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 |
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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