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– An Alternative Cavitation Analysis University of Arkansas
2007 STLE/ASME International Joint Tribology Conference Rolling Stream Trails – An Alternative Cavitation Analysis Coda H. Pan Global Technology Tae Ho Kim Texas A&M University Joseph J. Rencis University of Arkansas IJTC October
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Eccentric rotating shaft
INTRODUCTION Fluid film bearings generate hydrodynamic pressures in the region of local converging film thickness due to an eccentric rotating shaft Cavitation zone Bearing Eccentric rotating shaft Z Ω Fluid film At fluid film trailing edge, low film pressure close to ambient pressure causes cavitations (film rupture).
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Previous works Fluid film cavitations
Gumbel(1914): Half-Sommerfeld solution (No sub-ambient pressure due to rupture) Swift (1932) and Stieber(1933): Reynolds boundary condition (Pressure gradient is zero at the boundary of the void) Floberg (1957): Fluid transport streamers associated to the tensile strength of the fluid. Olsson (1965): A trans-rupture continuity equation to determine the speed of a moving rupture point Dowson (1974): Visual observations of the ruptured film in the steady-state operation Elrod (1981): Universal cavitation algorithm. Two dimensional rupture model in the bearing film. Most comprehensive model to date.
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Simplified Film pressure field
Reynolds boundary condition (dP/dx = 0, P=0) Half-Sommerfeld (P=0) Centerline pressures for Gumbel and Reynolds boundary conditions. Reynolds boundary may not satisfy flow continuity in the cavitation zone except at its onset.
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Fluid film cavitation Time varying rupture boundary
Adhered film flowing parallel to the shear surface velocity Time increases Half-Sommerfeld Steady-state Transient film model
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Width fraction of streamer in rupture front: 0< γ <1
Objective Elrod cavitation algorithm is most popular but does not treat the Olsson equation which considers the morphology model (partial film separation) for the ruptured region. Full film New cavitation model Emphasizing coexistence of ligament and ventilated cavitation regions side by side in rupture front. Speed increases Full film Void Film extending A A Width fraction of streamer in rupture front: 0< γ <1 B B Dowson (1974)
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Fluid film flow velocity profiles
A-A Coexistence of ligament and ventilated cavitation regions side by side in rupture front. Wetting terminated Wet void in rupture front Gumbel rupture Wetting trace Width fraction of streamer in rupture front: 0≤ γ <1 ωR Ventilated cavitation regions Streamer in rupture front ωR/2 ωR ligament regions B-B
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Schematic of journal bearings
L/D < 2 Long bearing, i.e. dp/dz ~ 0 Where D = Diameter L = Length P = Film pressure Z= axial coordinate One-dimensional analysis is useful for long journal bearings
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Governing equation (filled fluid film)
1D Reynolds equation Dimensionless form where where
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General solutions Generalized Gumbel solution with
Swift-Stieber Steady state boundary condition: is determined iteratively. - Existence of a steady state rupture location,
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Trans-rupture continuity (Olsson)
Rupture point speed Formation point speed No supply groove
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Rupture point speed vs rupture point angle
Time increases With a fixed formation point angle of – 90°, the uncavitated region is 292° (= 90°+ 202 °)
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Phase Chart With a fixed formation point angle of – 155°, the uncavitated region is eliminated. Wet initial void Dry initial void (γ = 0) Solution approach from Gumbel to Swift-Stieber boundary. Wet initial void increases the uncavitated region when compared to that with dry initial void.
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Rupture boundary speed
γ= γ= γ= γ= γ= Time increases Initial rupture point speed increases as the wet void portion (γ) increases. Final rupture point speed decreases to zero.
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Time for arrival at the rupture location
γ= γ= γ= γ= γ= Time for arrival at the current rupture boundary location increases as the wet void portion (γ) increases.
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Formation boundary speed
γ= γ= γ= γ= γ= Time increases Initial formation point speed increases as the wet void portion (γ) increases. Final formation point speed decreases to zero.
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Formation point angle γ= γ= γ= γ= γ= Formation point angle has different inverse-trajectories with different wet void portion (γ), as rupture point angle increases. Initial and final angles are identical.
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Fully filled film thickness
No cavitation with fully filled fluid film
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Swift-Stieber pressure and film thickness
In cavitated region, pressure is zero until the film is reformed. Pressure gradient is zero at film rupture front.
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Snapshots of pressure and film thickness fields.
Dry initial void (γ=0) Pressure field Snapshots of pressure and film thickness fields. As time increase, Solutions move from Gumbel boundary to Swift-Stieber boundary Time increases Time increases Film thickness field Time increases
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Snapshots of pressure and film thickness fields.
Wet initial void (γ=1) Pressure field Snapshots of pressure and film thickness fields. With wet initial void, positive pressure and uncavitated film region increases. Time increases Time increases Film thickness field Time increases Time increases
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Swift-Stieber pressure profile
Present study with two component rupture front conditions predicts different pressure from full Sommerfeld pressure
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Conclusions Modeled film rupture front with two (wet and dry initial voids) boundary conditions. => Verified by experimentally observation. Wet and dry initial voids show different pressure and film thickness behaviors. Pressure profile is different from that obtained using Elrod Cavitation Algorithm Alternative cavitation model. Demonstrate viability of Rolling Stream Trail cavitation analysis.
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