a lift greater than the current aerodynamic configuration;
and the manual control device being configured, when the movable member reaches the second position from the rest position, to output at least one signal representative of the reaching of the second position to change the high lift assembly from a current one of the aerodynamic configurations to another of the aerodynamic configurations having a lift less than the current aerodynamic configuration.