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Tytuł artykułu

Failure analysis (experimental and numerical approach) of gas turbine generator cooling fan in comparison between using 2types (14◦ and 19◦ angle of attack) of blades

Wybrane pełne teksty z tego czasopisma
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
In gas turbine power plants, a fan is used as a cooling system to dissipate generated heat in coils (copper conductors) and generator electric circuits at the end sides of its rotor. In some cases, fracture of blades causes a short circuit between rotor and stator and consequently generator explosion and financial problems. The fracture of cooling fan blades has occurred five times at the turbine side of the generator in our case of study, just 100hr after resuming operations after an overhaul. Using numerical analysis as well as laboratory investigation – including visual inspections, metallography and SEM – can help better find failure problems that cause blade failures. A series of numerical analysis was performed to diagnose the possible cause of failure. CFD analysis is used to study the airflow distribution in order to observe probable separation phenomenon and pressure forces as they are imposed on fan blades due to operation. A finite element method was utilized to determine the stresses and dynamic characteristics of the fan blade (natural frequencies, stresses and vibrations).
Rocznik
Strony
99--117
Opis fizyczny
Bibliogr. 10 poz., rys., tab., wykr.
Twórcy
autor
  • Semnan University, Faculty of Mechanical Engineering Semnan, Iran
  • NRI – Niroo Research Institute P.O. Box 14665/517, Tehran, Iran
  • Power & Water University of Technology P.O. Box 16765-1719, Tehran, Iran
Bibliografia
  • 1. Alsthom Company report in conjunction with some Gas Power Plants (1997).
  • 2. Anderson L., Fracture mechanics fundamental and applications, CRC Press, 9780849316562, Colorado, USA (1995).
  • 3. Barlow K.W., Chandra R., Fatigue crack propagation simulation in an aircraft engine fan blade attachment, Int. J. Fatigue, 27, 1661–1668, 2005.
  • 4. Beisheim J.R., Sinclair G.B., On the three-dimensional finite element analysis of dovetail attachment, [in:] Proceedings of ASME Turbo Expo 2002, Amsterdam, The Netherlands (2002).
  • 5. Failure analysis report of Iran-Montazer-Ghaem units 2, 4 & 6. Iran Power Plant Repair Co, (2003–2004).
  • 6. Hou J., Bryon J.W., Ross A., An investigation of fatigue failures of turbine blades in a gas turbine engine by mechanical analysis, Engineering Failure Analysis, 9, 201–211, 2002.
  • 7. Hutson A., Nicholas T., Johnc R., Fretting fatigue crack analysis in Ti-6Al-4V, Int. J. Fatigue, 27, 1582–1589, 2005.
  • 8. Joseph R., ASM Specialty Handbook, Aluminum and aluminum Alloys, ASM International, 087170496X, USA (1993).
  • 9. Moussavi Torshizi S.E., Yadavar Nikravesh S.M., Jahangiri A., Failure analysis of gas turbine generator cooling fan blades, Engineering Failure Analysis, 16, 1686–1695, 2009.
  • 10. Paris P.C., Gomez M.P., Anderson W.E., A rational analytical theory of fatigue,Trend Eng., 13, 1, 9–14, 1961.
  • 11. Poursaeidi E., Salavatian M., Failure analysis of generator rotor fan blades, Engineering Failure Analysis, 14, 851–860, 2007.
  • 12. Poursaeidi E., Salavatian M., Fatigue crack growth simulation in a generator fan blade, Engineering Failure Analysis, 16, 888–898, 2009.
  • 13. Xi N.S., Zhong P.D., Huang H.Q., Yan H., Tao C.H., Failure investigation of blade and disk in first stage compressor, Eng. Fail Anal., 7, 385–392.
  • 14. http://www.cfg.cornell.edu/software/software.htm.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-25d71df4-2846-4fe5-af5b-421e421fe6d3
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