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Process and device for monitoring the validity of a speed cue of an aircraft and system for generating a speed cue comprising such a device

机译:用于监视飞机的速度提示的有效性的过程和设备以及用于产生速度提示的系统,包括该设备

摘要

The monitoring device (1) comprises a means (2) for considering the values of static and total pressure, used to determine the speed cue, a means (5) for computing on the basis of these values a coefficient of lift which is representative of the lift of the aircraft, a means (7) for computing on the basis of this coefficient of lift a first value of angle of incidence, a means (9) for determining a second value of angle of incidence, a means (12) for computing the difference between these first and second values of angle of incidence, a means (15) for comparing the absolute value of this difference with a predetermined threshold value, and a means (17) for deducing from this difference whether the speed cue is or is not valid.
机译:监视设备( 1 )包括用于考虑静态和总压力值的装置( 2 ),用于确定速度提示,该装置( 5 ),以便根据这些值计算代表飞机升力的升力系数,以及根据此升力系数a计算的平均值( 7 )入射角的第一值,确定入射角的第二值的均值( 9 ),计算第一和第二入射角之差的均值( 12 )入射角的值,用于将该差的绝对值与预定阈值进行比较的平均值( 15 )以及用于从该差异推导出的平均值( 17 )速度提示是否有效。

著录项

  • 公开/公告号US2005043865A1

    专利类型

  • 公开/公告日2005-02-24

    原文格式PDF

  • 申请/专利权人 PHILIPPE SEVE;

    申请/专利号US20040892455

  • 发明设计人 PHILIPPE SEVE;

    申请日2004-07-16

  • 分类号G06F7/00;

  • 国家 US

  • 入库时间 2022-08-21 22:22:18

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