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INVERTED BRAYTON CYCLE ENGINE OPTIMIZATION FOR HYPERSONIC FLIGHT

Yıl 2023, Cilt: 24 Sayı: 4 - Eskişehir Technical University Journal of Science and Technology A - Applied Sciences and Engineering, 257 - 274, 27.12.2023

Mustafa Karabacak Onder Turan

https://doi.org/10.18038/estubtda.1270986

Öz

The objectives of this study are to determine the optimum design parameters of a IBCE for hypersonic flight and to investigate the relationship between engine performance and design parameters. The investigation of these objectives is made first in the literature in this study. The optimization of inverted Brayton cycle engine ,IBCE, is performed using the particle swarm optimization method in this study. The optimum specific thrust, sT, value is reached by staying within the optimization constraints. When the total temperature of the cooling section is examined, a temperature above the freezing temperature of the air is obtained. A very high sT value, 451 N.s/kg is obtained at the hypersonic flight Mach Number (5 Mach) as a result of optimization. By the investigation, it is concluded that specific fuel consumption, SFC, reduces % 5.3 and sT increases % 5.6 dependent on preburner exit total temperature, PETT, change from 2100 K to 1400 K. Based on total temperature decrease at cooling section,T_cooling, change from 100 K to 500 K, it is seen that by the investigation, SFC increases %23.7 and sT increases % 13.1. It is seen that SFC reduces by % 6.3 and sT increases by % 35.9 depending on afterburner exit total temperature, AETT, change from 2000 K to 2300 K. It is observed that SFC reduces % 10.5 and sT increases % 11.7 dependent on total pressure ratio of turbine, π_t , change from 0.9 to 0.1.

Anahtar Kelimeler

Jet engine Optimization Hypersonic flight Inverted Brayton cycle Engine performance

