Try Mobilus Beta
Search tips
 This content is not included in your SAE MOBILUS subscription, or you are not logged in.

Helicopter Turboshaft Engine Database as a Conceptual Design Tool

Journal Article
03-15-01-0003
ISSN: 1946-3936, e-ISSN: 1946-3944
DOI: https://doi.org/10.4271/03-15-01-0003
Published June 14, 2021 by SAE International in United States
Helicopter Turboshaft Engine Database as a Conceptual Design Tool
Citation: Bazmi, F. and Rahimi, A., "Helicopter Turboshaft Engine Database as a Conceptual Design Tool," SAE Int. J. Engines 15(1):31-56, 2022, https://doi.org/10.4271/03-15-01-0003.
Language: English

References

  1. Varga , B. Power Sources of Military Helicopters Academic and Applied Research in Military and Public Management Science (AARMS) 17 2 2018 139 168
  2. Schenderlein J. and Clayton T. Comparison of Helicopter Turboshaft Engines 2015 1 14 https://www.colorado.edu/faculty/kantha/sites/default/files/attached-files/16496-116619_-_tyler_clayton_-_dec_17_2015_110_pm_-_clayton_schenderlein_comparisonofhelicopterengines.pdf
  3. Ali , F. , Goulos , I. , and Pachidis , V. An Integrated Methodology to Assess the Operational and Environmental Performance of a Conceptual Regenerative Helicopter Aeronaut. J. 119 1211 2015 67 90 https://doi.org/10.1017/S0001924000010253
  4. Litalien , C. and Safah , F. 2007
  5. Coban , K. , Colpan , C.O. , and Karakoc , T.H. Application of Thermodynamic Laws on a Military Helicopter Engine Energy 140 2017 1427 1436 https://doi.org/10.1016/j.energy.2017.07.179
  6. Bayona-Roa , C. , Solis-Chaves , J.S. , Bonilla , J. , Rodriguez-Melendez , A.G. et al. Computational Simulation of PT6A Gas Turbine Engine Operating with Different Blends of Biodiesel—A Transient-Response Analysis Energies 12 22 2019 4258 https://doi.org/10.3390/en12224258
  7. Misté , G.A. , Benini , E. , Garavello , A. , and Gonzalez-Alcoy , M. A Methodology for Determining the Optimal Rotational Speed of a Variable RPM Main Rotor/Turboshaft Engine System J. Am. Helicopter Soc. 60 3 2015 1 11 https://doi.org/10.4050/JAHS.60.032009
  8. Alberto , G. and Benini , E. Performance of a Turboshaft Engine for Helicopter Applications Operating at Variable Shaft Speed Proceedings of the ASME 2012 Gas Turbine India Conference 2012 https://doi.org/10.1115/GTINDIA2012-9505 1 15
  9. Garavello , A. and Benini , E. Preliminary Study on a Wide-Speed-Range Helicopter Rotor/Turboshaft System J. Aircr. 49 4 2012 1032 1038 https://doi.org/10.2514/1.C031526
  10. Miste , G.A. and Benini , E. Variable-Speed Rotor Helicopters: Performance Comparison between Continuously Variable and Fixed-Ratio Transmissions J. Aircr. 53 5 2016 1189 1200 https://doi.org/10.2514/1.C032744
  11. Misté , G. 2015
  12. Ostertagová , E. Modelling Using Polynomial Regression Procedia Eng. 48 2012 500 506 https://doi.org/10.1016/j.proeng.2012.09.545
  13. Mattingly , J.D. Elements of Propulsion: Gas Turbines and Rockets 53 9 Reston, VA American Institute of Aeronautics and Astronautics 2006
  14. Mattingly , J.D. , Heiser , W.H. , and Pratt , D.T. Aircraft Engine Design 2nd Reston, VA American Institute of Aeronautics and Astronautics 2002
  15. Bojdo , N. and Filippone , A. Comparative Study of Helicopter Engine Particle Separators J. Aircr. 51 3 2014 1030 1042 https://doi.org/10.2514/1.C032322
  16. Yin , F. and Gangoli Rao , A. Performance Analysis of an Aero Engine with Inter-Stage Turbine Burner Aeronaut. J. 121 1245 2017 1605 1626 https://doi.org/10.1017/aer.2017.93
  17. Mattingly , J. Elements of Gas Turbine Propulsion, Illustrate Michigan McGraw-Hill 1996
  18. MTU 2018 https://www.mtu.de/maintenance/commercial-aircraft-engine-services/engine-portfolio-mro/helicopters/pw200/?pk_vid=62c883896fc430b215803288013992e1 2019
  19. Bose , T. An Introduction Airbreathing Propulsion Aerospace America 45 12 2012 58 59
  20. European Aviation Safety Agency (EASA) 2018
  21. Marcus , M. , Kachalla , I.A. , Chikeluba Uchenna , N. , and Fredrick , O.M. Effects of Components Deterioration on Helicopter Operation in Hostile Environment ATBU, J. Sci. Technol. Educ. 7 2 2019 99 107
  22. EASA 2019
  23. Snyder , C.A. and Tong , M.T. 2019
  24. EASA 2019
  25. EASA 2019
  26. Rolls-Royce 2019
  27. EASA 2015
  28. United Training Corp 2015
  29. Rolls-Royce 2015
  30. Uchida , S. , Nagashima , Y. , and Shimauchi , K. MG5 Series Commercial Helicopter Engine Development and Utilization International Gas Turbine Congress 2003 1 8
