Research Papers: Gas Turbines: Structures and Dynamics

A Computational Fluid Dynamics Simulation of Oil–Air Flow Between the Cage and Inner Race of an Aero-engine Bearing

[+] Author and Article Information
Akinola A. Adeniyi

Department of Motorsports
and Mechanical Engineering,
School of Engineering,
University of Central Lancashire,
Preston PR1 2HE, UK
e-mail: aadeniyi@uclan.ac.uk

Hervé Morvan

Gas Turbine and Transmissions
Research Centre (G2TRC),
The University of Nottingham,
Nottingham NG7 2RD, UK
e-mail: herve.morvan@nottingham.ac.uk

Kathy Simmons

Gas Turbine and Transmissions
Research Centre (G2TRC),
The University of Nottingham,
Nottingham NG7 2RD, UK
e-mail: kathy.simmons@nottingham.ac.uk

1Corresponding author.

Contributed by the Structures and Dynamics Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received June 20, 2016; final manuscript received June 28, 2016; published online September 8, 2016. Editor: David Wisler.

J. Eng. Gas Turbines Power 139(1), 012506 (Sep 08, 2016) (8 pages) Paper No: GTP-16-1245; doi: 10.1115/1.4034210 History: Received June 20, 2016; Revised June 28, 2016

In aero-engines, the shafts are supported on bearings that carry the radial and axial loads. A ball bearing is made up of an inner race, an outer race, and a cage, which contains the balls, these together comprise the bearing elements. The bearings require oil for lubrication and cooling. The design of the bearing studied in this work is such that the oil is fed to the bearing through holes/slots in the inner race. At each axial feed location, the oil is fed through a number of equispaced feedholes/slots but there are a different number of holes at each location. Once the oil has passed through the bearing, it sheds outward from both sides into compartments known as the bearing chambers. A number of studies have been carried out on the dynamics of bearings. Most of the analyses consider the contributions of fluid forces as small relative to the interaction of the bearing elements. One of the most sophisticated models for a cage–raceway analysis is based on the work of Ashmore et al. (2003, “Hydrodynamic Support and Dynamic Response for an Inner-Piloted Bearing Cage,” Proc. Inst. Mech. Eng. Part G, 217, pp. 19–28], where the cage–raceway is considered to be a short journal bearing divided into sectors by the oil feeds. It is further assumed that the oil exits from the holes and forms a continuous block of oil that exits outward on both sides of the cage–raceway. In the model, the Reynolds equation is used to estimate the oil dynamics. Of interest in this current work is the behavior of the oil and air within the space bounded by the cage and inner race. The aim is to determine whether oil feed to the bearing can be modeled as coming from a continuous slot or if the discrete entry points must be modeled. A volume of fluid (VOF) computational fluid dynamics (CFD) approach is applied. A sector of a ball bearing is modeled with a fine mesh, and the detailed simulations show the flow behavior for different oil splits to the three feed locations of the bearing, thus providing information useful to understanding oil shedding into the bearing chambers. This work shows that different flow behaviors are predicted by models where the oil inlets through a continuous slot are compared to discrete entry holes. The form and speed of oil shedding from the bearing are found to depend strongly on shaft speed with the shedding speed being slightly higher than the cage linear speed. The break-up pattern of oil on the cage inner surface suggests that smaller droplets will be shed at higher shaft speed.

