An experimental study on spray auto-ignition of RP-3 jet fuel and its surrogates
Yaozong DUAN, Wang LIU, Zhen HUANG, Dong HAN
An experimental study on spray auto-ignition of RP-3 jet fuel and its surrogates
Jet fuel is widely used in air transportation, and sometimes for special vehicles in ground transportation. In the latter case, fuel spray auto-ignition behavior is an important index for engine operation reliability. Surrogate fuel is usually used for fundamental combustion study due to the complex composition of practical fuels. As for jet fuels, two-component or three-component surrogate is usually selected to emulate practical fuels. The spray auto-ignition characteristics of RP-3 jet fuel and its three surrogates, the 70% mol n-decane/30% mol 1,2,4-trimethylbenzene blend (Surrogate 1), the 51% mol n-decane/49% mol 1, 2, 4-trimethylbenzene blend (Surrogate 2), and the 49.8% mol n-dodecane/21.6% mol iso-cetane/28.6% mol toluene blend (Surrogate 3) were studied in a heated constant volume combustion chamber. Surrogate 1 and Surrogate 2 possess the same components, but their blending percentages are different, as the two surrogates were designed to capture the H/C ratio (Surrogate 1) and DCN (Surrogate 2) of RP-3 jet fuel, respectively. Surrogate 3 could emulate more physiochemical properties of RP-3 jet fuel, including molecular weight, H/C ratio and DCN. Experimental results indicate that Surrogate 1 overestimates the auto-ignition propensity of RP-3 jet fuel, whereas Surrogates 2 and 3 show quite similar auto-ignition propensity with RP-3 jet fuel. Therefore, to capture the spray auto-ignition behaviors, DCN is the most important parameter to match when designing the surrogate formulation. However, as the ambient temperature changes, the surrogates matching DCN may still show some differences from the RP-3 jet fuel, e.g., the first-stage heat release influenced by low-temperature chemistry.
RP-3 jet fuel / surrogate / spray auto-ignition / constant volume combustion chamber
[1] |
Dagaut P, Cathonnet M. The ignition, oxidation, and combustion of kerosene: a review of experimental and kinetic modeling. Progress in Energy and Combustion Science, 2006, 32(1): 48–92
CrossRef
Google scholar
|
[2] |
Liu W, Zhai J Q, Lin B Y,
CrossRef
Google scholar
|
[3] |
Li X, Zhang W Z, Huang Z,
CrossRef
Google scholar
|
[4] |
Kang D, Kalaskar V, Kim D,
CrossRef
Google scholar
|
[5] |
Liu W, Zhang J B, Huang Z,
CrossRef
Google scholar
|
[6] |
Gao Z H, Hu E J, Xu Z H,
CrossRef
Google scholar
|
[7] |
Dean A J, Penyazkov O G, Sevruk K L,
CrossRef
Google scholar
|
[8] |
Dagaut P, El Bakali A, Ristori A. The combustion of kerosene: experimental results and kinetic modelling using 1- to 3-component surrogate model fuels. Fuel, 2006, 85(7–8): 944–956
CrossRef
Google scholar
|
[9] |
Mairinger G, Frassoldati A, Cuoci A,
CrossRef
Google scholar
|
[10] |
Dooley S, Won S H, Chaos M,
CrossRef
Google scholar
|
[11] |
Malewicki T, Gudiyella S, Brezinsky K. Experimental and modeling study on the oxidation of jet A and the n-dodecane/iso-octane/n-propylbenzene/1,3,5-trimethylbenzene surrogate fuel. Combustion and Flame, 2013, 160(1): 17–30
CrossRef
Google scholar
|
[12] |
Yu W B, Yang W M, Tay K L,
CrossRef
Google scholar
|
[13] |
Mao Y B, Yu L, Wu Z Y,
CrossRef
Google scholar
|
[14] |
Zhang C, Hui X, Lin Y Z,
CrossRef
Google scholar
|
[15] |
Zhang C H, Li B, Rao F,
CrossRef
Google scholar
|
[16] |
Yan Y W, Liu Y C, Fang W,
CrossRef
Google scholar
|
[17] |
Liu Y X, Richter S, Naumann C,
CrossRef
Google scholar
|
[18] |
Xu J Q, Guo J J, Liu A K,
CrossRef
Google scholar
|
[19] |
Yu J, Gou X L. Comprehensive surrogate for emulating physical and kinetic properties of jet fuels. Journal of Propulsion and Power, 2018, 34(3): 679–689
CrossRef
Google scholar
|
[20] |
Zheng D, Yu W M, Zhong B J,
CrossRef
Google scholar
|
[21] |
Yi R, Chen X, Chen C P. Surrogate for emulating physicochemical and kinetics characteristics of RP-3 aviation fuel. Energy & Fuels, 2019, 33(4): 2872–2879
CrossRef
Google scholar
|
[22] |
Liang X, Zhong A H, Sun Z Y,
CrossRef
Google scholar
|
[23] |
Han D, Zhai J Q, Huang Z. Autoignition of n-hexane, cyclohexane and methylcyclohexane in a constant volume combustion chamber. Energy & Fuels, 2019, 33(4): 3576–3583
CrossRef
Google scholar
|
[24] |
Han D, Duan Y Z, Zhai J Q. Autoignition comparison of n-dodecane/benzene and n-dodecane/toluene blends in a constant volume combustion chamber. Energy & Fuels, 2019, 33(6): 5647–5654
CrossRef
Google scholar
|
[25] |
Design Institute for Physical Properties. D IPPR Project 801, Full Version. Sponsored by AICHE, 2012
|
[26] |
ASTM International. ASTM D7668–14 standard test method for determination of derived cetane number (DCN) of diesel fuel oils ignition delay using a constant volume combustion chamber method. ASTM International: West Conshohocken, PA, 2014
|
[27] |
Poon H M, Pang K M, Ng H K,
CrossRef
Google scholar
|
[28] |
Woschni G. A universally applicable equation for the instantaneous heat transfer coefficient in the internal combustion engine. SAE Technical Paper, 1967
CrossRef
Google scholar
|
[29] |
Shao J K, Choudhary R, Peng Y Z,
CrossRef
Google scholar
|
[30] |
Yehia O R, Reuter C B, Ju Y G. On the chemical characteristics and dynamics of n-alkane low-temperature multistage diffusion flames. Proceedings of the Combustion Institute, 2019, 37(2): 1717–1724
CrossRef
Google scholar
|
[31] |
Zheng Z L, Badawy T, Henein N,
CrossRef
Google scholar
|
[32] |
Assanis D N, Filipi Z S, Fiveland S B,
CrossRef
Google scholar
|
/
〈 | 〉 |