TY - JOUR
T1 - Study on Performance of High Bypass Ratio Fan with a Novel Solidity-Balanced Stator Structure
AU - Gao, Li Min
AU - Zeng, Rui Hui
AU - Li, Rui Yu
AU - Xu, Hao Liang
N1 - Publisher Copyright:
© 2017, Editorial Department of Journal of Propulsion Technology. All right reserved.
PY - 2017/11/1
Y1 - 2017/11/1
N2 - A novel solidity-balanced stator structure for high bypass ratio fan was presented aimed at solving the non-matching of solidity between tip and root. By increasing the tip solidity, the structure would enhance the blade load in tip region which is conductive to control flow separation. And the validity of the structure of solidity-balanced stator was verified by numerical simulation. The results showed that the introduction of small blades inhibited the flow separation on the tip of stator, and improved the flow field structure of the flow passage. In the single stator environment, the expansion capacity of stator increased by 1.52%, and the total pressure loss reduced by 23.6%. In the stage environment, the expansion capacity of stator increased by 0.93%, and the total pressure loss reduced by 15.0%. Furthermore, the structure of solidity-balanced stator showed better ability of stability enhancement in the stage environment, and flow margin increased by 53.8%. The length of small blade affected the performance of the solidity-balanced stator, and there was an optimum small blade length.
AB - A novel solidity-balanced stator structure for high bypass ratio fan was presented aimed at solving the non-matching of solidity between tip and root. By increasing the tip solidity, the structure would enhance the blade load in tip region which is conductive to control flow separation. And the validity of the structure of solidity-balanced stator was verified by numerical simulation. The results showed that the introduction of small blades inhibited the flow separation on the tip of stator, and improved the flow field structure of the flow passage. In the single stator environment, the expansion capacity of stator increased by 1.52%, and the total pressure loss reduced by 23.6%. In the stage environment, the expansion capacity of stator increased by 0.93%, and the total pressure loss reduced by 15.0%. Furthermore, the structure of solidity-balanced stator showed better ability of stability enhancement in the stage environment, and flow margin increased by 53.8%. The length of small blade affected the performance of the solidity-balanced stator, and there was an optimum small blade length.
KW - Balance solidity
KW - Diffusion capability
KW - High bypass ratio fan
KW - Solidity-balanced stator
KW - Stability enhancement
KW - Total pressure loss
UR - http://www.scopus.com/inward/record.url?scp=85045471523&partnerID=8YFLogxK
U2 - 10.13675/j.cnki.tjjs.2017.11.012
DO - 10.13675/j.cnki.tjjs.2017.11.012
M3 - 文章
AN - SCOPUS:85045471523
SN - 1001-4055
VL - 38
SP - 2496
EP - 2503
JO - Tuijin Jishu/Journal of Propulsion Technology
JF - Tuijin Jishu/Journal of Propulsion Technology
IS - 11
ER -