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DEVICE TO DETERMINE MATERIAL COMBUSTIBILITY INDEX IN CIRCUMSTANCES TYPICAL FOR INHABITED COMPARTMENTS OF SPACECRAFTS

机译:用于确定典型的情况下划伤太空舱的情况下材料的可燃性指数的装置

摘要

FIELD: fire-fighting methods, equipment or accessories, particularly to determine combustibility index from gravity.;SUBSTANCE: device comprises combustion chamber with material sample to be tested. Two flat parallel walls of the chambers are transversal to gravity vector. One wall may perform plane-parallel motion. Combustion chamber is arranged in centrifuge having plane of rotation transversal to gravity vector. Opposite combustion chamber walls are porous. Correlation to calculate combustion chamber height hc for material combustibility index determination in dependence of working gaseous atmosphere parameters is presented. The invention provides minimization of natural convection in direction transversal to gravity vector, as well as heat and mass transfer during sample burning under convection created by centripetal acceleration.;EFFECT: decreased costs, possibility to estimate material combustibility in circumstances typical for other planets or for space craft interior, possibility to work out fire-protection measures for inhabited compartments of extraterrestrial objects and objects to be arranged on other planets.;4 dwg
机译:领域:灭火方法,设备或配件,尤其是根据重力确定可燃性指标。;物质:设备包括带有待测材料样品的燃烧室。腔室的两个平坦的平行壁横向于重力矢量。一堵墙可以执行平面平行运动。燃烧室布置在离心机中,该离心机的旋转平面横向于重力矢量。相对的燃烧室壁是多孔的。给出了计算燃烧室高度h c 的相关性,以根据工作气体气氛参数确定材料可燃性指标。本发明提供了在与重力矢量横向的方向上自然对流的最小化,以及在由向心加速度产生的对流下的样品燃烧过程中的传热和传质的最小化。航天器内部,有可能为居住的外星物体隔间和将要布置在其他行星上的物体制定防火措施; 4 dwg

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