Research on Oil–Gas Two-Phase Flow Characteristics and Improvement of Aero-Engine Bearing Chamber
Abstract
:1. Introduction
2. Numerical Method
2.1. Control Equation of Two-Phase Flow in Bearing Chamber
- 1.
- Two-phase flow mixture model
- 2.
- Continuity equation
- 3.
- Momentum equation
- 4.
- Energy equation
- 5.
- Turbulent flow model
2.2. Geometric Structure of Bearing Cavity
2.3. Mesh and Boundary Conditions
2.4. Accuracy Verification of Numerical Method
3. Analysis of Two-Phase Flow Field Characteristics
3.1. Analysis of Calculation Results of Embedded Improvement Scheme
3.1.1. Leakage Analysis
3.1.2. Analysis of Volume Fraction of Lubricating Oil in Cavity
3.1.3. Scavenge Efficiency Analysis
3.2. Analysis of Calculation Results of Slope Improvement Scheme
3.2.1. Leakage Analysis
3.2.2. Analysis of Volume Fraction of Lubricating Oil in Cavity
3.2.3. Scavenge Efficiency Analysis
3.3. Analysis of Calculation Results of Combined Improvement Scheme
3.3.1. Leakage Analysis
3.3.2. Analysis of Volume Fraction of Lubricating Oil in Cavity
3.3.3. Scavenge Efficiency Analysis
3.4. Analysis of Flow Improvement Mechanism
4. Conclusions
- (1)
- Compared with the conventional bearing chamber, the vent wall embedded in the improved scheme can effectively block the lubricating oil in the cavity. At the same time, with the increase in embedding depth, the amount of lubricating oil flowing out from the vent is further reduced, the amount of lubricating oil flowing out from the return port is further increased, the volume fraction of lubricating oil in the cavity is further increased and the scavenge efficiency is further improved.
- (2)
- The slope improvement scheme is beneficial to the oil on the right side of scavenge port to flow into the scavenge port, and the oil accumulation area on the right side of the scavenge port is obviously suppressed. At the same time, with the increase in the depth of the oil return groove, the drag effect of the air shear force in the cavity on the oil near the scavenge port is further weakened, the volume fraction of the oil in the cavity is further reduced and the scavenge efficiency is further improved.
- (3)
- The combined improvement scheme will take into account the advantages of the embedded improvement and the slope improvement scheme, effectively inhibit the outflow of lubricating oil from the vent and then make more lubricating oil flow out of the oil return port, and the scavenge efficiency is greatly improved. Compared with the conventional bearing chamber structure, when the oil flow rate is 200L / h and the speed is 15000r / min, the scavenge efficiencies of the three improved schemes are the most obvious, and the scavenge efficiencies of the embedded, slope and combined improvement schemes are increased by 20.19%, 13.43% and 37.94%, respectively.
Author Contributions
Funding
Data Availability Statement
Conflicts of Interest
References
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Parameter | Normal | Embed | Slope | ES |
---|---|---|---|---|
Rotation radius r/(mm) | 72 | 72 | 72 | 72 |
Height e/(mm) | 32 | 32 | 32 | 32 |
Width b/(mm) | 48 | 48 | 48 | 48 |
Port diameter d/(mm) | 36 | 36 | 36 | 36 |
Tangential angle α/(o) | 0 | 0 | 45 | 45 |
Inlet height H/(mm) | 16 | 16 | 16 | 16 |
Structure | Parameter | Structure | Parameter |
---|---|---|---|
Rotation radius rsh/(mm) | 62 | Height of bearing cavity h1/(mm) | 28 |
Bearing cavity width b/(mm) | 46 | Diameter of vent d/(mm) | 17 |
Diameter of scavenge d/(mm) | 17 | Height of vent h2/(mm) | 40 |
Height of scavenge h2/(mm) | 40 |
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Ren, G.; Li, Y.; Zhao, H.; Yan, Y.; Xu, W.; Sun, D. Research on Oil–Gas Two-Phase Flow Characteristics and Improvement of Aero-Engine Bearing Chamber. Lubricants 2023, 11, 360. https://doi.org/10.3390/lubricants11090360
Ren G, Li Y, Zhao H, Yan Y, Xu W, Sun D. Research on Oil–Gas Two-Phase Flow Characteristics and Improvement of Aero-Engine Bearing Chamber. Lubricants. 2023; 11(9):360. https://doi.org/10.3390/lubricants11090360
Chicago/Turabian StyleRen, Guozhe, Yanpeng Li, Huan Zhao, Yang Yan, Wenfeng Xu, and Dan Sun. 2023. "Research on Oil–Gas Two-Phase Flow Characteristics and Improvement of Aero-Engine Bearing Chamber" Lubricants 11, no. 9: 360. https://doi.org/10.3390/lubricants11090360
APA StyleRen, G., Li, Y., Zhao, H., Yan, Y., Xu, W., & Sun, D. (2023). Research on Oil–Gas Two-Phase Flow Characteristics and Improvement of Aero-Engine Bearing Chamber. Lubricants, 11(9), 360. https://doi.org/10.3390/lubricants11090360