TY - JOUR
T1 - Performance comparison between high temperature rise triple-swirler combustor and double-swirler combustor
AU - Li, Feng
AU - Guo, Rui Qing
AU - Shang, Shou Tang
AU - Cheng, Ming
AU - Tang, Zheng Fu
AU - Song, Bo
AU - Gao, Xian Zhi
N1 - Publisher Copyright:
©, 2015, BUAA Press. All right reserved.
PY - 2015/1/1
Y1 - 2015/1/1
N2 - With use of the parametric modeling method, when the size of diffuser, the maximum dimension of outer case and exit size of combustor were kept the same as single annular combustor (SAC), the combustor head swirler was redesigned from the double-swirler structure into triple-swirler structure; the three-dimensional flow and combustion processes of double-swirler combustor (TSC) and triple-swirler combustor (TSC) were numerically simulated, and the performance of two high temperature rise combustors were compared. The results indicate that, the traditional DSC cannot meet performance requirement such as combustion efficiency of high temperature rise combustion with fuel air ratio of 0.037; by using the TSC, the total pressure recovery coefficient, combustion efficiency and temperature rise can be improved compared with the DSC; the outlet temperature distribution factor (OTDF) and radial outlet temperature distribution factor (RTDF) of TSC is lower than that of DSC. With fuel air ratio of 0.037, the total pressure drop of designed high temperature rise TSC is less than 5%, OTDF reaching 0.162, RTDF reaching 0.106, and combustion efficiency is more than 99%.
AB - With use of the parametric modeling method, when the size of diffuser, the maximum dimension of outer case and exit size of combustor were kept the same as single annular combustor (SAC), the combustor head swirler was redesigned from the double-swirler structure into triple-swirler structure; the three-dimensional flow and combustion processes of double-swirler combustor (TSC) and triple-swirler combustor (TSC) were numerically simulated, and the performance of two high temperature rise combustors were compared. The results indicate that, the traditional DSC cannot meet performance requirement such as combustion efficiency of high temperature rise combustion with fuel air ratio of 0.037; by using the TSC, the total pressure recovery coefficient, combustion efficiency and temperature rise can be improved compared with the DSC; the outlet temperature distribution factor (OTDF) and radial outlet temperature distribution factor (RTDF) of TSC is lower than that of DSC. With fuel air ratio of 0.037, the total pressure drop of designed high temperature rise TSC is less than 5%, OTDF reaching 0.162, RTDF reaching 0.106, and combustion efficiency is more than 99%.
KW - Combustor performance prediction
KW - Double-swirler combustor
KW - High temperature rise combustor
KW - Parametric modeling
KW - Triple-swirler combustor
UR - https://www.scopus.com/pages/publications/84923823245
U2 - 10.13224/j.cnki.jasp.2015.01.002
DO - 10.13224/j.cnki.jasp.2015.01.002
M3 - 文章
AN - SCOPUS:84923823245
SN - 1000-8055
VL - 30
SP - 10
EP - 15
JO - Hangkong Dongli Xuebao/Journal of Aerospace Power
JF - Hangkong Dongli Xuebao/Journal of Aerospace Power
IS - 1
ER -