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HELICOPTER HEAD-MOUNTED SEE-THROUGH DISPLAYS

机译:直升机头戴式直通显示器

摘要

Head-mounted see-through displays and methods are provided which improve helicopter displays and provide more relevant information to the pilot while reducing the information load on the display. Displays comprise a peripheral pilot-scene pitch indication region, indicating scene orientation information according to an orientation of the pilot's head with respect to the scene, a propulsion state indication region, indicating rotor and engines states with respect to their nominal operation states by presenting only deviations of the rotor and engines states from their nominal operation states, a speed indication region, indicating, in association with displayed air speed, a calculated ground speed or a calculated ground speed component in a direction of propagation and a helicopter pitch indication region displaying a pitch ladder which is re-arranged to space close pitch lines and crowd remote pitch lines.
机译:提供了头戴式透视显示器和方法,其改善了直升机的显示器并向飞行员提供了更多相关信息,同时减少了显示器上的信息负荷。显示器包括周围的飞行员场景俯仰指示区域,根据飞行员头部相对于场景的方向指示场景方向信息,推进状态指示区域,通过仅显示转子和发动机相对于其标称运行状态的状态转子和发动机状态与其标称运行状态之间的偏差,一个速度指示区域(与显示的空气速度相关)指示传播方向上的计算出的地面速度或计算出的地面速度分量,以及直升机俯仰指示区域,显示出重新排列的音高梯子,以隔开密集的音高线并挤满较远的音高线。

著录项

  • 公开/公告号EP3612885A1

    专利类型

  • 公开/公告日2020-02-26

    原文格式PDF

  • 申请/专利权人 ELBIT SYSTEMS LTD.;

    申请/专利号EP20180787291

  • 发明设计人 NAHUM TOMER;SARNA GILI;

    申请日2018-04-16

  • 分类号G02B27/01;G02B27;G01C23;

  • 国家 EP

  • 入库时间 2022-08-21 11:38:32

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