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Effects of Pressure on Minimum Hot Surface Ignition Temperatures (MHSIT) in Hot Air Crossflows

机译:压力对热空气交叉流量最小热表面点火温度(MHSIT)的影响

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Hot surface ignition of flammable liquids in ground and air transportation vehicles is a risk that must be mitigated. Hot surfaces are typically exposed to airflow, and leaking fuel, oil and hydraulic fluid heated by these surfaces may vaporize and mix. The minimum hot surface ignition temperature (MHSIT) of flammable liquids depends on several factors including leak type (spray or stream), liquid temperature, air temperature, velocity, and pressure. ASTM standardized methods for ignition are limited to stagnant and falling drops downward (autoignition) at atmospheric pressure (ASTM E659, ASTM D8211, and ASTM E1491) and at pressures from 2.1 to 20.7 MPa (ASTM G72). Past studies have shown that MHSIT decreases with increasing pressure, but the available databases lack results of extensive testing. Therefore, such data for pressures between 100 kPa to 250 kPa are missing or inadequate. A previously designed experimental apparatus was modified to produce the 100 kPa to 250 kPa air duct pressure levels representative of a typical turbofan engine. In this paper, the modifications over a relevant range of air duct pressures are discussed.
机译:地面和空运车辆中易燃液体的热表面点火是必须减轻的风险。热表面通常暴露于气流,并通过这些表面加热的漏油,油和液压流体可以蒸发和混合。易燃液体的最小热表面点火温度(MHSIT)取决于几个因素,包括泄漏型(喷雾或流),液体温度,空气温度,速度和压力。 ASTM用于点火的标准化方法限于停滞和下降(ASTM E659,ASTM D8211和ASTM E1491)下降(自燃),并且在2.1至20.7MPa(ASTM G72)的压力下。过去的研究表明,MHSIT随着压力的增加而降低,但可用的数据库缺乏大量测试的结果。因此,缺少100kPa至250kPa之间的压力的这种数据缺失或不充分。修饰了先前设计的实验装置以产生典型的涡轮机发动机的100kPa至250kPa空气管道压力水平。在本文中,讨论了在相关的风管压力范围内的修改。

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