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contributor authorBaker, C.
contributor authorRahmani, R.
contributor authorTheodossiades, S.
contributor authorRahnejat, H.
contributor authorFitzsimons, B.
date accessioned2017-05-09T01:17:40Z
date available2017-05-09T01:17:40Z
date issued2015
identifier issn1528-8919
identifier othergtp_137_03_032512.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/157899
description abstractEnergy losses in an internal combustion engine are either thermal or parasitic. The latter are the mechanical inefficiencies, chiefly as the result of generated friction. Nearly half of these losses are attributed to the piston–cylinder system. During idle and at low engine speeds, friction is the major contributor to the overall engine losses. In particular, the rather small top compression ring accounts for a disproportionate share. Therefore, detailed understanding of compression ring tribology/dynamics (referred to as tribodynamics) is essential. Moreover, the ring’s primary sealing function may be breached by its elastodynamic behavior. The reported analyses in literature do not account for the transient nature of ring elastodynamics, as an essential feature of ring–bore tribology. The transient inplane dynamics of incomplete rings are introduced in the analysis and verified using a finite element analysis (FEA) model, in order to address this shortcoming. The methodology is then coupled with the tribological analysis of the top compression ring. Comparison is made with experimental measurements which show the validity of the proposed method. The radial inplane elastodynamic response of the ring improves the accuracy of the frictional power loss calculations.
publisherThe American Society of Mechanical Engineers (ASME)
titleOn the Effect of Transient In Plane Dynamics of the Compression Ring Upon Its Tribological Performance
typeJournal Paper
journal volume137
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4028496
journal fristpage32512
journal lastpage32512
identifier eissn0742-4795
treeJournal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 003
contenttypeFulltext


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