The invention discloses a digital cabin pressure adjusting method and system for a large aircraft. Collecting pressure signals of an onboard system and a cabin to calculate target pressure; resolving a target flow based on the target pressure; based on the target flow, the exhaust flow of the exhaust valve I and the exhaust flow of the exhaust valve II are calculated according to a preset exhaust flow distribution proportion; and the opening angles of the exhaust valves I and II are calculated based on the exhaust flow of the exhaust valves I and II to control the flow proportion of air flowing out of the cabin. The purpose of controlling the height of the cabin, the change rate of the height of the cabin and air exhaust flow distribution in the cabin can be achieved.

    本发明公开了一种大型飞机用数字式座舱压力调节方法及系统。采集机上系统和座舱压力信号解算目标压力;基于目标压力解算目标流量;基于目标流量根据预设的排气流量分配比例解算排气活门Ⅰ和排气活门Ⅱ的排气流量;基于排气活门Ⅰ、Ⅱ的排气流量解算排气活门Ⅰ、Ⅱ的打开角度控制流出座舱的空气流量比例。本发明能实现控制座舱高度、座舱高度变化速率和座舱内空气排气流量分配的目的。


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    Titel :

    Digital cabin pressure adjusting method and system for large aircraft


    Weitere Titelangaben:

    一种大型飞机用数字式座舱压力调节方法及系统


    Beteiligte:
    LI SHUAITAO (Autor:in) / REN SHIHAO (Autor:in) / LIU YUNGE (Autor:in) / SUN SHENGLI (Autor:in) / XU YANFEI (Autor:in) / LIU YINGLONG (Autor:in) / ZHANG JIANWEI (Autor:in) / SONG ZHAOJIE (Autor:in) / CHEN BING (Autor:in)

    Erscheinungsdatum :

    19.12.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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