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飞行中客舱烟雾控制。

In-flight cabin smoke control.

作者信息

Eklund T I

机构信息

Federal Aviation Administration Technical Center, US Department of Transportation, Atlantic City International Airport, New Jersey 08405, USA.

出版信息

Toxicology. 1996 Dec 31;115(1-3):135-44. doi: 10.1016/s0300-483x(96)03502-0.

Abstract

Fatal accidents originating from in-flight cabin fires comprise only about 1% of all fatal accidents in the civil jet transport fleet. Nevertheless, the impossibility of escape during flight accentuates the hazards resulting from low visibility and toxic gases. Control of combustion products in an aircraft cabin is affected by several characteristics that make the aircraft cabin environment unique. The aircraft fuselage is pressurized in flight and has an air distribution system which provides ventilation jets from the ceiling level air inlets running along the cabin length. A fixed quantity of ventilation air is metered into the cabin and air discharge is handled primarily by pressure controlling outflow valves in the rear lower part of the fuselage. Earlier airplane flight tests on cabin smoke control used generators producing minimally buoyant smoke products that moved with and served as a telltales for overall cabin ventilation flows. Analytical studies were done with localized smoke production to predict the percent of cabin length that would remain smoke-free during continuous generation. Development of a buoyant smoke generator allowed simulation of a fire plume with controllable simulated temperature and heat release rates. Tests on a Boeing 757, modified to allow smoke venting out through the top of the cabin, showed that the buoyant smoke front moved at 0.46m/s (1.5ft/sec) with and 0.27m/sec (0.9ft/sec) against, the axial ventilation airflow. Flight tests in a modified Boeing 727 showed that a ceiling level counterflow of about 0.55m/sec (1.8ft/sec) was required to arrest the forward movement of buoyant smoke. A design goal of 0.61m/s (2ft/sec) axial cabin flow would require a flow rate of 99m3/min (3500ft3/min) in a furnished Boeing 757. The current maximum fresh air cabin ventilation flow is 78m3/min (2756 ft3/min). Experimental results indicate that buoyancy effects cause smoke movement behaviour that is not predicted by traditional design analyses and flight test methodologies. Augmenting available ventilation for smoke control remains a design and safety challenge.

摘要

因机舱内起火导致的致命事故仅占民用喷气式运输机队所有致命事故的约1%。然而,飞行过程中无法逃生加剧了低能见度和有毒气体带来的危险。机舱内燃烧产物的控制受到若干特性的影响,这些特性使机舱环境独具特色。飞机机身在飞行中处于增压状态,并有一个空气分配系统,该系统从沿着机舱长度分布的天花板进气口提供通风射流。固定数量的通风空气被计量送入机舱,空气排放主要通过机身后部下部的压力控制外流阀进行处理。早期关于机舱烟雾控制的飞机飞行试验使用产生最小浮力烟雾产物的发生器,这些烟雾产物随整体机舱通风气流移动并作为其指示物。进行了局部烟雾产生的分析研究,以预测在持续产生烟雾期间机舱内无烟的长度百分比。浮力烟雾发生器的开发使得能够模拟具有可控模拟温度和热释放率的火羽。在一架经过改装以允许烟雾从机舱顶部排出的波音757上进行的测试表明,浮力烟雾前沿在轴向通风气流方向上的移动速度为0.46米/秒(1.5英尺/秒),逆着轴向通风气流方向的移动速度为0.27米/秒(0.9英尺/秒)。在一架改装的波音727上进行的飞行试验表明,需要约0.55米/秒(1.8英尺/秒)的天花板逆流来阻止浮力烟雾的向前移动。在配备家具的波音757中,轴向机舱气流速度达到0.61米/秒(2英尺/秒)的设计目标将需要99立方米/分钟(3500立方英尺/分钟)的流量。目前机舱新鲜空气的最大通风流量为78立方米/分钟(2756立方英尺/分钟)。实验结果表明,浮力效应导致烟雾移动行为无法通过传统设计分析和飞行测试方法进行预测。增加用于烟雾控制的可用通风仍然是一个设计和安全挑战。

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