e xperimental r esponse of an o pen e nds sfd and a s
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E XPERIMENTAL R ESPONSE OF AN O PEN E NDS SFD AND A S EALED E NDS SFD - PowerPoint PPT Presentation

TRC-SFD-01-2016 May TRC Project 2016 400124-00099 Year V E XPERIMENTAL R ESPONSE OF AN O PEN E NDS SFD AND A S EALED E NDS SFD Luis San Andrs Sung-Hwa Jeung Graduate Research Assistant Mast-Childs Chair Professor Squeeze Film Dampers


  1. TRC-SFD-01-2016 May TRC Project 2016 400124-00099 Year V E XPERIMENTAL R ESPONSE OF AN O PEN E NDS SFD AND A S EALED E NDS SFD Luis San Andrés Sung-Hwa Jeung Graduate Research Assistant Mast-Childs Chair Professor

  2. Squeeze Film Dampers (SFD) Lubricant Anti-rotation film pin Whirl motion from the Shaft journal squeezes Journal Ball bearing the lubricant film and generates dynamic pressures that aid to damp Housing the rotor vibrations. Aid to attenuate rotor vibrations, suppress system instabilities, and provide mechanical isolation. Too little damping may not be enough to reduce vibrations. Too much damping may lock damper & will degrade system performance. 2

  3. SFD Test Rig – cut section Test Journal Bearing Piston ring seal Cartridge (location) Supply orifices (3) Main support Flexural rod (4) Rod (4, 8, 12) Journal Base Pedestal in

  4. Lubricant flow path ISO VG 2 oil Oil in inlet ISO VG 2 23 ° C (73 ° F) Supply temperature, T in Lubricant viscosity @ T in , μ 2.6 cP 800 kg/m 3 Lubricant density, ρ 4

  5. SFD Test Rig – cut section Piston ring seals Geometry (three feed holes 120 o apart) Short length SFD Journal Diameter, D 12.7 cm (5.0 in) Land Length, L 2.54 cm (1.0 in) 254 μm (10.0 mil) L/D =0.2 Radial Land Clearance, c 7 Feed orifice Diameter, ϕ 2.54 mm (0.1 inch)

  6. Funded TRC (2015-2016) Justification End seals amplify viscous damping while reducing the flowrate and reducing air ingestion Evaluate the forced performance of sealed ends SFD. Tasks: 1.Test a short length ( L/D =0.2), Sealed ends SFD with nominal clearance 254 μm (10 mil) . 2.Conduct dynamic load tests for motions from centered and off-centered positions. 3.Evaluate SFD dynamic forced performance. 6

  7. Piston rings as end seals Reduce flow rate and side leakage  raise film dynamic pressures and increase damping while also reduce air ingestion. Leakage Housing Journal Film Lubricant Piston rings Piston ring design as an end seal is highly empirical. 7

  8. Leakage vs lub. supply pressure 10 Damper A Inlet flow Clearance : 254 μ m Land length : 25.4 mm 8 Flow rate [liter/min] Open Test data: ends Q in open ends Q B open ends 6 Q in sealed ends Q B sealed ends Bottom land flow 4 Inlet flow Sealed 2 ends 0 0.0 0.5 1.0 1.5 2.0 2.5 Feed hole pressure P S [bar(g)] Piston ring end seals are effective in reducing the side leakage .

  9. How do the whirl amplitude & static eccentricity affect sealed ends SFD force coefficients?

  10. Sealed ends SFD: Damping coeff. Direct Cross-coupled C XX ~C YY Damping grows with orbit amplitude r while remain constant with static eccentricity ( e s ) 10

  11. Sealed ends SFD: Inertia coeff. Direct Cross-coupled M XX ~M YY Direct added masses increase with static eccentricity, but decrease with orbit size ( r ). 11

  12. How much more damping if damper has end seals?

  13. Open ends SFD vs sealed ends SFD ~ 12 Sealed ends SFD gives 12X more damping and 11X more added ~ 11 mass than open ends SFD at small r/c A 13

  14. How do the seal conductance affect sealed ends SFD force coefficients? Two pairs of piston seals Leaks more, Leaks less, less resistance more resistance

  15. Sealed ends Effect of flow conductance ( c A = 254 μ m) At fixed ~ 20% Leaks less, more resistance Leaks more, less resistance Two pairs of C   ave S 2 1.6 piston rings C  ave S 1 Sealed ends SFD with smaller flow conductance gives ~20% larger damping at r/c A =0.6. However, both results are within uncertainty range 15

  16. How does the lubricant supply pressure affect force coefficients?

  17. Sealed ends Effect of flow supply pressure ( c A = 254 μ m) At fixed P   in 2 4 P  in 1 Larger supply pressure r/c A =0.15 SFD supplied with higher pressure gives ~26% - 50% more damping. Differences increase as eccentricity e/c A increases. 17

  18. Pressure sensors in housing

  19. Pressure & Film Thickness vs. time P 4 Journal Flat pressure zones BC Flat pressure zones Peak pressure increases with orbit amplitude. Damper with larger P in-2 generates more dynamic pressure and reduces air ingestion. Oil vapor cavitation is at constant pressure.

  20. Visual inspection Effect of feed pressure ( P in ) to reduce bubbly mixture (air in lubricant).

  21. Visual inspection Top oil collector r/c A =0.45, ω =80Hz

  22. Comparison of Damper ( c =254 μ m (10 mil)) force coefficients: test data vs 2.54 cm predictions (1.0 in) Piston ring seals L/D =0.2, 25.4 mm (1 inch) land

  23. Sealed ends Damping: predictions & tests ( c A = 254 μ m) e s /c A =0.0 Good correlation : predictions vs. tests 23

  24. Conclusion (a) Damping coefficient grows with orbit amplitude ( r ), but not with static eccentricity ( e s ) . Added mass increases with amplitude ( r ), but decreases with eccentricity ( e s ). (a) Ends sealed SFD provide 12x more damping and 11x more added mass than open ends SFD. (b) A higher lubricant inlet pressure produces larger damping and avoids air ingestion. (c) Predictive model reproduces test data. 24

  25. 2016 proposal to TRC Engine qualification requires dampers to operate with oil delivery failure over a short period of time (~30 s), due to a malfunction or under a sudden 0 g maneuver load. 1. Machine journal with film land length and diameter ( L/D =0.2) and film clearance of 5 mil. 2. Characterize flow conductance of an open ends damper. 3. Perform transient - dynamic load measurements (fixed amplitude and frequency) while the supply of lubricant is suddenly cut. 4. Perform analysis to model test system, compare predictions vs. test data to validate damper flow model. Objective: evaluate the performance of a SFD with film starvation due to sudden loss of oil supply. 25

  26. TRC Budget 2016-2017 Year VI Year VI Support for graduate student (20 h/week) x $ 2,400 x 12 $ 28,800 months Fringe benefits (2.7%) and medical insurance ($360 /month) $ 4,995 Supplies for test rig (Lubricant $ 700, Machining a new $ 2,100 journal $ 1400) Tuition three semesters ($ 363 credit hour x 24 h/year) $ 9,090 $ 44,985 The TAMU SFD research program is the most renown in the world. The proposed research is of interest for SFDs applied in gas turbines, hydrodynamic bearings in compressors, cutting tool and grinding machines. 26

  27. Acknowledgments Turbomachinery Research Consortium & Pratt & Whitney Engines Questions (?) 27

  28. Back up slide Predicted damping vs flow conductance: 28

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