Analysis of the Flow Capacity of Variable Cycle Split Fans at the Middle Speed

Author:

An Guangfeng123ORCID,Zhou Rui1,Yu Xianjun123ORCID,Liu Baojie123,Wu Guanghan14

Affiliation:

1. Research Institute of Aero-Engine, Beihang University, Beijing 102206, China

2. National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, Beihang University, Beijing 102206, China

3. Frontiers Science Center for Super-Cycle Aeroengine’s Aerothermodynamics, Beihang University, Beijing 102206, China

4. Shenyang Engine Research Institute, Aero Engine Corporation of China, Shenyang 110015, China

Abstract

The next-generation variable cycle engine imposes stricter requirements on a fan’s flow capacity at the middle speed. To tackle this challenge, the implementation of split fans presents as a potential solution. In the present study, we conducted numerical simulations using the commercial software NUMECA to investigate the aerodynamic performance variation with bypass ratios for variable cycle split fans in “1 + 2” and “2 + 1” configurations at 80% rpm. The results indicate that the flow capacity of the split fans exhibits an increasing trend with a rise in the bypass ratio at 80% rpm and subsequently stabilizes upon reaching a certain bypass ratio. Specifically, the flow capacity of the “2 + 1” split fans is particularly stronger at the small bypass ratios, whereas the “1 + 2” split fans exhibit superior maximum flow capacity at the high bypass ratios. Additionally, there is a significantly faster increase in the flow capacity of the “1 + 2” split fans compared to that of the “2 + 1” split fans. Furthermore, when the flow capacity of the split fans reaches its maximum, both the efficiency and stall margin achieve their optimal values, indicating that the corresponding bypass ratio is optimal.

Funder

Aero-Engines and Gas Turbines Basic Science Center Project

National Defense Science and Technology Key Laboratory Fund Project

Fundamental Research Funds for the Central Universities

Publisher

MDPI AG

Reference17 articles.

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3. Performance Analysis of a Three-Stream Adaptive Cycle Engine during Throttling;Chen;Int. J. Aerosp. Eng.,2018

4. Thrust performance optimization calculation and analysis of triple bypass variable cycle engine;Han;J. Aerosp. Power,2018

5. Allan, R.D. (1979, January 18–20). General Electric Company Variable Cycle Engine Technology Demonstrator Program. Proceedings of the 15th Joint Propulsion Conference, Las Vegas, NV, USA.

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