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A Shock Tube Study on Petroleum Derived Aerospace Fuels and a Fischer-Tropsch Surrogate

机译:石油衍生航空航天燃料的冲击管研究和菲思修赛蛋白

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Ignition delay time data from shock tubes were generated for RP-1, RP-2, JP-8, and a JP-8 synthetic substitute prepared by means of a Fischer-Tropsch process. Samples of RP-1 and JP-8 were taken from regular service supply, while the RP-2 and JP-8 FT were obtained from smaller batch preparations. RP-2 is similar chemically to RP-1 except it is refined so that the sulfur content is much lower to reduce coking. JP-8 which has been synthetically derived from coal is gaining more interest scientifically but has not been compared within a shock tube to its petroleum distillate counterpart. These heavy fuels were tested in a newly heated shock-tube facility capable of maintaining steady-state temperatures of up to 120°C. Tests were made for each of the fuels at two equivalence ratios, Φ = 1 and 0.5, temperatures ranging from 1100 to 2000 K, and at an average pressure of 9 atm. One main result of this study is that there is very little difference in the ignition delay times amongst the four fuels over the conditions studied herein.
机译:从rp-1,RP-2,JP-8和通过Fischer-Tropsch工艺制备的JP-8合成替代品产生来自冲击管的点火延迟时间数据。 RP-1和JP-8的样品取自常规服务供应,而RP-2和JP-8FT是从较小的分批制剂中获得的。除了精制之外,RP-2与RP-1类似,以便硫含量低得多,以减少焦化。已从煤炭源自煤的JP-8正在科学地获得更多兴趣,但尚未在铲斗到其石油馏分对应物中比较。在新加热的冲击管设施中测试这些重型燃料,其能够维持高达120℃的稳态温度。以两个等效的比率为每个燃料进行测试,φ= 1和0.5,温度范围为1100至2000 k,平均压力为9atm。本研究的一个主要结果是,在本文研究的条件下,四个燃料中的点火延迟时间几乎没有差异。

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