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warning system for too big hojdforlust after take-off of aircraft with rotating wings

机译:机翼旋转飞机起飞后发生太大事故的预警系统

摘要

A warning system for rotary wing aircraft compares the accumulated altitude loss after take-off of the aircraft with its altitude above ground, and generates a warning if the altitude loss is excessive for the altitude above ground at which the aircraft is flying. The position of the landing gear, the speed of the aircraft and its altitude enable the system only during the take-off and missed approach phases of operation in order to minimize nuisance warnings during other phases. The relationship between radio altitude and altitude loss required to generate a warning is optimized for rotary wing aircaft such as helicopters.
机译:旋转翼飞机的警告系统将飞机起飞后的累积高度损失与其地面高度进行比较,如果高度损失对于飞机所飞行的地面以上高度而言过高,则会发出警告。起落架的位置,飞行器的速度及其高度仅在起飞和错过进近操作阶段启用系统,以便将其他阶段的讨厌警告最小化。无线电警告高度和产生警告所需的高度损失之间的关系已针对直升机的旋转翼飞机进行了优化。

著录项

  • 公开/公告号SE8403094L

    专利类型

  • 公开/公告日1984-12-11

    原文格式PDF

  • 申请/专利权人 SUNDSTRAND DATA CONTROL;

    申请/专利号SE19840003094

  • 发明设计人 PATERSON N S;

    申请日1984-06-08

  • 分类号B64D45/04;

  • 国家 SE

  • 入库时间 2022-08-22 08:11:20

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