公开(公告)号：US20240132205A1

公开(公告)日：2024-04-25

申请号：US18224392

申请日：2023-07-19

申请人： M Nizar Sanadiki

发明人： M Nizar Sanadiki

IPC分类号： B64C25/26 ,  B64C25/20 ,  B64C25/32

CPC分类号： B64C25/26 ,  B64C25/20 ,  B64C25/405

摘要： An aircraft landing gear control system. As an aircraft prepares to land, the system determines the ground speed of the aircraft and causes the aircraft's wheels to rotate at an angular velocity that corresponds to the aircraft's ground speed so that upon landing, the aircraft wheels are not subjected to a sudden jarring impact.

公开(公告)号：US20240228025A9

公开(公告)日：2024-07-11

申请号：US18224392

申请日：2023-07-20

申请人： M Nizar Sanadiki

发明人： M Nizar Sanadiki

IPC分类号： B64C25/26 ,  B64C25/20 ,  B64C25/32

CPC分类号： B64C25/26 ,  B64C25/20 ,  B64C25/405

摘要： An aircraft landing gear control system. As an aircraft prepares to land, the system determines the ground speed of the aircraft and causes the aircraft's wheels to rotate at an angular velocity that corresponds to the aircraft's ground speed so that upon landing, the aircraft wheels are not subjected to a sudden jarring impact.