Loughborough University
Leicestershire, UK
LE11 3TU
+44 (0)1509 263171
Loughborough University

Loughborough University Institutional Repository

Please use this identifier to cite or link to this item: https://dspace.lboro.ac.uk/2134/25919

Title: Coupled elastodynamics of piston compression ring subject to sweep excitation
Authors: Turnbull, Robert
Mohammadpour, Mahdi
Rahmani, Ramin
Rahnejat, Homer
Offner, Gunter
Keywords: Compression ring
In-plane dynamics
Out-of-plane dynamics
Issue Date: 2017
Publisher: © The authors. Published by SAGE Journals
Citation: TURNBULL, R., ...et al, 2017. Coupled elastodynamics of piston compression ring subject to sweep excitation. Proceedings of the Institution of Mechanical Engineers, Part K: Journal of Multi-body Dynamics, 231(3), pp. 469–479.
Abstract: The piston compression ring’s primary function is to seal the combustion chamber, thus mitigating gas leakage to the crankcase and avoiding loss of pressure loading. As a result the ring is meant to conform closely to the cylinder surface which promotes increased friction. The compression ring is subjected to combustion pressure loading, ring tension, varying inertial force and friction. It is a slender ring of low mass, thus undergoes complex elastodynamic behaviour, when subjected to a multitude of forces. These motions occur in the ring’s radial in-plane and axial out-of-plane dynamics, which comprise flutter, ring axial jump, compression-extension, ring twist and rotational drag. An implication of these motions can be loss of sealing, gas blow-by, loss of power and lubricant degradation/oil loss, to name but a few. Consequently, understanding and accurately predicting ring dynamic behaviour under transient conditions is an important step in any subsequent modelling for evaluation of cylinder system efficiency. There have been a plethora of investigations for ring dynamics, often decoupling the ring behaviour in its in-plane and out-of-plane motions. This approach disregards any transfer of dynamic energy from one degree of freedom to another which is only applicable to rectangular ring cross-sections. Alternatively, there are computationally intensive approaches such as finite element analysis (FEA) which are not conducive for inclusion in any subsequent system level engine modelling where ring response alters in an instantaneous manner. This would require embedded FEA within a transient analysis. This paper presents a finite difference numerical analysis for coupled in-plane and out-of-plane motions of compression rings with practical cross-sectional geometries, which are mostly not rectangular. The formulated method can be integrated into a system level transient cyclic analysis of ring-bore contact. The presented approach takes into account the energy transfer between different degrees of freedom. The predictions are validated against precise non-contact measurements of ring elastodynamic behaviour under amplitude-frequency sweeps. This approach has not hitherto been reported in literature and constitutes the main contribution of the paper.
Description: This article is distributed under the terms of the Creative Commons Attribution 4.0 License (http://www.creativecommons.org/licenses/by/4.0/) which permits any use, reproduction and distribution of the work without further permission provided the original work is attributed as specified on the SAGE and Open Access pages (https://us.sagepub.com/en-us/nam/open-access-at-sage).
Sponsor: This work was supported by the Engineering and Physical Science Research Council (EPSRC) and AVL List GmbH under the EPSRC-CDTei collaborative funding.
Version: Published
DOI: 10.1177/1464419317725942
URI: https://dspace.lboro.ac.uk/2134/25919
Publisher Link: https://doi.org/10.1177/1464419317725942
ISSN: 2041-3068
Appears in Collections:Published Articles (Mechanical, Electrical and Manufacturing Engineering)

Files associated with this item:

File Description SizeFormat
1464419317725942.pdfPublished version1.02 MBAdobe PDFView/Open


SFX Query

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.