发明授权
US07070148B2 Aerodynamic component for controlling a landing guide path of an aircraft 有权
用于控制飞行器的着陆引导路径的空气动力学部件

Aerodynamic component for controlling a landing guide path of an aircraft
摘要:
An aerodynamic including a main body and a control member. The main body is configured to be connected to a wing of an aircraft. The control member is connected to the main body, the control member including a fixed member secured to the main body and a pivotable member configured to increase a drag of the aircraft without substantially changing a lift of the aircraft.
信息查询
0/0