Strength Assessment of Fan Blade with Different Materials
DOI:
https://doi.org/10.32628/IJSRST196138Keywords:
Thermodynamic, Brayton- Cycle, RB211, JTBD, computational fluid dynamics, PROPFAN, Low Pressure Compressor , High Pressure Compressor , High Pressure Turbine , Low Pressure Turbine , Fibre-Reinforced PolymerAbstract
Weight reduction of turbofan engines is one of the main concerns of aero engine manufacturers in order to cut fuel burn. To achieve higher fuel efficiency, aero engine manufacturers develop turbofans with higher bypass ratio, which can only be achieved with larger (and heavier) fan sections. This makes weight reduction in fan components a major consideration and becomes a key driver for the use of composite materials in future engines. The objective of this project is to design, perform structural analysis and optimization of a Composite fan blade. Development of a fan blade is comparable to a future large aircraft engine fan blade. This thesis is about the structural analysis of a composite fan blade with a honeycomb sandwich construction with a polymer matrix composite and honeycomb Aluminium core compared with baseline solid basic fan blade made of titanium. The focus of this work is to design the sandwich composite blade with honeycomb core and conduct static and dynamic analysis.
References
- Zhenzhen Liu1 , Zhixiong Chen2 , Jin Chen “The Strength Analysis of CFM56 Engine Blade” MATEC Web of Conferences 166, 04001 (2018)
- H. C. TEICHMAN, R. N. TADROS “Analytical & Experimental Simulation of Fan Blade Behaviour & Damage Under Bird Impact” THE AMERICAN SOCIETY OF MECHANICAL ENGINEERS ^y 345 E. 47 St., New York, N.Y. 10017
- Adam Kozakiewicz “Structural ultimate strength analysis of a first stage fan blade in a turbine jet engine RD-33” Volume: 232 issue: 1, page(s): 77-84, October 17, 2016; Issue published: January 1, 2018
- James B Min, Louis J Ghosn and Bradley A Lerch “A study for stainless steel fan blade design with metal foam core” Journal of Sandwich Structures and Materials 2015, Vol. 17(1) 56–73
- RAJEEV JAIN “Foreign Object Damage Analysis of Leading Edge of Fan Rotor Blade” SIMA (B) Department, Gas Turbine Research Establishment, C V Raman Nagar, Post Office Box : 9302, Bangalore 560 093, India (Received 25 February 2013; Accepted 18 April 2013)
- J . I. G o a t h a m “Materials problems in the design of compressor blades with fibrous composites “Proc. Boy. Soc. Lond. A. 319, 45-57 (1970)
- Avinash Gudimetla “Optimum Material Evaluation of Fan Blades Using Reverse Engineering Approach” International Journal of Engineering Science Invention (IJESI) ISSN (Online): 2319 – 6734, ISSN (Print): 2319 – 6726
- Srijith Bangaru “Advanced Material for Front Fan Blade Manufacturing” "Imperial Journal of Interdisciplinary Research (IJIR) 3(5):80 · January 2017 with1,790
- Rula M. Coroneos “Structural Analysis and Optimization of a Composite Fan Blade for Future Aircraft Engine” 2012-09-20 | DOI: https://doi.org/10.1515/tjj-2012-0024
- Binesh Philip “NUMERICAL ESTIMATION OF FATIGUE LIFE OF AEROENGINE FAN BLADES” SASTECH Journal , Volume 9, Issue 2, September 2010
- YangBin “Blade containment evaluation of civil aircraft engines” Aeronautical Science & Technology Research Institute of Commercial Aircraft Corporation of China, Beijing 102211, China
- F. Gálvez “Materials behaviour and numerical simulation of a turbine blade-off containment analysis” Structures Under Shock and Impact IX 433
- N. Sreenivasa Babu “Analysis of Turbine Blade under the Effect of Damping with Different Materials” Journal of Engineering Research and Applications, ISSN : 2248-9622, Vol. 4, Issue 1( Version 3), January 2014, pp.01-05
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