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Taylor, G. , 1923, “ Stability of a Viscous Liquid Contained Between Two Rotating Cylinders,” Philos. Trans. R. Soc. London, Ser. A, 223, pp. 289–349. [CrossRef]
Farrall, M. , Hibberd, S. , Simmons, K. , and Gorse, P. , 2006, “ A Numerical Model for Oil Film Flow in an Aeroengine Bearing Chamber and Comparison to Experimental Data,” ASME J. Eng. Gas Turbines Power, 128(1), pp. 111–117. [CrossRef]
Williams, J. , 2008, “ Thin Film Rimming Flow Subject to Droplet Impact at the Surface,” Ph.D. thesis, The University of Nottingham, Nottingham, UK. http://eprints.nottingham.ac.uk/10670/
Kay, E. , Hibberd, S. , and Power, H. , 2014, “ A Depth-Averaged Model for Non-Isothermal Thin-Film Rimming Flow,” Int. J. Heat Mass Transfer, 70, pp. 1003–1015. [CrossRef]
Kakimpa, B. , Morvan, H. P. , and Hibberd, S. , 2015, “ Solution Strategies for Thin Film Rimming Flow Modelling,” ASME Paper No. GT2015-43503.
Adeniyi, A. , Morvan, H. , and Simmons, K. , 2013, “ Droplet-Film Impact Modelling Using a Coupled DPM-VoF Approach,” XXI International Symposium on Air Breathing Engines (ISABE), AIAA, Busan, South Korea, Paper No. ISABE-2013-1419.
Adeniyi, A. A. , Morvan, H. P. , and Simmons, K. A. , 2014, “ A Transient CFD Simulation of the Flow in a Test Rig of an Aeroengine Bearing Chamber,” ASME Paper No. GT2014-26399.
Tkaczyk, P. , and Morvan, H. , 2012, “ SILOET: CFD Modelling Guidelines of Engine Sumps—Oil and Air Flows Simulation of Bearing Chambers and Sumps Using an Enhanced Volume of Fluid (VOF) Method,” UTC in Gas Turbine Transmission Systems, The University of Nottingham, Nottingham, UK, Technical Report No. JF82/PT/06.
Chandra, B. , Simmons, K. , Pickering, S. , Colliocot, S. , and Wiedemann, N. , 2012, “ Study of Gas/Liquid Behaviour Within an Aeroengine Bearing Chamber,” ASME Paper No. GT2012-68753.
Glahn, A. , Blair, M. , Allard, K. , Busam, S. , O. Schfer , and Wittig, S. , 2003, “ Disintegration of Oil Films Emerging From Radial Holes in a Rotating Cylinder,” ASME J. Eng. Gas Turbines Power, 125(4), pp. 1011–1020. [CrossRef]
Crouchez-Pillot, A. , and Morvan, H. , 2014, “ CFD Simulation of an Aeroengine Bearing Chamber Using an Enhanced Volume of Fluid (VOF) Method,” ASME Paper No. GT2014-26405.
Adeniyi, A. A. , Morvan, H. P. , and Simmons, K. A. , 2015, “ A Multiphase Computational Study of Oil-Air Flow Within the Bearing Sector of Aeroengines,” ASME Paper No. GT2015-43496.
Kannel, J. , and Bupara, S. , 1978, “ A Simplified Model of Cage Motion in Angular Contact Bearings Operating in the ehd Lubrication Regime,” ASME J. Tribol., 100(3), pp. 395–403.
Gupta, P. , 2012, Advanced Dynamics of Rolling Elements, Springer Science and Business Media, New York, pp. 12–30.
Ashmore, D. R. , Williams, E. J. , and McWilliam, S. , 2003, “ Hydrodynamic Support and Dynamic Response for an Inner-Piloted Bearing Cage,” Proc. Inst. Mech. Eng., Part G, 217, pp. 19–28. [CrossRef]
Jones, A. B. , 1959, “ Ball Motion and Sliding Friction in Ball Bearings,” ASME J. Basic Eng., 81(3), pp. 1–12.
Gupta, P. , 1979, “ Dynamics of Rolling Element Bearings—Part 1: Cylindrical Roller Bearing Analysis,” ASME J. Lubr. Technol., 101(3), pp. 293–302.
Sum, W. W. , 2005, “ Dynamic Analysis of Angular-Contact Ball Bearings and the Influence of Cage Geometry,” Ph.D. thesis, The University of Nottingham, Nottingham, UK.
Ai, X. , and Moyer, C. A. , 2000, “ Rolling Element Bearings,” Modern Tribology Handbook, CRC Press, Boca Raton, FL, Chap. 28.
Foord, C. , 2014, “ High-Speed Ball Bearing Analysis,” Proc. Inst. Mech. Eng. Part G, 220, pp. 537–544.
Wang, W.-Z. , Hu, L. , Zhang, S.-G. , Zhao, Z.-Q. , and Ai, S. , 2014, “ Modelling Angular Contact Ball Bearing Without Raceway Control Hypothesis,” Mech. Mach. Theory, 82, pp. 154–172. [CrossRef]
Changqing, B. , and Qingyu, X. , 2006, “ Dynamic Model of Ball Bearings With Internal Clearance and Waviness,” J. Sound Vib., 294, pp. 23–48.
Sussman, M. , and Puckett, E. , 2000, “ A Coupled Level Set and Volume-of-Fluid Method for Computing 3D and Axisymmetric Incompressible Two-Phase Flows,” J. Comput. Phys., 162(2), pp. 301–337. [CrossRef]
ANSYS, 2015, “ ANSYS Fluent Theory Guide,” ANSYS, Canonsburg, PA.


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Fig. 1

Schematic representation of bearing in test facility

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Fig. 2

Under-race oil feed

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Fig. 3

Illustration of the model of Ashmore et al. [15] for an oil-fed cage–raceway

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Fig. 4

Cage–inner race periodic geometry

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Fig. 5

A section of the mesh used for the periodic geometry cases

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Fig. 6

Cage–inner race full 360 deg rotating geometry

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Fig. 8

Oil in the feed pipe

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Fig. 9

Oil wetting of the cage for the sector models

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Fig. 10

Oil behavior in hole and on cage for 360 deg case

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Fig. 11

Cage oil wetting from a slotted feed

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Fig. 12

Oil spread on the cage

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Fig. 13

Oil exit size factor

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Fig. 14

Exit oil velocity

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Fig. 15

Jet leading/trailing film thickness




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