发明名称 |
Method of controlling a landing guide path of an aircraft |
摘要 |
A method of controlling a landing guide path of an aircraft and a method of steeping a landing guide path of an aircraft include rotating a portion of an aerodynamic component to increase a drag without influencing a lift. A method of controlling a landing guide path of an aircraft including an aerodynamic component having a main portion and a control portion, the main portion connected to a wing of the aircraft, and the control portion including a fixed member connected to a pivotable member. The method includes rotating the pivotable member to increase a drag without influencing a lift. |
申请公布号 |
US2004155146(A1) |
申请公布日期 |
2004.08.12 |
申请号 |
US20030713160 |
申请日期 |
2003.11.17 |
申请人 |
WYREMBEK SUSANNE;MAY PETER;MUTHREICH KLAUS |
发明人 |
WYREMBEK SUSANNE;MAY PETER;MUTHREICH KLAUS |
分类号 |
B64C9/32;(IPC1-7):B64C9/32 |
主分类号 |
B64C9/32 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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