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    • 2. 发明授权
    • Trailing edge for an aircraft engine, of the type with moving chevrons
    • 飞机发动机的后缘,具有移动的人字形的类型
    • US08393435B2
    • 2013-03-12
    • US12918329
    • 2009-02-26
    • Philipe Guerin
    • Philipe Guerin
    • F02K1/08
    • F02K1/46F05D2250/11F05D2250/40F05D2250/42F05D2260/96Y02T50/671
    • This trailing edge is of the type with moving chevrons (9a, 9b, 9c). It comprises actuating means able to cause these chevrons (9a, 9b, 9c) to move from a passive position in which they are directed substantially in the direction of the airflow leaving the said engine, into an active position in which at least part of each chevron is inclined with respect to this direction. This trailing edge is notable in that the said active position is derived from the said passive position by pivoting, possibly combined with a translational movement, of at least part of each chevron about an axis (Aa, Ab, Ac) substantially parallel to the said direction.
    • 该后缘是具有移动的人字形(9a,9b,9c)的类型。 它包括致动装置,其能够使这些人字形(9a,9b,9c)从被动地位于基本上沿离开所述发动机的气流的方向的被动位置进入活动位置,其中每个 人字形相对于这个方向倾斜。 该后缘是值得注意的,因为所述主动位置是通过绕基本上平行于所述主动位置的轴线(Aa,Ab,Ac)绕轴线(Aa,Ab,Ac)的枢轴转动(可能与平移运动相结合)而衍生的, 方向。