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METHOD FOR CONTROLLING AIR PRESSURE IN SEALED CABIN DURING DEPRESSURISATION AND DEVICE THEREFOR

机译:减压过程中密封舱内气压的控制方法及其装置

摘要

FIELD: aviation.;SUBSTANCE: group of inventions relates to adjustment of air pressure in hermetically sealed cabin of aircraft during depressurisation and a system implementing said method. In order to adust air pressure in a sealed aircraft cabin, method includes measuring absolute and gauge pressure of air in aircraft cabin, and determining error value given and measured values with respect to atmospheric pressure and rate of change of absolute air pressure in cabin, forming a control action when a mismatch, comparing current rate of pressure change with a maximum permissible exercise forced air pressure control upon exceeding maximum permissible value. Pressure regulator comprises a flow part, two working elements in form of a gate, two drive systems with two electric motors each, a feedback device from position of working element with two channels, a unit of pressure sensors with two sensitive elements, arbiter, units of control of serviceability, standby channel, two multiplex channels controller, two intellectual channels, service channel, onboard system of upper level, control unit, electronic switch, connected in a certain manner.;EFFECT: maintaining pressure in hermetically sealed cabin within allowable limits.;2 cl, 2 dwg
机译:发明领域:组发明涉及在减压期间调节飞机的气密性机舱中的气压以及实现所述方法的系统。为了在密封的机舱中调节空气压力,该方法包括:测量机舱中空气的绝对压力和表压;确定相对于大气压力的误差值和测量值以及机舱中绝对空气压力的变化率,形成不匹配时的控制动作,将当前压力变化率与最大允许运动时的最大允许强制空气压力控制进行比较。压力调节器包括流量部分,两个门形式的工作元件,两个带两个电动机的驱动系统,一个带有两个通道的工作元件位置反馈装置,一个带有两个敏感元件的压力传感器单元,仲裁器,单元可维护性控制,备用通道,两个多路通道控制器,两个智能通道,服务通道,上层机载系统,控制单元,电子开关,以一定方式连接;效果:将密闭驾驶室的压力保持在允许的范围内。; 2 cl,2 dwg

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