Validation of a blowby model using experimental results in motoring condition with the change of compression ratio and engine speed
Autor: | E. Abdi Aghdam, M. M. Kabir |
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Rok vydání: | 2010 |
Předmět: |
Fluid Flow and Transfer Processes
Materials science Mechanical Engineering General Chemical Engineering Flow (psychology) Aerospace Engineering Thermodynamics Mechanics Pressure sensor Cylinder (engine) law.invention Integrated engine pressure ratio Nuclear Energy and Engineering Internal combustion engine law Compression ratio Piston ring Body orifice |
Zdroj: | Experimental Thermal and Fluid Science. 34:197-209 |
ISSN: | 0894-1777 |
DOI: | 10.1016/j.expthermflusci.2009.10.021 |
Popis: | Blowby and gas flow through the cylinder–piston–ring crevices are phenomena that affect the engine performance and exhaust emissions. Also these phenomena influence the cylinder pressure and temperature and the charge amount during a cycle. The study and validation of a sub-model for these phenomena in the absence of engine combustion deducts all effects arisen from the combustion event. During the current study, blowby sub-model and gas flow through crevices under motoring conditions has been noticed using a volume–orifice theory and the experimental results measured from a research engine. Blowby geometric parameters, consisting of a few critical cross-section areas (orifice areas) and volumes (top land and inter-ring crevice volumes), were measured in ambient temperature and corrected for hot running conditions. The cylinder pressure during cycle was measured by a piezoelectric pressure transducer and the low pressure parts of the cycle were measured using a piezoresistive pressure transducer for referencing purposes. The obtained results show a very good agreement between experimentally measured pressure data and model output for three compression ratios of 7.6, 10.2, 12.4 and three engine speeds of 750, 1500 and 2000 rpm, so that the maximum deviation was almost 5%. The model predicted that the maximum mass loss increased with increase of compression ratio and decreased with increase of engine speed. Also the peak mass loss position happened within the range of 3–9°CA after top dead center. After occurrence of the maximum loss, a reverse flow from the top land crevice into the cylinder was predicted in the model. |
Databáze: | OpenAIRE |
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