发明名称 AIRCRAFT WITH A CONTROL DEVICE
摘要 <p>An aircraft with aerofoils including a main wing and a control flap that includes an adjustment flap. The aircraft includes an actuator for the control flap, as well as a sensor device for acquiring the position of the control flap, an arrangement of flow-influencing devices for influencing the fluid that flows over a segment of the main wing, and flow-state sensor devices for measuring the flow state. The aircraft includes a flight control device connected to the sensor device for acquiring the position of the control flap and to the flow-state sensor devices, and connected to the actuator and flow-influencing devices for transmitting actuating commands, and a flight-state sensor device connected to the flight control device for transmitting flight states. The flight control device includes a function that selects the flow-influencing devices that are operated for optimizing local lift coefficients on the aerofoil, depending on the flight state.</p>
申请公布号 EP2516261(A2) 申请公布日期 2012.10.31
申请号 EP20100803243 申请日期 2010.12.23
申请人 AIRBUS OPERATIONS GMBH 发明人 GOELLING, BURKHARD;HAUCKE, FRANK;BAUER, MATTHIAS;NITSCHE, WOLFGANG;PELTZER, INKEN
分类号 B64C9/16;B64C9/38;B64C13/18;B64C21/04 主分类号 B64C9/16
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