Kaynakça

  • [1] Cross N, Cross AC. Expertise in engineering design. Research in engineering design 1998; 10(3): 141-149.
  • [2] Haik Y, Sivaloganathan S, Shahin, TM. Engineering design process. Cengage Learning 2015.
  • [3] Hubka V. Principles of engineering design. Elsevier 2015.
  • [4] Buede DM, Miller WD. The engineering design of systems: models and methods 2016.
  • [5] Cross N. Engineering design methods: strategies for product design. John Wiley & Sons 2021.
  • [6] Bianchi M, Negri di Montenegro G, Peretto A, Spina, PR. A feasibility study of inverted Brayton cycle for gas turbine repowering. J. Eng. Gas Turbines Power 2005; 127(3):599-605.
  • [7] Farokhi S. Aircraft propulsion. John Wiley & Sons 2014.
  • [8] Kurzke J. GasTurb 13: design and off-design performance of gas turbines. Aachen: GasTurb GmbH 2021. [9] Mattingly JD, Heiser WH, Pratt DT. Aircraft engine design. American Institute of Aeronautics and Astronautics 2002. [10] Pennington WA. Choice of engines for aircraft. Shell Aviation News. January 1959; 14–19 .
  • [11] Raymer D. Aircraft design: A conceptual approach. AIAA 1989; 233–236.
  • [12] Kyprianidis KG, Rolt AM, Grönstedt T. Multi-disciplinary analysis of a geared fan intercooled core aero-engine. In Turbo Expo: Power for Land, Sea, and Air, 2013; 55133: V002T07A027.
  • [13] Kyprianidis KG, Rolt AM. On the optimisation of a geared fan intercooled core engine design. In Turbo Expo: Power for Land, Sea, and Air. 2014;45653: V03AT07A018.
  • [14] Sato T, Tanatsugu N, Naruo Y, Omi J, Tomike JI, Nishino T. Development study on ATREX engine. Acta Astronautica 2000; 47(11): 799-808.
  • [15] Webber H, Bond A, Hempsell M. Sensitivity of pre-cooled air-breathing engine performance to heat exchanger design parameters. In 57th International Astronautical Congress, 2006; D2-P.
  • [16] Dong P, Tang H, Chen M. Study on multi-cycle coupling mechanism of hypersonic precooled combined cycle engine. Applied Thermal Engineering 2018; 131: 497-506.
  • [17] Yu X, Wang C, Yu D. Thermodynamic design and optimization of the multi-branch closed Brayton cycle based precooling-compression system for a novel hypersonic aeroengine. Energy Conversion and Management 2020; 205: 112412.
  • [18] Murray JJ, Guha A, Bond A. Overview of the development of heat exchangers for use in air-breathing propulsion pre-coolers. Acta astronautica 1997; 41(11): 723-729.
  • [19] Di Battista D, Fatigati F, Carapellucci R, Cipollone R. Inverted Brayton Cycle for waste heat recovery in reciprocating internal combustion engines. Applied Energy 2019; 253(113565).
  • [20] Kennedy I, Chen Z, Ceen B, Jones S, Copeland CD. Experimental investigation of an inverted Brayton cycle for exhaust gas energy recovery. Journal of Engineering for Gas Turbines and Power 2019; 141(3).
  • [21] Huang W, Du ZB, Yan L, Xia ZX. Supersonic mixing in airbreathing propulsion systems for hypersonic flights. Progress in Aerospace Sciences 2019; 109(100545).
  • [22] Huang W, Pourkashanian M, Ma L, Ingham DB, Luo SB, Wang ZG. Investigation on the flame holding mechanisms in supersonic flows: backward-facing step and cavity flameholder. Journal of Visualization 2011; 14: 63-74.
  • [23] Khan A, Akram S, Kumar R. Experimental study on enhancement of supersonic twin-jet mixing by vortex generators. Aerospace Science and Technology 2020; 96(105521).
  • [24] Verma KA, Pandey KM, Sharma KK. Study of Fuel Injection Systems in Scramjet Engine—A Review. Recent Advances in Mechanical Engineering: Select Proceedings of ICRAME, 2021; 2020: 931-940.
  • [25] Verma KA, Kapayeva S, Pandey KM, Sharma KK. The recent development of supersonic combustion ramjet engines for augmentation of the mixing performance and improvement in combustion Efficiency: A review. Materials Today: Proceedings 2021; 45: 7058-7062.
  • [26] Verma KA, Pandey KM, Ray M, Sharma KK. Effect of transverse fuel injection system on combustion efficiency in scramjet combustor. Energy 2021; 218(119511).
  • [27] Zhang W, Chen L, Sun F, Wu C. Second-law analysis and optimisation for combined Brayton and inverse Brayton cycles. International Journal of Ambient Energy 2007; 28(1): 15-26.
  • [28] Tsujikawa Y, Kaneko KI, Tokumoto S. Inverted Turbo-Jet Engine for Hypersonic Propulsion. In Turbo Expo: Power for Land, Sea and Air, 2005; 47284: 343-349.
  • [29] Kennedy J, Eberhart R. Particle swarm optimization. In Proceedings of ICNN'95-international conference on neural networks IEEE, 1995; 4:1942-1948.
  • [30] Poli R, Kennedy J, Blackwell T. Particle swarm optimization. Swarm intelligence 2007; 1(1): 33-57.
  • [31] Hu X, Eberhart R. Multiobjective optimization using dynamic neighborhood particle swarm optimization. In Proceedings of the 2002 Congress on Evolutionary Computation. CEC'02, 2002; 2: 1677-1681.
  • [32] Hu X. Particle Swarm Optimization. http://www.swarmintelligence.org [Online: accessed 16-May-2016 ]
  • [33] Beltrán-Prieto JC, Komínková Oplatková Z, Torres Friás R, Escoto Hernández JL. A time performance comparison of particle swarm optimization in mobile devices. In MATEC Web of Conferences 20th International Conference on Circuits, Systems, Communications and Computers (CSCC 2016). EDP Sciences, 2016.

