Use of a high-efficiency bimetallic recuperator of micro gas turbine units with the power of under 100 kW

Cover Page


Cite item

Full Text

Open Access Open Access
Restricted Access Access granted
Restricted Access Subscription or Fee Access

Abstract

BACKGROUND: Modern micro gas turbine units (MGTUs) with the power of dozen of kilowatts are single-shaft and recuperative. Being in the position where improvement of new MGTU cycles is being studied, it is necessary to choose optimal parameters of the MGTU cycle according to the scheme with regeneration when developing such simple units with the aim of ensuring small size and efficiency. Nevertheless, there are several practical restrictions for the development of recuperators, related to the issue of complicated designs together with pressure losses increase caused by regeneration degree increase and to the restriction of materials quality.

AIMS: Study of influence of a recuperator on efficiency of the MGTU, as it is essential for the development of MGTUs.

METHODS: As a part of the study, the overall assessment of the influence of recuperators on parameters of an ordinary Brayton cycle with recuperation is presented in the article. The influence of main parameters, including degree of pressure increase in a compressor, inlet gas temperature and regeneration degree, on MGTU efficiency is considered in depth in the article.

RESULTS: According to the study results, it is revealed that the use of the regeneration degree of over 0,9 with low coefficient of pressure losses in recuperators for the development of modern recuperative MGTUs leads to the unit effective efficiency not exceeding 38…40% because of certain restrictions of gas temperature at the MGTU turbine inlet caused by difficulties with cooling and ensuring small size and efficiency of the unit.

CONCLUSIONS: Use of new heatproof materials is to become an important part of improvement of MGTU in future, therefore it is necessary to study new technical solution when using prospective materials of recuperators for choosing optimal parameters of the MGTU cycle with regeneration. In addition, the option of using bimetallic recuperators is considered.

Full Text

Restricted Access

About the authors

V.Ch. Chu

Peter the Great St. Petersburg Polytechnic University

Author for correspondence.
Email: turbotechvn95@gmail.com
ORCID iD: 0000-0001-7029-409X
SPIN-code: 8214-5919

Postgraduate of the Institute of Energy

Russian Federation, Saint Petersburg

Viktor A. Rassokhin

Peter the Great St. Petersburg Polytechnic University

Email: v-rassokhin@yandex.ru
ORCID iD: 0000-0003-4609-4252
SPIN-code: 3815-2975

Dr. Sci. (Tech.), Professor of the Institute of Energy

Russian Federation, Saint Petersburg

Viktor V. Barskov

Peter the Great St. Petersburg Polytechnic University

Email: viktorbarskov@mail.ru
ORCID iD: 0000-0001-6914-8212
SPIN-code: 3312-9427
Scopus Author ID: 57220246932

Cand. Sci. (Tech), Associate Professor of the Institute of Energy

Russian Federation, Saint Petersburg

Yury V. Matveev

Peter the Great St. Petersburg Polytechnic University

Email: matyury@mail.ru
ORCID iD: 0000-0003-3947-2630
SPIN-code: 9918-1199

Cand. Sci. (Tech), Associate Professor of the Institute of Energy

Russian Federation, Saint Petersburg

Mikhail A. Laptev

Peter the Great St. Petersburg Polytechnic University

Email: mikhail.laptev@outlook.com
ORCID iD: 0000-0001-6045-3288
SPIN-code: 2315-1330

Postgraduate of the Institute of Energy

Russian Federation, Saint Petersburg

Mehdi Basati Panah

Peter the Great St. Petersburg Polytechnic University

Email: mehdibp.energy@gmail.com
ORCID iD: 0000-0001-5566-8508
SPIN-code: 6388-8007

