Iranian Journal of Mechanical Engineering Transactions of ISME

Iranian Journal of Mechanical Engineering Transactions of ISME

Investigation of pilot fuel advancing time influences on dual fuelled engine(Diesel-Natural Gas) pollutant in various loads

Authors
Abstract
In this paper investigations performed on dual fueled constant speed diesel engine. At first; performance and emission of diesel engine investigated and after converting to dual fuel mode experimental tests performed on performance and emissions in different injection timing (at 14, 17, 20 degree before TDC) and loads (100%, 75%, 50%, 25%, 10% of full loads). Results show that in different loads and injections timing, amount of Nox and particle materials (PM) in dual fueled engine are lower than diesel engine. Amount of CO2 in dual fuelled mode have a little difference with diesel mode, although, it is lower than diesel engine. In loads lower than 75% load, amount of CO in diesel engine was lower than dual fuelled engine but in full load this term was inverse and have significant difference. Amount of HC in dual fuel mode was higher than diesel mode in all injections timing and loads.

Highlights

[1] Bin, H., Huang, Y., Wang, F., and Xie, F., "Numerical Simulation of Cold Flow Field of Aero-engine Combustors for Lean Blow Off Analysis", ASME Turbo Expo. Power for Land, Sea and Air, GT 45467, Vancouver, British Columbia, Canada, (2011).

 

[2] Rankin, D., "Lean Combustion Technology and Control", Second Edition, USA, California, Elsevier, (2016).

 

[3] Bin, H., Huang, Y., and Jianzhong, X., "A Hybrid Semi-empirical Model for Lean Blow-Out Limit Predictions of Aero-engine Combustors", Journal of Engineering for Gas Turbines and Power, Vol. 137, pp. 501-510, (2015).

 

[4] Zukowski, E., and Marbel, F., "The Role of Wake Transition in the Process of Flame Stabilization on Bluff Bodies", AGARD Combustion,Vol. 28, pp. 167–80, (1955).

 

[5] Mellor, A., "Design of Modern Turbine Combustors", Academic Press, San Diego, CA, (1990).

 

[6] Longwell, J., Frost, E., and Weiss, M., "Flame Stability in Bluff Body Recirculation Zones", Ind. Eng. Chem, Vol. 45, pp. 1629–1633, (1953).

 

[7] Bin, H., Huang, Y., and Wang, F., "CFD Predictions of LBO Limits for Aero-engine Combustors using Fuel Iterative Approximation", Chin. J. Aeronaut,Vol. 26, pp. 74–84, (2012).

 

[8] Lefebvre, A., "Gas Turbine Combustion", Fourth Edition, Printed by CRC Press Taylor and Francis Group, (2016).

 

[9] Bin, H., Huang, Y., and Wang, F., "FIA Method for LBO Limit Predictions of Aero-engine Combustors Based on FV Model", Aerospace Science Technology,Vol. 28, pp. 435–446, (2013).

 

[10] Zheng, H., and Zhang, H., "Feature-parameter-criterion for Predicting Lean Blow out Limit of Gas Turbine Combustor and Bluff Body Burner", Mathematical Problems in Engineering, Hindawi Publishing , Vol. 2013, pp. 1-17, (2013).

 

[11] Ateshkadi, A., McDonell, V., and Samuelsen, G., "Lean Blowout Model for a Spray-fired Swirl-stabilized Combustor", Proceedings of the Combustion Institute,  Vol. 28, pp. 1281-1288, (2000).

 

 [12] Xie, F., Huang, Y., Bin, H., and Wang, F., "Investigation of the Relation between Flame Volume and LBO Limits for a Swirl-stabilized Combustor", IEEE Publication, pp. 2049-2053, (2011).

 

[13] Bin, H., Huang, Y., and Fang, W., "Improved Semiempirical Correlation to Predict Lean Blowout Limits for Gas Turbine Combustors", Journal of Propulsion and Power, pp.197-203, (2011).

 

[14] Davoudzadeh, F., and Liu, F., "Investigation of Swirling Air Flows Generated by Axial Swirlers in a Flame Tube", Asme Turbo Expo. Power for Land, Sea and Air, Barcelona. Spain. 8-11May, (2006).

 

[15] Anderson, J., "Computational Fluid Dynamics the Basic with Applications", Michigan State University, McGraw-Hill Inc, (1995).

 

[16] صنیعی­نژاد.، م.، " اصول جریان­های توربولانسی و مدل­سازی آنها"، انتشارات دانش­نگار، تهران، )1388(.

 

[17] Wilcox, D., "Turbulence Modeling for CFD", Third Edition, Dcw Industries, Incorporated, (2008).

 

[18] "Ansys Fluent User’s Guide", Ansys Inc, (2016).

 

[19] Dodds, W., and Bahr, D., "Combustion System Design in A. M. Mellor, Design of Modern Gas Turbine Combustors", pp. 343–476, Academic Press, San Diego, CA, (1990).

