首页> 外国专利> Control system for a shutter valve of an aircraft, aircraft equipped with such a control system and associated control method

Control system for a shutter valve of an aircraft, aircraft equipped with such a control system and associated control method

机译:用于飞机的闸阀的控制系统,配备了这种控制系统的飞机和相关的控制方法

摘要

The present invention relates to a control system (1) for controlling a shutter valve (2) of an aircraft (3), said shutter valve (2) being configured to open a bypass circuit (4) initially closed. , said bypass circuit (4) making it possible to supply air to at least one engine (5) of said aircraft (3) without passing through at least one air filter (6) fitted to an air inlet (7), said system order (1) comprising: a manual control member (8) for controlling said shutter valve (2), said manual control member (8) being manually operable by a pilot of said aircraft (3) to control an opening of said bypass circuit (4), at least one computer (10) configured to calculate a current value of a clogging rate TC of said at least one air filter (6). Said control system (1) comprises at least one comparator (11) for comparing said current value of said clogging rate TC with a first threshold value TC1 and with a second threshold value TC2 and at least one alerter (12) to generate a first sensory signal and a second sensory signal. Abstract figure: Figure 1
机译:控制系统(1)技术领域本发明涉及一种用于控制飞机(3)的挡板阀(2)的控制系统(1),所述快门阀(2)被配置为打开旁路电路(4)最初关闭。 ,所述旁路电路(4)使得可以向所述飞机(3)的至少一个发动机(5)供应到至少一个空气入口(7)的至少一个空气过滤器(6),所述旁路电路(4)供应到所述飞机(3)的至少一个发动机(5),所述系统顺序(1)包括: 用于控制所述快门阀(2)的手动控制构件(8),所述手动控制构件(8)由所述飞行器(3)的导频手动操作,以控制所述旁路电路(4)的开口, 至少一台计算机(10),被配置为计算所述至少一个空气过滤器(6)的堵塞速率Tc的电流值。 所述控制系统(1)包括至少一个比较器(11),用于将所述堵塞速率Tc的所述电流值与第一阈值Tc1进行比较,并且具有第二阈值Tc2和至少一个Alerter(12)以产生第一感觉信号和第二感觉信号。 抽象图:图1

著录项

  • 公开/公告号FR3103177A1

    专利类型

  • 公开/公告日2021-05-21

    原文格式PDF

  • 申请/专利权人 AIRBUS HELICOPTERS;

    申请/专利号FR20190012718

  • 发明设计人 ANTOINE BIGEARD;

    申请日2019-11-14

  • 分类号B64D33/02;F02C7/04;

  • 国家 FR

  • 入库时间 2024-06-14 21:34:56

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