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Systems and methods for issuing a hard landing warning and providing maintenance advisories for hard landing incidents

机译:用于发布硬着陆警告并为硬着陆事件提供维护建议的系统和方法

摘要

An aircraft (100) is provided. The aircraft may include, but is not limited to, an accelerometer (160) configured to measure a deceleration experienced by the aircraft (100) and a processor (120) coupled to the accelerometer (160). The processor (120) may be configured to determine if the aircraft (100) experienced a hard landing if the deceleration experienced by the aircraft (100) was greater than a predetermined threshold, and generate a maintenance advisory if the aircraft (100) experienced a hard landing.
机译:提供了飞机(100)。飞机可以包括但不限于被配置为测量飞机(100)经历的减速度的加速度计(160)和耦合至加速度计(160)的处理器(120)。处理器(120)可以被配置为:如果飞机(100)经历的减速度大于预定阈值,则确定飞机(100)是否经历了硬着陆,并且如果飞机(100)经历了降速,则生成维护建议。硬着陆。

著录项

  • 公开/公告号EP2612816A3

    专利类型

  • 公开/公告日2017-07-26

    原文格式PDF

  • 申请/专利权人 HONEYWELL INTERNATIONAL INC.;

    申请/专利号EP20130150048

  • 发明设计人 LAD GIRISH M.;CHANDRAN NAGARAJAN;

    申请日2013-01-02

  • 分类号B64D45/04;B64D45/00;

  • 国家 EP

  • 入库时间 2022-08-21 14:07:24

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