INVERTED BRAYTON CYCLE ENGINE OPTIMIZATION FOR HYPERSONIC FLIGHT

Yıl 2023, Cilt: 24 Sayı: 4 - Eskişehir Technical University Journal of Science and Technology A - Applied Sciences and Engineering, 257 - 274, 27.12.2023

Mustafa Karabacak Onder Turan

https://doi.org/10.18038/estubtda.1270986

Öz

Optimization of inverted Brayton cycle engine is made by particle swarm optimization method in this study. The optimum specific thrust value is reached by staying within the optimization constraints. When the total temperature of the cooling section is examined, it is seen that a temperature above the freezing temperature of the air is obtained. A very high specific thrust value, 451 N.s/kg is obtained at the hypersonic flight Mach Number (5 Mach) as a result of optimization. Temperature decrease with increasing altitude effect performance dramatically as positive. Low preburner exit total temperature and turbine total pressure ratio values and high afterburner exit total temperature values are desirable in terms of performance but values of total temperature at cooling section effect performance conversely in terms of specific thrust and specific fuel consumption

Anahtar Kelimeler

Jet engine Optimization Hypersonic flight Inverted Brayton cycle Engine performance

Kaynakça

  • [1] Cross N, Cross AC. Expertise in engineering design. Research in engineering design 1998; 10(3): 141-149.
  • [2] Haik Y, Sivaloganathan S, Shahin, TM. Engineering design process. Cengage Learning 2015.
  • [3] Hubka V. Principles of engineering design. Elsevier 2015.
  • [4] Buede DM, Miller WD. The engineering design of systems: models and methods 2016.
  • [5] Cross N. Engineering design methods: strategies for product design. John Wiley & Sons 2021.
  • [6] Bianchi M, Negri di Montenegro G, Peretto A, Spina, PR. A feasibility study of inverted Brayton cycle for gas turbine repowering. J. Eng. Gas Turbines Power 2005; 127(3):599-605.
  • [7] Farokhi S. Aircraft propulsion. John Wiley & Sons 2014.
  • [8] Kurzke J. GasTurb 13: design and off-design performance of gas turbines. Aachen: GasTurb GmbH 2021. [9] Mattingly JD, Heiser WH, Pratt DT. Aircraft engine design. American Institute of Aeronautics and Astronautics 2002. [10] Pennington WA. Choice of engines for aircraft. Shell Aviation News. January 1959; 14–19 .
  • [11] Raymer D. Aircraft design: A conceptual approach. AIAA 1989; 233–236.
  • [12] Kyprianidis KG, Rolt AM, Grönstedt T. Multi-disciplinary analysis of a geared fan intercooled core aero-engine. In Turbo Expo: Power for Land, Sea, and Air, 2013; 55133: V002T07A027.
  • [13] Kyprianidis KG, Rolt AM. On the optimisation of a geared fan intercooled core engine design. In Turbo Expo: Power for Land, Sea, and Air. 2014;45653: V03AT07A018.
  • [14] Sato T, Tanatsugu N, Naruo Y, Omi J, Tomike JI, Nishino T. Development study on ATREX engine. Acta Astronautica 2000; 47(11): 799-808.
  • [15] Webber H, Bond A, Hempsell M. Sensitivity of pre-cooled air-breathing engine performance to heat exchanger design parameters. In 57th International Astronautical Congress, 2006; D2-P.
  • [16] Dong P, Tang H, Chen M. Study on multi-cycle coupling mechanism of hypersonic precooled combined cycle engine. Applied Thermal Engineering 2018; 131: 497-506.
  • [17] Yu X, Wang C, Yu D. Thermodynamic design and optimization of the multi-branch closed Brayton cycle based precooling-compression system for a novel hypersonic aeroengine. Energy Conversion and Management 2020; 205: 112412.
