2014
DOI: 10.15680/ijirset.2014.0309036
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Design, Construction and Testing Of a Burner That Uses an Admixture of Used Engine Oil and Kerosene for Foundry Application

Abstract: An admixture burner for the atomization and combustion of used engine oil and kerosene for foundry application was constructed and tested to reduce the cost of operation in the foundry since the fuel is easily accessible, in addition to avoid pollution by the incessant dumping of the used engine oil. The nozzle, springs, screws, tank and the fuel hose were predominantly used materials for its construction. A test was carried out to determine the time taken for some selected engineering materials (copper, alumi… Show more

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Cited by 2 publications
(3 citation statements)
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“…Madu [2] designed, constructed and tested a burner that uses an admixture of used engine oil and kerosene for foundry application. Tests were carried out to determine the time taken to melt 1 kg each of the selected engineering materials (copper, aluminum, brass, and lead).…”
Section: Introductionmentioning
confidence: 99%
“…Madu [2] designed, constructed and tested a burner that uses an admixture of used engine oil and kerosene for foundry application. Tests were carried out to determine the time taken to melt 1 kg each of the selected engineering materials (copper, aluminum, brass, and lead).…”
Section: Introductionmentioning
confidence: 99%
“…Based on the findings of the study, optimization of the fuel and air flow parameters and re-design of the burner to incorporate automatic ignition system would significantly improve its performance. Madu et al [6] examined the performance of a WLO burner where WLO and kerosene were mixed to ease ignition and increase efficiency. The thermal efficiency of the burner was reported as 66%.…”
Section: Introductionmentioning
confidence: 99%
“…World Journal of Engineering and TechnologyMass flow rate of air to the burner, is calculated as shown in Equation(11) [6] mass flow rate of air; ρ = density of air = 1.225 kg/m 3 ; A = cross-sectional area of the impeller; u = velocity of air flow to the burner;…”
mentioning
confidence: 99%