  31. T. T. Engine 2003
  32. Rolls-Royce Corporation 2003
  33. Saeed , F. 2004
  34. Bräunling , W.J. Aircraft Engines: Basics, Aero-Thermodynamics, Cycle Processes, Thermal Turbo Machines, Components and Emissions 2nd Berlin Springer-Verlag Berlin 2004
  35. US Army 2004
  36. Data , G. Outlook/Specifications Gas Turbine Engines General Data Aviation Week & Space Technology 2005 122 134
  37. Eames , D.J.H. 2006
  38. Rolls-Royce 2006
  39. US Army 2006
  40. Turbomeca 2006
  41. Richard Chait , D.L. and Lyons , J. 2006
  42. Suhr , S. 2006
  43. U.S. Federal Aviation Administration (FAA) 2007
  44. Kong , C.-D. , Ki , J.-Y. , and Lee , C.-H. A Study on Fault Detection of a Turboshaft Engine Using Neural Network Method KSAS Int. J. 9 1 2008 100 110 https://doi.org/10.5139/ijass.2008.9.1.100
  45. Helicopter Association International 2009
  46. Chang , Y.W. , Hsieh , C.J. , Chang , K.W. , Ringgaard , M. et al. Training and Testing Low-Degree Polynomial Data Mappings via Linear SVM J. Mach. Learn. Res. 11 2010 1471 1490
  47. Snyder , C.A. and Thurman , D.R. 2010
  48. EASA 2010
  49. Zeng , W.S. and Tang , S.Z. Bias Correction in Logarithmic Regression and Comparison with Weighted Regression for Non-Linear Models For. Res. 24 2 2011 137 143 https://doi.org/10.1038/npre.2011.6708.1
  50. Forecast International 2011
  51. Helsinki 2012
  52. Intro , P. and Shepherd , D. 2012
  53. Bazmi , F. Helicopter Turboshaft Engines, One Tehran, IR Chortkeh 2012
  54. Turbomeca 2012
  55. European Aviation Safety Agency 2012
  56. Nkoi , B. , Pilidis , P. , and Nikolaidis , T. Performance Assessment of Simple and Modified Cycle Turboshaft Gas Turbines Propuls. Power Res. 2 2 2013 96 106 https://doi.org/10.1016/j.jppr.2013.04.009
  57. EASA 2013
  58. Warning , R.P.M. Bell 212 Pilot Training Manual Abbotsford, B.C. Campbell Helicopters 2013 1 15
  59. EASA 2014
  60. Cohen , J. , West , S.G. , Aiken , L. , and Cohen , P. Applied Multiple Regression/Correlation Analysis for the Behavioral Sciences New York Taylor & Francis 2014
  61. Power G. 2014
  62. EASA 2014
  63. EASA 2015
  64. Turan , Ö. and Aydin , H. Numerical Calculation of Energy and Exergy Flows of a Turboshaft Engine for Power Generation and Helicopter Applications Energy 115 2016 914 923 https://doi.org/10.1016/j.energy.2016.09.070
  65. Chen , R. , Wen , C.Y. , Lorente , S. , and Bejan , A. The Evolution of Helicopters J. Appl. Phys. 120 1 2016 014901 https://doi.org/10.1063/1.4954976
  66. Engine M. , Jetranger B. , and Searanger B.T. 2016
  67. Adamec , J. 2016
  68. Varga , B. , Óvári , G. , and Kavas , L. The Turbine Inlet Temperature and Compressor Pressure Ratio, the Siamese Twins of the Gas Turbine Engines Sci. Res. Educ. Air Force 18 1 2016 393 398 https://doi.org/10.19062/2247-3173.2016.18.1.53
  69. EASA 2016
  70. Bulanov , M. 2016
  71. EASA 2017
  72. AminiMagham , M. , Ebrahimi , A. , and Zolfaghari , A. 2018
  73. Przybyła , B. , Przysowa , R. , and Zapałowicz , Z. Implementation of a New Inlet Protection System into HEMS Fleet Aircr. Eng. Aerosp. Technol. 92 2018 67 79 https://doi.org/10.14339/STO-MP-AVT-306-08-PDF
  74. Reddy , D.S. , Kumar , K.P. , Manikanta , Y. , Sai , B.P. et al. Analysis of Turboshaft Engine-Low Power Margin Int. J. Innov. Res. Manag. Eng. Technol. 3 3 2018 40 57
  75. EASA 2018
  76. Al , S. 2005
  77. L. Document 1974
  78. Stigler , S.M. Gergonne’s 1815 Paper on the Design and Analysis of Polynomial Regression Experiments Hist. Math. 1 4 1974 431 439 https://doi.org/10.1016/0315-0860(74)90033-0
  79. Stratford , C. Student Training Manual: Gas Turbine Engine T5313 Series T53-L-13 Series Williamsport, PA Lycoming Division 1975
  80. Walter , T.J. 1978
  81. Leissler , G.W. and Yuhas , J.S. 1988
  82. Faragher , J. 1989
  83. CEF 1990
  84. Pratt & Whitney Canada PT6T-3 Training Manual Longueuil, Quebec Pratt & Whitney Canada Corp 1990
  85. Gunston , B. Jane’s Aero-Engines 12th Surrey, UK Janes Information Group 1996
  86. Haynes , S.R. 1997
  87. Silet , J. 1997
  88. 1 2 2000
  89. Turbomeca 2001
  90. Turbomeca 2002

Cited By

Recommended Content

Technical Paper Survey of Past, Present and Planned Human Space Mission Simulators
Technical Paper Fretting Damage Analysis and Predicting of Engine Head and Block
Technical Paper Parameterization of Particles Emitted from a Jet Engine during Stationary Tests