发明名称 Interfaz de control para dispositivos de borde anterior y posterior
摘要 A system (500) for controlling a high-lift device of an aircraft may include an interface (502) for placement in a flight deck of an aircraft. The interface (502) may include an edge control device (504) for controlling a position of the high-lift device. The interface (502) may be operable to select any of a plurality of control device positions (510). Each one of the plurality of control device positions (510) may correspond to a different flight phase of the aircraft. The edge control device may be operable to engage, in response to a selection of a first control device position, a command mode for actuating the high-lift device in an automated manner based on the flight phase associated with the first control device position.
申请公布号 ES2604605(T3) 申请公布日期 2017.03.07
申请号 ES20140185978T 申请日期 2014.09.23
申请人 The Boeing Company 发明人 Moser, Matthew A;Finn, Michael R;Thoreen, Adam
分类号 B64C13/04;B64C9/28;B64C13/16 主分类号 B64C13/04
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