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Method of determination of parameters aerodynamic and method of detection of a breakdown of a probe which is used for determining the parameters aerodynamic

机译:空气动力学参数的确定方法和用于确定空气动力学参数的探针故障的检测方法

摘要

The aerodynamic parameters of an air stream surrounding an aircraft are determined using at least two probes located on the skin of the aircraft. These are used to determine both the incidence ( alpha ) and the side slip ( beta ) of the aircraft. By comparison of the data from two probes it is possible to detect possible failure of one probe. The method for determining the aerodynamic parameters of an air stream surrounding an aircraft is based on the use of at least two probes located on the skin of the aircraft. Each probe is able to measure the local incidence, and this is used to determine both the incidence ( alpha ) and the side slip ( beta ) of the aircraft. The method also allows detection of the failure of a probe, by detecting the incidence and side slip on the basis of measurements from two probes, and using the different pressure coefficient values of each probe. This information is used in conjunction with the upstream infinite static pressure and the total pressure measurements in order to detect possible failure of a probe.
机译:使用位于飞机皮肤上的至少两个探针来确定飞机周围气流的空气动力学参数。这些用于确定飞机的入射角(α)和侧滑率(beta)。通过比较来自两个探针的数据,可以检测到一个探针的可能故障。用于确定飞机周围气流的空气动力学参数的方法是基于使用位于飞机皮肤上的至少两个探针。每个探头都能够测量局部入射角,这可用于确定飞机的入射角(alpha)和侧滑率(beta)。该方法还可以通过基于两个探头的测量值检测入射率和侧滑,并使用每个探头的不同压力系数值,来检测探头的故障。该信息与上游无限静压力和总压力测量结合使用,以检测探头可能的故障。

著录项

  • 公开/公告号FR2817044B1

    专利类型

  • 公开/公告日2003-02-14

    原文格式PDF

  • 申请/专利权人 THOMSON CSF;

    申请/专利号FR20000014885

  • 申请日2000-11-17

  • 分类号G01P5/00;

  • 国家 FR

  • 入库时间 2022-08-21 23:38:11

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