TY - JOUR
T1 - Quenching distance of laminar methane-air flames at cryogenic temperatures and implications for flame arrester design
AU - Guiberti, Thibault
AU - Belhi, Memdouh
AU - Roberts, William L.
AU - Lacoste, Deanna
AU - Damazo, Jason S.
AU - Kwon, Eddie
N1 - KAUST Repository Item: Exported on 2020-10-01
PY - 2020/6/8
Y1 - 2020/6/8
N2 - Understanding flame quenching is needed to develop efficient flame arresters. Here, the quenching distance of methane-air laminar flames is measured at atmospheric pressure for temperatures of the quenching surface down to the cryogenic, Tw = 138 K to 293 K, for two configurations: head-on and tube quenching. Fuels or flammable mixtures in contact with surfaces at temperatures below 293 K are, for example, representative of aircraft during cruise, cryogenic rocket engines, fuel distribution pipes at high altitude, or cryogenic storage of liquified natural gas and hydrogen. The experimental methods are first validated for Tw = 293 K by comparing measured quenching distances to that available in the literature. Then, quenching distances are measured for Tw = 138 K to 293 K. The quenching distance increases when temperature decreases. In the head-on quenching configuration, the quenching distance is almost multiplied by two, from δq = 0.17 mm for Tw = 290 K to δq = 0.32 mm for Tw = 175 K. In the tube quenching configuration, the quenching diameter increases by 40%, from 2.5 mm for Tw = 293 K to 3.5 mm for Tw = 138 K. Experiments conducted in tubes demonstrate that reducing the wall temperature allows quenching with larger tube diameters, yielding lower pressure drops in tubes, which is of practical interest.
AB - Understanding flame quenching is needed to develop efficient flame arresters. Here, the quenching distance of methane-air laminar flames is measured at atmospheric pressure for temperatures of the quenching surface down to the cryogenic, Tw = 138 K to 293 K, for two configurations: head-on and tube quenching. Fuels or flammable mixtures in contact with surfaces at temperatures below 293 K are, for example, representative of aircraft during cruise, cryogenic rocket engines, fuel distribution pipes at high altitude, or cryogenic storage of liquified natural gas and hydrogen. The experimental methods are first validated for Tw = 293 K by comparing measured quenching distances to that available in the literature. Then, quenching distances are measured for Tw = 138 K to 293 K. The quenching distance increases when temperature decreases. In the head-on quenching configuration, the quenching distance is almost multiplied by two, from δq = 0.17 mm for Tw = 290 K to δq = 0.32 mm for Tw = 175 K. In the tube quenching configuration, the quenching diameter increases by 40%, from 2.5 mm for Tw = 293 K to 3.5 mm for Tw = 138 K. Experiments conducted in tubes demonstrate that reducing the wall temperature allows quenching with larger tube diameters, yielding lower pressure drops in tubes, which is of practical interest.
UR - http://hdl.handle.net/10754/663439
UR - https://linkinghub.elsevier.com/retrieve/pii/S2666352X20300017
U2 - 10.1016/j.jaecs.2020.100001
DO - 10.1016/j.jaecs.2020.100001
M3 - Article
SN - 2666-352X
SP - 100001
JO - Applications in Energy and Combustion Science
JF - Applications in Energy and Combustion Science
ER -