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Title: Influence of in-plane dynamics of thin compression rings on friction in internal combustion engines
Authors: Baker, Christopher E.
Theodossiades, Stephanos
Rahnejat, Homer
Fitzsimons, Brian
Keywords: Compression ring
In-plane dynamics
Modal response
Mixed regime of lubrication
Issue Date: 2012
Publisher: © ASME
Citation: BAKER, C.E. ... et al, 2012. Influence of in-plane dynamics of thin compression rings on friction in internal combustion engines. Journal of Engineering for Gas Turbines and Power-Transaction of the ASME, 134 (9), 092801, 11pp.
Abstract: The compression ring-bore conjunction accounts for significant frictional parasitic losses relative to its size. The prerequisite to improving the tribological performance of this contact is a fundamental understanding of ring dynamics within the prevailing transient nature of regime of lubrication. Studies reported thus far take into account ring-bore conformance, based on static fitment of the ring within an out-of-round bore, whose out-of-circularity is affected by manufacturing processes, surface treatment and assembly. The static fitment analyses presume quasi-static equilibrium between ring tension and gas pressure loading with generated conjunctional pressures. This is an implicit assumption of ring rigidity whilst in situ. The current analysis considers the global modal behaviour of the ring as an eigenvalue problem, thus including its dynamic in-plane behaviour in the tribological study of a mixed-hydrodynamic regime of lubrication. The results show that the contact transit time is shorter than that required for the ring to reach steady state condition. Hence, the conjunction is not only subject to transience on account of changing contact kinematics and varied combustion loading, but also subject to perpetual ring transient dynamics. This renders the ring-bore friction a more complex problem than usually assumed in idealised ring fitment analyses. An interesting finding of the analysis is increased ring-bore clearance at and in the vicinity of top dead centre, which reduces the ring sealing effect and suggests a possible increase in blow-by. The current analysis, integrating ring in-plane modal dynamics and mixed regime of lubrication includes salient features which are closer representation of practice, an approach which has not hitherto been reported in literature.
Description: This article was been accepted for publication in the Journal of Engineering for Gas Turbines and Power. The definitive version can be found at: http://dx.doi.org/10.1115/1.4006690
Sponsor: The authors wish to express their gratitude to Engineering and Physical Sciences Research Council (EPSRC) for the funding extended to the Encyclopaedic Program Grant (www.Encyclopaedic.org), under which this research is carried out in collaboration with a consortium of industry and academic institutions. In particular, the authors acknowledge the financial and technical support of Aston Martin Lagonda.
Version: Accepted for publication
DOI: 10.1115/1.4006690
URI: https://dspace.lboro.ac.uk/2134/13351
Publisher Link: http://dx.doi.org/10.1115/1.4006690
ISSN: 0742-4795
Appears in Collections:Published Articles (Mechanical, Electrical and Manufacturing Engineering)

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