公开(公告)号：US4615497A

公开(公告)日：1986-10-07

申请号：US821217

申请日：1986-01-21

申请人： Hartwig Seeler ,  Helmut Zimmermann

发明人： Hartwig Seeler ,  Helmut Zimmermann

IPC分类号： B64C13/16

CPC分类号： B64C13/16

摘要： The invention relates to a method and an arrangement for the wings of a h speed aircraft, for increasing the flutter velocity. Aerodynamic auxiliary flaps or vortex generators are placed into an effective position in response to filtered sensor signals for causing a reduction in the local lift rise or for shifting the local neutral point toward the wing trailing edge to thereby provide an effective "flutter brake". The auxiliary flaps or vortex generators are activated only once when needed and stay in an activated effective position for a length of time sufficient for increasing the flutter velocity or speed and the activation takes place rapidly in about 200 to 400 milliseconds from the time the sensors pick up or provide a signal for such activation.

摘要翻译： 本发明涉及一种用于增加颤振速度的用于高速飞行器的机翼的方法和装置。 响应于过滤的传感器信号，将空气动力学辅助翼片或涡流发生器置于有效位置，用于引起局部升高降低或使局部中性点朝向机翼后缘移动，从而提供有效的“颤振制动”。 辅助襟翼或涡流发生器在需要时仅被激活一次，并保持在激活的有效位置一段足以增加颤振速度或速度的时间，并且激活在传感器拾取时间的大约200至400毫秒内快速发生 或提供这种激活的信号。