 

[20] Zabetakis, M., "Flammability Characteristics of Combustible Gases and Vapors", U. S. Department of Interior, U. S. Government Printing Office, Washington D. C, Bulletin 62, (1965).

 

[21] "Flammability Characteristics of Combustible Gases and Vapors", ISA Standard, ISA–TR12.13.01–1999 (R200X), Draft Technical Report, (1999).

Keywords

Subjects


[1] Bin, H., Huang, Y., Wang, F., and Xie, F., "Numerical Simulation of Cold Flow Field of Aero-engine Combustors for Lean Blow Off Analysis", ASME Turbo Expo. Power for Land, Sea and Air, GT 45467, Vancouver, British Columbia, Canada, (2011).
 
[2] Rankin, D., "Lean Combustion Technology and Control", Second Edition, USA, California, Elsevier, (2016).
 
[3] Bin, H., Huang, Y., and Jianzhong, X., "A Hybrid Semi-empirical Model for Lean Blow-Out Limit Predictions of Aero-engine Combustors", Journal of Engineering for Gas Turbines and Power, Vol. 137, pp. 501-510, (2015).
 
[4] Zukowski, E., and Marbel, F., "The Role of Wake Transition in the Process of Flame Stabilization on Bluff Bodies", AGARD Combustion,Vol. 28, pp. 167–80, (1955).
 
[5] Mellor, A., "Design of Modern Turbine Combustors", Academic Press, San Diego, CA, (1990).
 
[6] Longwell, J., Frost, E., and Weiss, M., "Flame Stability in Bluff Body Recirculation Zones", Ind. Eng. Chem, Vol. 45, pp. 1629–1633, (1953).
 
[7] Bin, H., Huang, Y., and Wang, F., "CFD Predictions of LBO Limits for Aero-engine Combustors using Fuel Iterative Approximation", Chin. J. Aeronaut,Vol. 26, pp. 74–84, (2012).
 
[8] Lefebvre, A., "Gas Turbine Combustion", Fourth Edition, Printed by CRC Press Taylor and Francis Group, (2016).
 
[9] Bin, H., Huang, Y., and Wang, F., "FIA Method for LBO Limit Predictions of Aero-engine Combustors Based on FV Model", Aerospace Science Technology,Vol. 28, pp. 435–446, (2013).
 
[10] Zheng, H., and Zhang, H., "Feature-parameter-criterion for Predicting Lean Blow out Limit of Gas Turbine Combustor and Bluff Body Burner", Mathematical Problems in Engineering, Hindawi Publishing , Vol. 2013, pp. 1-17, (2013).
 
[11] Ateshkadi, A., McDonell, V., and Samuelsen, G., "Lean Blowout Model for a Spray-fired Swirl-stabilized Combustor", Proceedings of the Combustion Institute,  Vol. 28, pp. 1281-1288, (2000).
 
 [12] Xie, F., Huang, Y., Bin, H., and Wang, F., "Investigation of the Relation between Flame Volume and LBO Limits for a Swirl-stabilized Combustor", IEEE Publication, pp. 2049-2053, (2011).
 
[13] Bin, H., Huang, Y., and Fang, W., "Improved Semiempirical Correlation to Predict Lean Blowout Limits for Gas Turbine Combustors", Journal of Propulsion and Power, pp.197-203, (2011).
 
[14] Davoudzadeh, F., and Liu, F., "Investigation of Swirling Air Flows Generated by Axial Swirlers in a Flame Tube", Asme Turbo Expo. Power for Land, Sea and Air, Barcelona. Spain. 8-11May, (2006).
 
[15] Anderson, J., "Computational Fluid Dynamics the Basic with Applications", Michigan State University, McGraw-Hill Inc, (1995).
 
[16] صنیعی­نژاد.، م.، " اصول جریان­های توربولانسی و مدل­سازی آنها"، انتشارات دانش­نگار، تهران، )1388(.
 
[17] Wilcox, D., "Turbulence Modeling for CFD", Third Edition, Dcw Industries, Incorporated, (2008).
 
[18] "Ansys Fluent User’s Guide", Ansys Inc, (2016).
 
[19] Dodds, W., and Bahr, D., "Combustion System Design in A. M. Mellor, Design of Modern Gas Turbine Combustors", pp. 343–476, Academic Press, San Diego, CA, (1990).
 
[20] Zabetakis, M., "Flammability Characteristics of Combustible Gases and Vapors", U. S. Department of Interior, U. S. Government Printing Office, Washington D. C, Bulletin 62, (1965).
 
[21] "Flammability Characteristics of Combustible Gases and Vapors", ISA Standard, ISA–TR12.13.01–1999 (R200X), Draft Technical Report, (1999).
Volume 18, Issue 4 - Serial Number 45
Fluid Mechanics and Heat Transfer
Winter 2017
Pages 55-71

  • Receive Date 05 March 2016
  • Accept Date 01 November 2016