Tribology of new thin compression ring of fired engine under controlled conditions-A combined experimental and numerical study.
Saved in:
| Title: | Tribology of new thin compression ring of fired engine under controlled conditions-A combined experimental and numerical study. |
|---|---|
| Authors: | Zavos, Anastasios1, Nikolakopoulos, Pantelis G.1 pnikolakop@upatras.gr |
| Source: | Tribology International. Dec2018, Vol. 128, p214-230. 17p. |
| Subjects: | Engine testing, Computational fluid dynamics, Surface roughness, Strain gages, Lubrication & lubricant testing |
| Abstract: | In this paper, a CFD model combined with experimental measurements of the ring deformations, in a single-cylinder fired engine, using a strain gauge through the cylinder bore is presented. The strain gauge data is analysed to measure the primary reflection due to friction between the thin compression ring and the cylinder wall. The findings show that the prediction of the calculated ring friction, needs the suitable surface roughness, particularly at TDC reversal. The experiments under cold controlled condition and low engine speed, proved that a higher contribution is noticeable by thin compression ring friction. In addition, the investigation of lubricant film and flow rate is shown that the thin profile design can affect the sealing performance momentary of compression ring. [ABSTRACT FROM AUTHOR] |
| Copyright of Tribology International is the property of Elsevier B.V. and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.) | |
| Database: | Engineering Source |
| FullText | Text: Availability: 0 |
|---|---|
| Header | DbId: egs DbLabel: Engineering Source An: 131334273 AccessLevel: 6 PubType: Academic Journal PubTypeId: academicJournal PreciseRelevancyScore: 0 |
| IllustrationInfo | |
| Items | – Name: Title Label: Title Group: Ti Data: Tribology of new thin compression ring of fired engine under controlled conditions-A combined experimental and numerical study. – Name: Author Label: Authors Group: Au Data: <searchLink fieldCode="AR" term="%22Zavos%2C+Anastasios%22">Zavos, Anastasios</searchLink><relatesTo>1</relatesTo><br /><searchLink fieldCode="AR" term="%22Nikolakopoulos%2C+Pantelis+G%2E%22">Nikolakopoulos, Pantelis G.</searchLink><relatesTo>1</relatesTo><i> pnikolakop@upatras.gr</i> – Name: TitleSource Label: Source Group: Src Data: <searchLink fieldCode="JN" term="%22Tribology+International%22">Tribology International</searchLink>. Dec2018, Vol. 128, p214-230. 17p. – Name: Subject Label: Subjects Group: Su Data: <searchLink fieldCode="DE" term="%22Engine+testing%22">Engine testing</searchLink><br /><searchLink fieldCode="DE" term="%22Computational+fluid+dynamics%22">Computational fluid dynamics</searchLink><br /><searchLink fieldCode="DE" term="%22Surface+roughness%22">Surface roughness</searchLink><br /><searchLink fieldCode="DE" term="%22Strain+gages%22">Strain gages</searchLink><br /><searchLink fieldCode="DE" term="%22Lubrication+%26+lubricant+testing%22">Lubrication & lubricant testing</searchLink> – Name: Abstract Label: Abstract Group: Ab Data: In this paper, a CFD model combined with experimental measurements of the ring deformations, in a single-cylinder fired engine, using a strain gauge through the cylinder bore is presented. The strain gauge data is analysed to measure the primary reflection due to friction between the thin compression ring and the cylinder wall. The findings show that the prediction of the calculated ring friction, needs the suitable surface roughness, particularly at TDC reversal. The experiments under cold controlled condition and low engine speed, proved that a higher contribution is noticeable by thin compression ring friction. In addition, the investigation of lubricant film and flow rate is shown that the thin profile design can affect the sealing performance momentary of compression ring. [ABSTRACT FROM AUTHOR] – Name: AbstractSuppliedCopyright Label: Group: Ab Data: <i>Copyright of Tribology International is the property of Elsevier B.V. and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract.</i> (Copyright applies to all Abstracts.) |
| PLink | https://search.ebscohost.com/login.aspx?direct=true&site=eds-live&db=egs&AN=131334273 |
| RecordInfo | BibRecord: BibEntity: Identifiers: – Type: doi Value: 10.1016/j.triboint.2018.07.034 Languages: – Code: eng Text: English PhysicalDescription: Pagination: PageCount: 17 StartPage: 214 Subjects: – SubjectFull: Engine testing Type: general – SubjectFull: Computational fluid dynamics Type: general – SubjectFull: Surface roughness Type: general – SubjectFull: Strain gages Type: general – SubjectFull: Lubrication & lubricant testing Type: general Titles: – TitleFull: Tribology of new thin compression ring of fired engine under controlled conditions-A combined experimental and numerical study. Type: main BibRelationships: HasContributorRelationships: – PersonEntity: Name: NameFull: Zavos, Anastasios – PersonEntity: Name: NameFull: Nikolakopoulos, Pantelis G. IsPartOfRelationships: – BibEntity: Dates: – D: 01 M: 12 Text: Dec2018 Type: published Y: 2018 Identifiers: – Type: issn-print Value: 0301679X Numbering: – Type: volume Value: 128 Titles: – TitleFull: Tribology International Type: main |
| ResultId | 1 |