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Defining the flammability of cylindrical metal rods throughudcharacterization of the thermal effects of the ignitionudpromoter

机译:通过 ud定义圆柱形金属棒的可燃性点火热效应的表征 ud发起人

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摘要

All relevant international standards for determining if a metallic rod is flammable in oxygen utilize some form of “promoted ignition” test. In this test, for a given pressure, an overwhelming ignition source is coupled to the end of the test sample and the designation flammable or nonflammable is based upon the amount burned, that is, a burn criteria. It is documented that (1) the initial temperature of the test sample affects the burning of the test sample both (a) in regards to the pressure at which the sample will support burning (threshold pressure) and (b) the rate at which the sample is melted (regression rate of the melting interface); and, (2) the igniter used affects the test sample by heating it adjacent to the igniter as ignition occurs. Together, these facts make it necessary to ensure, if a metallic material is to be considered flammable at the conditions tested, that the burn criteria will exclude any region of the test sample that may have undergone preheating during the ignition process. A two-dimensional theoretical model was developed to describe the transient heat transfer occurring and resultant temperatures produced within this system. Several metals (copper, aluminum, iron, and stainless steel) and ignition promoters (magnesium, aluminum, and Pyrofuze®) were evaluated for a range of oxygen pressures between 0.69 MPa (100 psia) and 34.5 MPa (5,000 psia). A MATLAB® program was utilized to solve the developed model that was validated against (1) a published solution for a similar system and (2) against experimental data obtainedudduring actual tests at the National Aeronautics and Space Administration White Sands Test Facility. The validated model successfully predicts temperatures within the test samples with agreement between model and experiment increasing as test pressure increases and/or distance from the promoter increases. Oxygen pressure and test sample thermal diffusivity were shown to have the largest effect on the results. In all cases evaluated, there is no significant preheating (above about 38°C/100°F) occurring at distances greater than 30 mm (1.18 in.) during the time the ignition source is attached to the test sample. Thisudvalidates a distance of 30 mm (1.18 in.) above the ignition promoter as a burn length upon which a definition of flammable can be based for inclusion in relevant international standards (that is, burning past this length will always be independent of the ignition event for the ignition promoters considered here.udKEYWORDS: promoted ignition, metal combustion, heat conduction, thin fin, promoted combustion,udburn length, burn criteria, flammability, igniter effects, heat affected zone.
机译:用于确定金属棒在氧气中是否易燃的所有相关国际标准都采用某种形式的“助燃”测试。在该测试中,对于给定的压力,将压倒性的点火源连接到测试样品的末端,并且根据燃烧量(即燃烧标准)来指定可燃或不可燃。据记录,(1)测试样品的初始温度会影响测试样品的燃烧(a)关于样品支持燃烧的压力(阈值压力),以及(b)测试样品的燃烧速率。样品熔化(熔化界面的回归速率); (2)所使用的点火器通过在发生点火时将其靠近点火器加热来影响测试样品。总之,这些事实使得有必要确保,如果要在测试条件下将金属材料视为易燃品,则燃烧标准将排除试样在点火过程中可能已进行预热的任何区域。建立了二维理论模型来描述该系统中发生的瞬态热传递和产生的温度。评估了几种金属(铜,铝,铁和不锈钢)和助燃剂(镁,铝和Pyrofuze®)的氧气压力范围为0.69 MPa(100 psia)至34.5 MPa(5,000 psia)。利用MATLAB®程序来求解已开发的模型,该模型已针对(1)类似系统的已发布解决方案和(2)针对在美国国家航空航天局白沙测试设施进行的实际测试获得的实验数据进行了验证。经过验证的模型可以成功预测测试样品中的温度,并且随着测试压力的增加和/或与促进剂的距离的增加,模型和实验之间的一致性也将提高。氧气压力和试样的热扩散率对结果的影响最大。在所有评估的情况下,在将点火源连接到测试样品的过程中,距离大于30毫米(1.18英寸)时,都没有发生明显的预热(约38°C / 100°F以上)。这验证了点火助燃剂上方30毫米(1.18英寸)的距离作为燃烧长度,可燃性定义可依据该燃烧长度纳入相关国际标准中(也就是说,燃烧超过该长度将始终独立于燃烧长度) ud关键词:促进点火,金属燃烧,导热,薄翅片,促进燃烧,燃烧长度,燃烧标准,可燃性,点火剂效应,热影响区。

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