Postgraduate of the Institute of Energy

Russian Federation, Saint Petersburg

References

  1. do Nascimento MAR, de Oliveira Rodrigues L, dos Santos EC, et al. Micro gas turbine engine: A review. In: Benini E. Editor. Progress in Gas Turbine Performance. Rijeka: IntechOpen; 2013:107–141. doi: 10.5772/54444
  2. Besedin SN. Metodologiya sozdaniya i prakticheskaya realizatsiya mikroturbinnykh ustanovok [dissertation] Saint-Petersburg; 2021. (in Russ). [cited: Apr 04 2022] Available from: http://www.spbstu.ru/dsb/07dc-thesis.pdf
  3. Xiao G, Yang T, Liu H, et al. Recuperators for micro gas turbines: A review. Applied Energy. 2017;197:83–99. doi: 10.1016/j.apenergy.2017.03.095
  4. Kostukov AV, Kosach LA, Gornovskii AS. Microturbinewith heat exchanger with regeneration ratio equal 95%. In: Proceedings of the 4th International Conference on Industrial Engineering. Cham: Springer; 2019:2229–2235. doi: 10.1007/978-3-319-95630-5_240
  5. Arseniev LV, Rassokhin VA, Olennikov SYu, et al. Calculation of the thermal scheme of gas turbines. Tutorial. Saint Petersburg: LGTU; 1992.
  6. Barskov VV, Besedin SN, Zabelin NA, et al. Calculation of the thermal scheme of a gas turbine plant: a tutorial. Saint Petersburg: Izd-vo Politekhn. un-ta; 2018.
  7. Rassokhin VA, Homenok LA, Mikhailov VB, et al. Turbine installations. Vol. IV-19. Engineering. Encyclopedia. Editors Frolov KV, et al. Moscow: Mashinostroenie; 2015.
  8. Aronson KE, Brezgin VI, Brodov YuM. Heat exchangers for technological subsystems of turbine installations. Vol. IV-10. Engineering. Encyclopedia. Editors Frolov KV, et al. Moscow: Innovatsionnoe Mashinostroenie; 2016.
  9. Barskov VV. The choice of optimal solutions in the design of gas turbine plants of low power. Globalnaya energiya. 2013;4–1(183):244–249. [cited: Apr 04 2022] Available from: https://engtech.spbstu.ru/userfiles/files/articles/2013/4/30_barskov.pdf
  10. Aronson KE, Blinkov SN, Brezgini VI, et al. Heat exchangers of power plants: tutorial. Ekaterinburg: UrFU; 2015. [cited: Mar 02 2022] Available from: https://openedu.urfu.ru/files/book/
  11. Arseniev LV, Tyryshkin VG, Bogov IA, et al. Stationary gas turbine installations: a reference book. Liningrad: Mashinostroenie; 1989.
  12. Aquaro D, Pieve M. High temperature compact heat exchangers: performance of advanced metallic recuperators for power plants. In: Proc. of fifth international conference on enhanced, compact and ultra-compact heat exchangers: science, engineering and technology. September 2005. Hoboken, USA. Hoboken: Engineering Conferences International. [cited: Feb 25 2022] Available from: https://core.ac.uk/download/pdf/185670699.pdf

Supplementary files

Supplementary Files
Action
1. JATS XML
2. Fig 1. The scheme of MGTU with regeneration and its real operating cycle: a) thermal scheme; b) real cycle in the form of T-s diagram of MGTU with regeneration; K — a compressor; T — a turbine; KC — combustion chamber; ВхУ — an inlet; ВыхУ — an outlet; H-1, 4-H’ are isothermal processes of working body flow in the inlet and in the outlet; 1–2t, 3–4t are isoentropic processes of compression in the compressor and expansion in the turbine; 1–2, 3–4 are real processes of compression in the compressor and expansion in the turbine; 2–3 is the process of heat supply in the combustion chamber; H–H’ is an isobaric process of heat dissipation; 2t–5, 2–5 and 4t–6, 4–6 are processes of heat supply to air and heat dissipation by gas in the recuperator.

Download (177KB)
3. Fig. 2. The block diagram to calculation of the influence of a recuperator on the choice of the MGTU cycle optimal parameters.

Download (247KB)
4. Fig. 3. The influence of regeneration degree on MGTU efficiency with various cycle parameters ().

Download (316KB)
5. Fig. 4. The dependence of net capacity to fuel consumption ratio (He*GГ)/GТОП of the MGTU on compression ratio πк* of the compressor with various values of regeneration degree μ .

Download (133KB)
6. Fig. 5. Dependence of effective efficiency of the MGTU in the real cycle with regeneration on coefficient of pressure losses in the recuperator with various values of regeneration degree ().

Download (107KB)
7. Fig. 6. Influence of working body parameters on the MGTU indicators with various parameters of a cycle with regeneration ().

Download (84KB)
8. Fig. 7. Dependence of net capacity to fuel consumption ratio (He*GГ)/GТОП of the MGTU on inlet gas temperature Т3* with various values of regeneration degree μ ().

Download (156KB)
9. Fig. 8. Dependence of optimization of recuperative MGTU cycle parameters on materials of turbines and recuperators for common range of T3* and degree of pressure increase πк* in the compressor ().

Download (399KB)
10. Fig. 9. Use of bi-metal recuperator in a cycle of the SGTU with power of under 100 kW for improvement of the unit efficiency when inlet gas temperature T3* is increased ().

Download (148KB)

Copyright (c) 2023 Eco-Vector

License URL: https://eco-vector.com/for_authors.php#07

This website uses cookies

You consent to our cookies if you continue to use our website.

About Cookies