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This optimization parameters and characteristics of the operation of a 371 a rotary wing

机译:这种优化参数和371 A旋翼的运行特性

摘要

A method of determining parameters that are characteristics of the operation of a vehicle having a power plant with at least one engine and mechanical transmission means, sensors, and display means. During the method, various items of information about the aircraft, its state and/or its operation and/or its environment are measured, and then, for at least one parameter Pi relating to the state and the operation of the aircraft there are determined a first limit value Pi_lim for the parameter Pi, a second value Pi_X for each parameter Pi to enable the aircraft to perform a predetermined maneuver X, and an instantaneous third value Pi_inst for each parameter Pi. Thereafter, each first, second, and third values Pi_lim, Pi_X, Pi_inst is displayed simultaneously in order to show up the relative position of second and third values Pi_X and Pi_inst relative to a first value Pi_lim for each parameter Pi.
机译:一种确定参数的方法,该参数是具有发电厂的车辆的运行的特征,该发电厂具有至少一个发动机和机械传动装置,传感器和显示装置。在该方法期间,测量关于飞行器,其状态和/或其操作和/或其环境的各种信息,然后,对于与飞行器的状态和操作有关的至少一个参数Pi,确定a。参数Pi的第一极限值Pi_lim,使飞机能够执行预定机动X的每个参数Pi的第二值Pi_X,以及每个参数Pi的瞬时第三值Pi_inst。之后,同时显示每个第一,第二和第三值Pi_lim,Pi_X,Pi_inst,以便针对每个参数Pi显示第二和第三值Pi_X和Pi_inst相对于第一值Pi_lim的相对位置。

著录项

  • 公开/公告号FR3033316B1

    专利类型

  • 公开/公告日2018-04-06

    原文格式PDF

  • 申请/专利权人 AIRBUS HELICOPTERS;

    申请/专利号FR20150000411

  • 发明设计人 SERGE GERMANETTI;

    申请日2015-03-04

  • 分类号B64D43/00;

  • 国家 FR

  • 入库时间 2022-08-21 12:33:15

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