公开(公告)号：US11884379B2

公开(公告)日：2024-01-30

申请号：US17724653

申请日：2022-04-20

申请人： DASSAULT AVIATION

发明人： Jérôme Le Borloch ,  François Pineau

IPC分类号： B64C13/04 ,  G05G1/015 ,  G05G1/04 ,  G05G5/00 ,  G05G5/05

CPC分类号： B64C13/042 ,  G05G1/015 ,  G05G1/04 ,  G05G5/005 ,  G05G5/05 ,  G05G2505/00

摘要： A control system is for a high lift assembly of an aircraft. The assembly is controllable in two aerodynamic configurations each with different lift. The control system includes a manual control device operable by a pilot of the aircraft. The manual control device includes at least one member movable relative to a base body. The movable member can be moved relative to the base body between a rest position, a first position and a second distinct position. The manual control device includes a resilient return device for the movable member in the rest position. The manual control device issues a signal when the movable member reaches either the first or second position, to move the high lift assembly between two of the aerodynamic configurations.

公开(公告)号：US12084191B2

公开(公告)日：2024-09-10

申请号：US17724662

申请日：2022-04-20

申请人： DASSAULT AVIATION

发明人： Jérôme Le Borloch ,  François Pineau

IPC分类号： B64D31/04 ,  B64C13/04 ,  G05G1/04 ,  H01H23/14

CPC分类号： B64D31/04 ,  B64C13/04 ,  B64C13/042 ,  G05G1/04 ,  G05G2505/00 ,  H01H23/145

摘要： A command device for controlling a mechanical energy reduction assembly of an aircraft, movable between an inactive configuration and a maximum mechanical energy reduction configuration, includes a rocker button, movable between a mechanical energy reduction assembly configuration maintaining position, a first position of incremental movement of the mechanical energy reduction assembly to its maximum mechanical energy reduction configuration and a second position of incremental movement of the mechanical energy reduction assembly to its inactive configuration. The command device further includes at least one return element configured to return the rocker button to its maintaining position.

公开(公告)号：US11945570B2

公开(公告)日：2024-04-02

申请号：US17550006

申请日：2021-12-14

申请人： DASSAULT AVIATION

发明人： Fabien Cockenpot ,  François Pineau ,  Jérôme Le Borloch

IPC分类号： B64C13/04 ,  B64C13/06 ,  B64C13/12

CPC分类号： B64C13/0421 ,  B64C13/06 ,  B64C13/12

摘要： A piloting device for piloting an aircraft comprises a first and a second control stick mounted movable on a support. The device comprises a priority selection module configured to switch the first and second control sticks between a piloting configuration and a non-piloting configuration. The device further comprises a detection system for detecting the positions of the first and second control sticks; a first and second actuation system configured to generate respective first and second forces on the respective first and second control stick; and a control module configured to control the actuation system of the control stick which is in a non-piloting configuration such that the positions of the control sticks are identical.