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CN107010206A 前缘高升力装置及降低噪声的方法 无效 - 撤回

前缘高升力装置及降低噪声的方法
摘要：
一种前缘高升力装置及降低噪声的方法，该前缘高升力装置可从飞机的机翼展开，可包括前缘和后缘。下表面和上表面均可在前缘和后缘之间延伸。后缘区域可通过后缘和与后缘相邻的区域限定。成形装置可设置在后缘区域处且可在未激活位置和激活位置之间移动。
摘要（英）：

A leading edge high lift device and a method of reducing noise which can be deployed from the wing of the airplane and may include a leading edge and a trailing edge. Both the lower surface and the upper surface extend between the leading edge and the trailing edge. The trailing edge region may be defined by a trailing edge and a region adjacent to the trailing edge. The forming means may be provided at the trailing edge region and movable between an inactive position and an active position.

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