Fluid Mechanics & Aerodynamics

Fluid Mechanics & Aerodynamics

Numerical Investigation of The Effect of Spraying Vapor in Combustion Chamber of Turbine Engine on Engine Performance

Document Type : Original Article

Authors
1 Master's degree, Imam Hussein (AS) University, Tehran, Iran
2 Professor, Imam Hussein (AS) University, Tehran, Iran
Abstract
Turbine engines are one of the vital components in the transportation sector. Due to their widespread usage, there have been continuous strides to enhance the power and thrust of the turbine engines and also the overall cycle efficiency using various techniques. One of those techniques is the introduction of steam into the combustion chamber. The addition of steam enhances the mass flow rate of the working fluid, hence increasing the power and thrust of the engine. This would, additionally, reduce the outlet temperature from the combustion chamber and extend the turbine life while reducing the emissions; besides, as mentioned above, the steam generation from exhaust gases of the engine increases the overall cycle efficiency. The investigations are presented over LF502 engine in this study on injecting steam into a combustion chamber. The type of research that has been carried out is dealing with various flow rates and pressures besides fuel to air ratios. Calculations with STAR-CCM+ are carried out, then with a MATLAB code, the analysis for a suitable gas cycle of the engine and engine power and thrust calculation was found, at the same time, producible steam from exhaust gases estimation is done. The tests demonstrated that the injection of steam, solely derived from exhaust gases for the generation of steam without any additional fuel, resulted in power up to a maximum increase of 17%. Moreover, when added the required supplementary fuel to generate steam, three times the power increase and an increase in thrust by two-thirds were achievable.
Keywords

Smiley face

[1]    “Turbojet Enhancements | Glenn Research Center | NASA.” https://www1.grc.nasa.gov/historic-facilities/special-projects-laboratory/turbojet-enhancements/ (accessed Jan. 26, 2020).
[2]    H. W. Jones, William L.;Dowman, “Investigation of thrust augmentation of a 1600-pound thrust centrifugal-flow-type turbojet engine by injection of refrigerants at compressor inlets,” 1947. [Online]. Available: https://ntrs.nasa.gov/search.jsp?R=19930085811
[3]    H. W. Jones, William L.;Engelman, “Experimental investigation of thrust augmentation of 4000-pound-thrust centrifugal-floe-type turbojet engine by injection of water and alcohol at compressor inlets,” 1948. [Online]. Available: https://ntrs.nasa.gov/search.jsp?R=19930085748
[4]    E. C. Wilcox, “Analysis of water-injection methods of thrust augmentation,” 1948. [Online]. Available: https://ntrs.nasa.gov/search.jsp?R=19740075147
[5]    B. T. Lundin, “Experimental investigation of thrust augmentation by water-alcohol injection,” 1948. [Online]. Available: https://ntrs.nasa.gov/search.jsp?R=19740075147
[6]    W. C. Baron, Burnett; Dowman, Harry W.;Dackis, “Experimental investigation of thrust augmentation of axial-flow-type 4000-pound-thrust turbojet engine by water and alcohol injection at compressor inlet,” 1948. [Online]. Available: https://ntrs.nasa.gov/search.jsp?R=19930085789
[7]    J. H. Useller, James W.;Povolny, “Experimental investigation of turbojet-engine thrust augmentation by combined compressor coolant injection anf tail-pipe burning,” 1951. [Online]. Available: https://ntrs.nasa.gov/search.jsp?R=19930086891
[8]    W. E. Boman, David S.;Mallett, “Investigation of thrust augmentation using water-alcohol injection on a 5200-pound-thrust axial-flow-type turbojet engine at static sea-level conditions,” 1952. [Online]. Available: https://ntrs.nasa.gov/search.jsp?R=19930090414
[9]    L. Fan, S. L. Yang, and K. P. Kundu, “Evaluation of water injection effect on NOx formation for a staged gas turbine combustor,” in 34th Aerospace Sciences Meeting and Exhibit, 1996. doi: 10.2514/6.1996-706.
[10]  M. Cârdu and M. Baica, “Gas turbine installation with total water injection in the combustion chamber,” Energy Convers. Manag., vol. 43, no. 17, pp. 2395–2404, Nov. 2002, doi: 10.1016/S0196-8904(01)00175-3.
[11]  D. L. Daggett, S. Ortanderl, D. Eames, C. Snyder, and J. Berton, “Water injection: Disruptive technology1 to reduce airplane emissions and maintenance costs,” in SAE Technical Papers, 2004, vol. 113, pp. 1547–1556. doi: 10.4271/2004-01-3108.
[12]  D. L. Daggett, “Water misting and injection of commercial aircraft engines to reduce airport NOx,” Natl. Aeronaut. Sp. Adm. Glenn …, no. x, 2004, Accessed: Jan. 28, 2020. [Online]. Available: https://ntrs.nasa.gov/search.jsp?R=20040035576
[13]  D. Daggett, “Water Injection Feasibility for Boeing 747 Aircraft,” Nasa Cr-2005-213656, no. December, Dec. 2005, Accessed: Jan. 28, 2020. [Online]. Available: http://gltrs.grc.nasa.gov/reports/2005/CR-2005-213656.pdf
[14]  A. Brankovic, R. C. Ryder, R. C. Hendricks, N. S. Liu, D. T. Shouse, and W. M. Roquemore, “Emissions prediction and measurement for liquid fueled TVC combustor with and without water injection,” in 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers, 2005, pp. 6117–6128. doi: 10.2514/6.2005-215.
[15]  A. Farokhipour, E. Hamidpour, and E. Amani, “A numerical study of NOx reduction by water spray injection in gas turbine combustion chambers,” Fuel, vol. 212, pp. 173–186, Jan. 2018, doi: 10.1016/j.fuel.2017.10.033.
[16]  E. Amani, M. R. Akbari, and S. Shahpouri, “Multi-objective CFD optimizations of water spray injection in gas-turbine combustors,” Fuel, vol. 227, pp. 267–278, Sep. 2018, doi: 10.1016/j.fuel.2018.04.093.
[17]  D. A. Block Novelo, U. Igie, V. Prakash, and A. SzymaƄski, “Experimental investigation of gas turbine compressor water injection for NOx emission reductions,” Energy, vol. 176, pp. 235–248, Jun. 2019, doi: 10.1016/j.energy.2019.03.187.
[18]  H. Wang et al., “A physics-based approach to modeling real-fuel combustion chemistry - I. Evidence from experiments, and thermodynamic, chemical kinetic and statistical considerations,” Combust. Flame, vol. 193, pp. 502–519, Jul. 2018, doi: 10.1016/J.COMBUSTFLAME.2018.03.019.
[19]  H. F. Trembley, “Determination of Effects on Ambient Conditions on Aircraft Engine Emissions. ALF 502 Combustor Rig and Engine Verification Test. | National Technical Reports Library - NTIS,” 1977. Accessed: Apr. 18, 2022. [Online]. Available: https://nepis.epa.gov/Exe/ZyNET.exe/94002MVY.TXT?ZyActionD=ZyDocument&Client=EPA&Index=1976+Thru+1980&Docs=&Query=&Time=&EndTime=&SearchMethod=1&TocRestrict=n&Toc=&TocEntry=&QField=&QFieldYear=&QFieldMonth=&QFieldDay=&IntQFieldOp=0&ExtQFieldOp=0&XmlQuery=
[20]  C. Borgnakke, R. E. Sonntag, and G. J. Wylen, Fundamentals of Thermodynamics-6e. Wiley, 2002.