NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Analytic Modeling of the Hydrodynamic, Thermal, and Structural Behavior of Foil Thrust BearingsA simulation and modeling effort is conducted on gas foil thrust bearings. A foil bearing is a self acting hydrodynamic device capable of separating stationary and rotating components of rotating machinery by a film of air or other gaseous lubricant. Although simple in appearance these bearings have proven to be complicated devices in analysis. They are sensitive to fluid structure interaction, use a compressible gas as a lubricant, may not be in the fully continuum range of fluid mechanics, and operate in the range where viscous heat generation is significant. These factors provide a challenge to the simulation and modeling task. The Reynolds equation with the addition of Knudsen number effects due to thin film thicknesses is used to simulate the hydrodynamics. The energy equation is manipulated to simulate the temperature field of the lubricant film and combined with the ideal gas relationship, provides density field input to the Reynolds equation. Heat transfer between the lubricant and the surroundings is also modeled. The structural deformations of the bearing are modeled with a single partial differential equation. The equation models the top foil as a thin, bending dominated membrane whose deflections are governed by the biharmonic equation. A linear superposition of hydrodynamic load and compliant foundation reaction is included. The stiffness of the compliant foundation is modeled as a distributed stiffness that supports the top foil. The system of governing equations is solved numerically by a computer program written in the Mathematica computing environment. Representative calculations and comparisons with experimental results are included for a generation I gas foil thrust bearing.
Document ID
20050203843
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Bruckner, Robert J.
(NASA Glenn Research Center Cleveland, OH, United States)
DellaCorte, Christopher
(NASA Glenn Research Center Cleveland, OH, United States)
Prahl, Joseph M.
(Case Western Reserve Univ. Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2005
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA/TM-2005-213811
E-15168
Report Number: NASA/TM-2005-213811
Report Number: E-15168
Meeting Information
Meeting: 2005 Annual Meeting and Exhibition, 60th Society of Tribologists and Lubrication Engineers
Location: Las Vegas, NV
Country: United States
Start Date: May 15, 2005
End Date: May 19, 2005
Sponsors: Society of Tribologists and Lubrication Engineers
Funding Number(s)
WBS: WBS 973-80-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available