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Method of calculating oxygen required and system for monitoring oxygen supply and/or calculating flight level after emergency cabin decompression

机译:紧急客舱减压后所需氧气的计算方法和监控氧气供应和/或计算飞行水平的系统

摘要

A system useable in a jet aircraft having installed therein a pressurized oxygen supply which feeds oxygen into the interior of the plane when it flies at high cabin altitudes, the system indicating the changing status of the supply as oxygen is drained therefrom. The system includes a pressure transducer coupled to the supply and means associated with the transducer to determine the lapse rate at which the pressure of the supply is reduced as oxygen is drained therefrom to yield a first signal representing this pressure lapse rate, and to concurrently determine the lapse rate at which the number of liters of oxygen in the supply is reduced as oxygen is drained therefrom to yield a second signal representing the liter lapse rate. These signals are applied to a microprocessor in whose data base is entered the total oxygen inventory of the supply and the oxygen demand of the plane in which the supply is installed. When oxygen is being drained from the supply, the microprocessor calculates and reads out the prevailing supply pressure, the number of liters remaining in the supply, and the time in hours and minutes remaining before the supply is exhausted based on the current rate of oxygen consumption.;The invention provides both a method for calculating the oxygen required, as well as a real time monitoring and calculating system for emergency conditions. The invention is applicable to any pressurized gas system, such as for divers, compressed gas cooking or vehicles, therapeutic oxygen, and the like.
机译:一种可用于喷气飞机的系统,其中安装有加压氧气供应装置,当其在较高的机舱高度飞行时,该氧气供应装置将氧气供应到飞机内部,该系统指示随着氧气从飞机上的排放而改变的状态。该系统包括耦合到供应源的压力传感器和与该传感器相关联的装置,以确定随着氧气从其排出而降低供应源压力以产生代表该压力下降率的第一信号的降低速率,并同时确定当氧气从其中排出时,供应中氧气的升数减少的流逝速率,以产生代表升流速率的第二信号。这些信号被施加到微处理器,在微处理器的数据库中输入了供应的总氧气存量和安装了供应的飞机的氧气需求。当从供气中排出氧气时,微处理器会根据当前的氧气消耗率计算并读取当前的供气压力,供气中剩余的升数以及用尽之前的小时数和分钟数本发明提供了一种用于计算所需氧气的方法,以及用于紧急情况的实时监视和计算系统。本发明适用于任何加压气体系统,例如用于潜水员,压缩气体烹饪或车辆,治疗用氧气等。

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