公开(公告)号：WO2007115359A1

公开(公告)日：2007-10-18

申请号：PCT/AU2007/000445

申请日：2007-04-05

Applicant: WINDBIDCO PTY LTD ,  MARTIN, Andrew, Louis

Inventor： MARTIN, Andrew, Louis

IPC: G08G5/04 ,  G01S7/04 ,  B64D45/00 ,  G01C23/00

CPC classification number: G08G5/0082 ,  G08G5/0052 ,  G08G5/006 ,  G08G5/0078

Abstract: A display system is disclosed for use in controlling aircraft traffic. The display system includes means for displaying a representation of a first aircraft relative to a second aircraft. The display system also includes means for displaying a safety/risk zone in association with at least the representation of the first aircraft, wherein the safety/risk zone is adapted to move with the representation of the first aircraft to provide a dynamic indication of allowable spacing between the first and second aircraft. The safety/risk zone is updated at least periodically based on input data that contributes to the allowable spacing. The input data may include meteorological and wake vortex data in the vicinity of the first and second aircraft as well as aircraft and other relevant data.

Abstract translation: 公开了一种用于控制飞机交通的显示系统。 显示系统包括用于显示相对于第二飞行器的第一飞行器的表示的装置。 该显示系统还包括与至少第一飞行器的表示相关联地显示安全/风险区域的装置，其中安全/风险区域适于与第一飞行器的表示一起移动以提供允许间隔的动态指示 在第一和第二架飞机之间。 基于有助于允许间距的输入数据，至少周期性地更新安全/风险区域。 输入数据可以包括在第一和第二飞机附近的气象和尾流涡流数据以及飞机和其他相关数据。

公开(公告)号：WO2015164905A1

公开(公告)日：2015-11-05

申请号：PCT/AU2015/000238

申请日：2015-04-21

Applicant: WINDBIDCO PTY LTD

Inventor： MARTIN, Andrew, Louis

IPC: G01F1/66

CPC classification number: G01S15/885 ,  B64F1/36 ,  G01N29/02 ,  G01N2291/0215 ,  G01N2291/044 ,  G01S15/003 ,  G01S15/104 ,  G01W1/00 ,  G01W2001/003 ,  G08G5/0091

Abstract: A method is disclosed for detecting atmospheric turbulence including aircraft induced wake turbulence and/or wind shear within an aperture associated with an aircraft approach or departure corridor around an airport. The method comprises transmitting into the aperture acoustic signals having a waveform suitable for pulse compression and receiving backscattered acoustic echoes of the acoustic signals from the atmospheric turbulence and/or wind shear. The method further includes processing the acoustic echoes in a matched filter receiver to provide a measure of the atmospheric turbulence and discriminating the aircraft induced demise time, being a time taken for the aircraft induced wake turbulence and/or wind shear to fall below a set threshold at least in the aperture. A system for detecting atmospheric turbulence including aircraft induced wake turbulence and/or wind shear associated with an aircraft approach or departure corridor around an airport is also disclosed.

Abstract translation: 公开了一种用于检测大气湍流的方法，其包括在与机场周围的飞行器接近或出发走廊相关联的孔内的飞机引起的尾流湍流和/或风切变。 该方法包括向具有适于脉冲压缩的波形的孔径声信号中传送并接收来自大气湍流和/或风切变的声信号的反向散射声回波。 该方法还包括处理匹配滤波器接收器中的声学回波以提供大气湍流的量度，并区分飞行器引起的死亡时间，飞行器引起的尾流湍流和/或风切变降低到设定阈值以下所花费的时间 至少在光圈中。 还公开了一种用于检测大气湍流的系统，包括飞机引起的尾流湍流和/或与机场周围的飞行器接近或出发走廊相关联的风切变。