Fatigue Analysis of Axial flow Compressor
Keywords:
Axial Flow Compressor, Steel Alloy, Nickel Alloy, Titanium AlloyAbstract
Axial flow compressors are used in medium to large thrust gas turbine and jet engines. The aerodynamic compressor design process basically consist of mean line prediction is the first step during compressor blade design. In this project design and fatigue analyze of the micro turbine compressor blade is carried with different material and rotational speed for various rotor and stator angles. Based on the given micro turbine output power, the dimensions and physical properties of the compressor blade were calculated. Stainless-steel alloy, Nickel alloy and Titanium alloys, these materials effect on compressor blade are found out by carrying stress and modal analysis.
References
- Design and Optimization of Axial Flow Compressor Koduru. Srinivas Kandula. Deepthi, K.N.D.Malleswara Rao
- Ujjawal A. Jaiswal and Prof. S. J. Joshi “Design and Analysis of Stator, Rotor and Blades of Axial flow Compressor” | ISSN: 2321-9939
- P Lakshmi “Design Modification and FEA Analysis of Axial Flow Compressor” Volume No.5, Issue No.5, August - September 2017, 7160-7165.
- Kiran D Chaudhari, Prof. Dr. N. A. Wankhede “Aerodynamic Design of a single stage Axial Flow Compressor using CFD approach”
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