  • [18] Murray JJ, Guha A, Bond A. Overview of the development of heat exchangers for use in air-breathing propulsion pre-coolers. Acta astronautica 1997; 41(11): 723-729.
  • [19] Di Battista D, Fatigati F, Carapellucci R, Cipollone R. Inverted Brayton Cycle for waste heat recovery in reciprocating internal combustion engines. Applied Energy 2019; 253(113565).
  • [20] Kennedy I, Chen Z, Ceen B, Jones S, Copeland CD. Experimental investigation of an inverted Brayton cycle for exhaust gas energy recovery. Journal of Engineering for Gas Turbines and Power 2019; 141(3).
  • [21] Huang W, Du ZB, Yan L, Xia ZX. Supersonic mixing in airbreathing propulsion systems for hypersonic flights. Progress in Aerospace Sciences 2019; 109(100545).
  • [22] Huang W, Pourkashanian M, Ma L, Ingham DB, Luo SB, Wang ZG. Investigation on the flame holding mechanisms in supersonic flows: backward-facing step and cavity flameholder. Journal of Visualization 2011; 14: 63-74.
  • [23] Khan A, Akram S, Kumar R. Experimental study on enhancement of supersonic twin-jet mixing by vortex generators. Aerospace Science and Technology 2020; 96(105521).
  • [24] Verma KA, Pandey KM, Sharma KK. Study of Fuel Injection Systems in Scramjet Engine—A Review. Recent Advances in Mechanical Engineering: Select Proceedings of ICRAME, 2021; 2020: 931-940.
  • [25] Verma KA, Kapayeva S, Pandey KM, Sharma KK. The recent development of supersonic combustion ramjet engines for augmentation of the mixing performance and improvement in combustion Efficiency: A review. Materials Today: Proceedings 2021; 45: 7058-7062.
  • [26] Verma KA, Pandey KM, Ray M, Sharma KK. Effect of transverse fuel injection system on combustion efficiency in scramjet combustor. Energy 2021; 218(119511).
  • [27] Zhang W, Chen L, Sun F, Wu C. Second-law analysis and optimisation for combined Brayton and inverse Brayton cycles. International Journal of Ambient Energy 2007; 28(1): 15-26.
  • [28] Tsujikawa Y, Kaneko KI, Tokumoto S. Inverted Turbo-Jet Engine for Hypersonic Propulsion. In Turbo Expo: Power for Land, Sea and Air, 2005; 47284: 343-349.
  • [29] Kennedy J, Eberhart R. Particle swarm optimization. In Proceedings of ICNN'95-international conference on neural networks IEEE, 1995; 4:1942-1948.
  • [30] Poli R, Kennedy J, Blackwell T. Particle swarm optimization. Swarm intelligence 2007; 1(1): 33-57.
  • [31] Hu X, Eberhart R. Multiobjective optimization using dynamic neighborhood particle swarm optimization. In Proceedings of the 2002 Congress on Evolutionary Computation. CEC'02, 2002; 2: 1677-1681.
  • [32] Hu X. Particle Swarm Optimization. http://www.swarmintelligence.org [Online: accessed 16-May-2016 ]
  • [33] Beltrán-Prieto JC, Komínková Oplatková Z, Torres Friás R, Escoto Hernández JL. A time performance comparison of particle swarm optimization in mobile devices. In MATEC Web of Conferences 20th International Conference on Circuits, Systems, Communications and Computers (CSCC 2016). EDP Sciences, 2016.
Toplam 31 adet kaynakça vardır.

Ayrıntılar

Birincil Dil İngilizce
Konular Mühendislik
Bölüm Makaleler
Yazarlar

Mustafa Karabacak 0000-0002-3301-9862

Onder Turan 0000-0003-0303-4313

Yayımlanma Tarihi 27 Aralık 2023
Yayımlandığı Sayı Yıl 2023 Cilt: 24 Sayı: 4 - Eskişehir Technical University Journal of Science and Technology A - Applied Sciences and Engineering

Kaynak Göster

AMA Karabacak M, Turan O. INVERTED BRAYTON CYCLE ENGINE OPTIMIZATION FOR HYPERSONIC FLIGHT. Eskişehir Technical University Journal of Science and Technology A - Applied Sciences and Engineering. Aralık 2023;24(4):257-274. doi:10.18038/estubtda.1270986