首页> 外国专利> METHOD AND ON BOARD SYSTEM FOR ENSURING DISTANCE MINIMA FOR LONGITUDINAL SEPARATION UNDER TURBULENT CONDITIONS FROM A VORTEX WAKE

METHOD AND ON BOARD SYSTEM FOR ENSURING DISTANCE MINIMA FOR LONGITUDINAL SEPARATION UNDER TURBULENT CONDITIONS FROM A VORTEX WAKE

机译:在涡流尾迹湍流条件下确保纵向最小距离最小的方法和车载系统

摘要

With the aid of the proposed method and on board system standardized distance minima for longitudinal separation is ensured during flight of a second aircraft (3) behind a first aircraft (1) on take off or landing of said aircraft on one runway or on two parallel runways located near to each other or during flight one behind the other at near altitude levels in conditions where there is the risk of turbulence from the vortex wake of the first aircraft possibly being present along the direction of movement of the second aircraft wherein according to the invention continuous monitoring of the level of wake vortex flight safety of the second aircraft (3) is carried out in a buffer zone (6) which surrounds said aircraft and is selected on the basis of the direction of the aircraft (3) outside the standardized distance minimum taking into account pilot reaction time and the time for the system for controlling the second aircraft to respond to a command to change the speed of movement of the aircraft and in a situation in which the level of wake vortex safety is reduced a command is supplied to change the speed of the second aircraft to ensure that the aircraft flies at distances greater than the standardized minimum separation distance (5) and less than the calculated maximum distance (8) recommended between aircraft with the pilot being presented with the option of independently changing the speed of the aircraft by braking or accelerating during the continuous monitoring of the implementation of standardized requirements regarding longitudinal separation without a reduction in wake vortex safety.
机译:借助于所提出的方法和机载系统,在第二架飞机(3)在第一架飞机(1)上在一条跑道或两条平行线上起飞或着陆时,在第二架飞机(3)在第一架飞机(1)后面飞行期间,确保了用于纵向分离的标准化距离最小值在可能会沿第二架​​飞机的运动方向出现第一架飞机的涡流尾流引起湍流的风险的情况下,位于彼此接近的跑道上或在飞行过程中在高度高度接近的跑道上本发明在围绕飞机的缓冲区域(6)中进行第二飞机(3)的尾流涡流飞行安全水平的连续监控,并且根据标准之外的飞机(3)的方向来选择最小距离,考虑飞行员反应时间和控制第二架飞机的系统响应命令以更改移动速度的时间在降低尾流涡流安全水平的情况下,系统会发出命令更改第二架飞机的速度,以确保飞机以大于标准最小间隔距离(5)且小于计算出的建议的飞机与飞行员之间的最大距离(8),可以选择在连续监控纵向间隔标准要求的实施过程中,通过制动或加速来独立改变飞机的速度,而不会降低尾流涡流的安全性。

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号