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Introduction of JET ENGINE and type of jet engine.

Nikhil Advani

Abstract


The conventional jet engine is optimized to produce high thrust and low specific fuel
consumption. The changes are made in compressor which is responsible for the pressure raise in the total process. The compressor section is replaced with two smaller compressors which are parallel to each other with separate individual inlets. It is designed that the two compressors do compression separately and produce high pressure raise. This pressure raise will reduce the fuel demand considerably and increase in thrust.

Keywords: High thrust jet engine, low fuel consuming jet engine, double compressor jet engine


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References


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Dr. P. Pilidis Variable cycle propulsion systems for a supersonic civil transport, Ph.D.

thesis, Cranfield university, 1997.

H. G. Munzberg and J. Kurzke, The Pros and Cons of Variable Geometry Turbines- A

GARD-CP-205.

Liu Zhigang etc. Design and analysis of HP-turbine for variable cycle engine. ASME GT

-22449, 2010.

YIN Zhao et al Research of design method of variable area nozzle turbine for variable

cycle engine ASME GT 2011- 45166, 2011.

Nicallas Falck, Axial Flow Compressor Mean Line Design, Master thesis, Lund

University, Sweden, Feb.2008.

Saravanamutto, Rogers, Cohen. H, Gas Turbine Theory fifth Edition, Pearson Prentice

Hall, 2001.

Fang Changde. Variable Cycle Engines [J], Gas Turbine Experiment and Research. 2008,

(3):1-6.

Ronald H. Aungier, "Axial Flow Compressor", 2nd edition, 2003.

UIUC Airfoil Coordinates Database Source

datfile,http://airfoiltools.com/airfoil/details?airfoil=nac a65410-il

Dr. P. Pilidis Variable cycle propulsion systems for a supersonic civil transport, Ph.D.

thesis, Cranfield university, 1997.

H. G. Munzberg and J. Kurzke, The Pros and Cons of Variable Geometry Turbines- A

GARD-CP-205.

Liu Zhigang etc. Design and analysis of HP-turbine for variable cycle engine. ASME GT

-22449, 2010.

YIN Zhao et al Research of design method of variable area nozzle turbine for variable

cycle engine ASME GT 2011- 45166, 2011.

Nicallas Falck, Axial Flow Compressor Mean Line Design, Master thesis, Lund

University, Sweden, Feb.2008.

Saravanamutto, Rogers, Cohen. H, Gas Turbine Theory fifth Edition, Pearson Prentice

Hall, 2001.

Fang Changde. Variable Cycle Engines [J], Gas Turbine Experiment and Research. 2008,

(3):1-6.

Ronald H. Aungier, "Axial Flow Compressor", 2nd edition, 2003.

UIUC Airfoil Coordinates Database Source

datfile,http://airfoiltools.com/airfoil/details?airfoil=nac a65410-il




DOI: https://doi.org/10.37591/.v10i2.998

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