The invention relates to flight deck constant outside airflow for all flight conditions. Example implementations for maintaining airflow into a flight deck of an aircraft are described herein. An example method may involve detecting, at a computing system and using a flow sensor, a decrease in a level of airflow entering into the flight deck such that the level of airflow is below a threshold level. The aircraft may include air sources configured to direct airflow towards occupancy areas (e.g., the cabin and flight deck) of the aircraft. The method may further involve adjusting a control valve to cause an increase in the level of airflow entering into the flight deck based on detecting the decrease in level of airflow entering into the flight deck. The control valve may be configured to enable and disable airflow from entering into the flight deck.
本申请题为“针对所有飞行条件的驾驶舱恒定外部气流”。本文描述了用于维持进入飞行器的驾驶舱中的气流的示例实施方式。一种示例方法可以涉及在计算系统处使用流量传感器来检测进入驾驶舱的气流水平的降低使得气流水平低于阈值水平。飞行器可以包括被配置为将气流引向飞行器的乘员区域(例如,客舱和驾驶舱)的空气源。该方法可以进一步涉及基于检测到进入驾驶舱的气流水平的降低来调节控制阀以促使进入驾驶舱的气流水平的增加。控制阀可以被配置为允许和禁止气流进入驾驶舱。
FLIGHT DECK CONSTANT OUTSIDE AIRFLOW FOR ALL FLIGHT CONDITIONS
针对所有飞行条件的驾驶舱恒定外部气流
2021-06-18
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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