- 专利标题： AIRCRAFT LANDING GEAR CONTROL SYSTEM
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申请号： US18224392申请日： 2023-07-20
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公开(公告)号： US20240228025A9公开(公告)日： 2024-07-11
- 发明人: M Nizar Sanadiki
- 申请人： M Nizar Sanadiki
- 申请人地址： US CA Dana Point
- 专利权人： M Nizar Sanadiki
- 当前专利权人： M Nizar Sanadiki
- 当前专利权人地址： US CA Dana Point
- 主分类号： B64C25/26
- IPC分类号： B64C25/26 ; B64C25/20 ; B64C25/32
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/授权文献
- US20240132205A1 AIRCRAFT LANDING GEAR CONTROL SYSTEM 公开/授权日：2024-04-25
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