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for flygfarkost intended warning device for warning of too high rate of descent

机译:用于flygfarkost的警告装置,用于警告下降率过高

摘要

In an aircraft ground proximity warning system that compares the rate of descent of an aircraft with its altitude above the terrain and in response thereto generates a warning signal when the aircraft's sink rate exceeds a predetermined limit for a particular altitude, a first type of advisory voice warning is generated for combinations of lesser descent rates and greater altitudes and a second type of imperative voice warning is generated for greater sink rates at lower altitudes where the danger of the aircraft impact with the terrain is more significant. In addition, the repetition rate of the advisory warning is increased as a function of increasing descent rate and the amplitude of the advisory warning can similarly be increased as function of increasing descent rate in order to call attention to an increasing undesirable operating condition.
机译:在飞机地面接近警告系统中,该系统将飞机的下降率与其在地面之上的高度进行比较,并且当飞机的下沉率超过特定高度的预定极限时,响应于此生成警告信号,第一类建议性语音对于下降率较低和高度较高的组合,将生成警报,而对于较低的高度,则第二种命令式语音警报将针对较大的下沉率生成,在这种情况下,飞机撞击地面的危险更为明显。另外,建议警告的重复率根据下降率的增加而增加,并且建议警告的幅度可以类似地根据下降率的增加而增加,以便引起人们对不断增加的不希望的工作条件的注意。

著录项

  • 公开/公告号SE7707872L

    专利类型

  • 公开/公告日1978-01-20

    原文格式PDF

  • 申请/专利权人 SUNDSTRAND DATA CONTROL;

    申请/专利号SE19770007872

  • 发明设计人 BATEMAN C D;

    申请日1977-07-06

  • 分类号B64D45/04;

  • 国家 SE

  • 入库时间 2022-08-22 22:36:57

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