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Methods and systems to detect and alert a dynamic rollover condition for an aircraft

机译:检测和警告飞机动态侧翻状况的方法和系统

摘要

A method for providing data associated with rollover of an aircraft is provided. The method detects a potential dynamic rollover condition for the aircraft based on at least one of a current rotor thrust, a slope of terrain surrounding the aircraft, a state of ground contact components, and a position of a lateral center of gravity, by at least one processor onboard the aircraft, wherein the potential dynamic rollover condition indicates imminent rollover of the aircraft occurring within a predetermined period of time; and presents an alert associated with the potential dynamic rollover condition via an aircraft onboard display communicatively coupled to the at least one processor.
机译:提供了一种用于提供与飞行器侧翻相关联的数据的方法。该方法至少基于当前旋翼推力,飞机周围的地形坡度,地面接触组件的状态以及横向重心的位置中的至少一项来检测飞机的潜在动态侧倾状况。飞机上的一个处理器,其中潜在的动态侧翻条件表示飞机在预定的时间段内即将发生侧翻;并通过通信方式耦合到至少一个处理器的飞机机载显示器提供与潜在动态侧翻条件相关的警报。

著录项

  • 公开/公告号US10099802B2

    专利类型

  • 公开/公告日2018-10-16

    原文格式PDF

  • 申请/专利权人 HONEYWELL INTERNATIONAL INC.;

    申请/专利号US201715431997

  • 发明设计人 MAHIPAL REDDY;ANIL KUMAR SONGA;

    申请日2017-02-14

  • 分类号B64D45/08;G08G5;B64C27;G05D1;G01S19/13;B64D45;

  • 国家 US

  • 入库时间 2022-08-21 13:06:20

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