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|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-015/00 B64C-029/00 B64C-023/00|
|미국특허분류(USC)||701/003; 244/207; 244/208; 244/012.1; 416/020R; 416/114|
|우선권정보||DE-10 2009 060 327 (2009-12-23)|
|발명자 / 주소||
|출원인 / 주소||
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 14|
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 d...
1. An aircraft with aerofoils comprising a main wing and at least one control flap that is arranged so as to be adjustable relative to the main wing, and comprising at least one adjustment flap, with the aircraft comprising: an actuator for operating the at least one control flap, as well as a sensor device for acquiring a set position of the control flap,at least one arrangement of flow-influencing devices, which extends in at least one surface segment of the main wing, wherein the surface segment extends in a wingspan direction, and/or of at least one ...