NASA NTRS · 19860002007
Lateral dampers for thrust bearings
Abstract
The development of lateral damping schemes for thrust bearings was examined, ranking their applicability to various engine classes, selecting the best concept for each engine class and performing an in-depth evaluation. Five major engine classes were considered: large transport, military, small general aviation, turboshaft, and non-manrated. Damper concepts developed for evaluation were: curved beam, constrained and unconstrained elastomer, hybrid boost bearing, hydraulic thrust piston, conical squeeze film, and rolling element thrust face.
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Hibner, D. H., Szafir, D. R.. 1985-08-01. Lateral dampers for thrust bearings. https://ntrs.nasa.gov/citations/19860002007
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