公开(公告)号：WO2009053649A8

公开(公告)日：2009-12-17

申请号：PCT/FR2008051869

申请日：2008-10-16

Applicant: AIRBUS FRANCE ,  JOURNADE JEROME

Inventor： JOURNADE JEROME

IPC: B64C9/12 ,  B64C13/16 ,  B64C23/06

CPC classification number: B64C23/06 ,  B64C9/12 ,  B64C13/16 ,  Y02T50/162

Abstract: The invention relates to a method and a device for creating a continuous protected space along the path of an aircraft (1), in which protected space a maximum induced speed Vtc in a vortex (3) of radius Rtc in the wake of an aircraft (1) is decreased by increasing the radius Rtc. The method comprises - a preliminary step of identifying changes in the aerodynamic configurations of the aircraft (1) liable to initiate disruptions in the wake that will have the effect of increasing the radius Rtc, - for each change in configuration determining beforehand the characteristics of propagation of the wake disturbances in the vortex (3), - carrying out, along the course of the aircraft (1), at least two configuration changes separated by a distance such that spaces, in which the effects of the wake disturbances resulting from each of the configuration changes propagated for a predetermined length of time, forms a substantially continuous protected space

Abstract translation: 本发明涉及一种用于沿着飞机（1）的路径创建连续受保护空间的方法和设备，其中受保护空间在飞机尾部（RTC）中具有半径Rtc的涡旋（3）中的最大感应速度Vtc 1）通过增加半径Rtc而减小。 该方法包括 - 识别飞机（1）的空气动力学配置中的变化的初步步骤，其容易在尾流中引起中断，这将具有增加半径Rtc的效果， - 对于预先确定传播特性的每个配置变化 - 涡流（3）中的尾流扰动， - 沿着飞机（1）的走向实现至少两个由距离分开的配置变化，以使得空间（其中由每个 配置变化传播预定的时间长度，形成基本上连续的保护空间