Exergy Approach to Evaluate Performance of a Mini Class Turboprop Engine

Coban K., ŞÖHRET Y., Sogut M. Z., TURAN Ö., KARAKOÇ T. H.

ENERGY SOLUTIONS TO COMBAT GLOBAL WARMING, cilt.33, ss.465-475, 2017 (SCI-Expanded) identifier identifier identifier

  • Yayın Türü: Makale / Tam Makale
  • Cilt numarası: 33
  • Basım Tarihi: 2017
  • Doi Numarası: 10.1007/978-3-319-26950-4_23
  • Dergi Adı: ENERGY SOLUTIONS TO COMBAT GLOBAL WARMING
  • Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
  • Sayfa Sayıları: ss.465-475
  • Anahtar Kelimeler: Thermodynamics, Energy, Exergy, Second law, Turboprop, Aircraft engine, Gas-turbines, THERMODYNAMICS
  • Anadolu Üniversitesi Adresli: Evet

Özet

In this chapter, performance assessment of a mini class turboprop engine is presented. Exergy analysis is used for this purpose on the basis of applicability on thermal systems. As a result of the component-based exergy analysis, relative irreversibility of the combustion chamber is higher relatively. Exergy destruction rates within the air compressor, combustion chamber and gas turbine components are 24.08 kW, 100.76 kW and 15.80 kW respectively. Additionally, exergy efficiencies of the components are 74.11, 69.68 and 98.99 % in order of air compressor, combustion chamber and gas turbine.