Studying an air cooling unit with the two-stage expansion for the passenger aircraft electrical air conditioning system
Authors: Grishina L.A., Panevin A.Yu. | Published: 14.01.2025 |
Published in issue: #1(778)/2025 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
Keywords: air conditioning system, air cooling unit, electric-driven autonomous compressor, turbo-refrigerator turbine, two-stage expansion |
Increasing energy efficiency in the aviation air conditioning systems appears to be one of the main problems to be solved in their design. In the electric air conditioning systems, reducing the energy costs to ensure the system operation is achieved not only by using an electric-driven autonomous compressor, but also by selecting the rational air cooling subsystem that takes air out of it. An air cooling unit with the two-stage expansion for the passenger aircraft electric air conditioning system was developed using a mathematical model. The paper studies the influence of heat exchangers efficiency, power generated by the turbo-refrigerator turbine stages, and the air flow through the bypass dampers on the outlet air temperature from the cooling unit.
EDN: EJYQVH, https://elibrary/ejyqvh
References
[1] Panevin A.Yu. [Analysis and computational evaluation of the application of an electric-driven autonomous compressor for the air conditioning system in the concept of a more electric medium-haul passenger aircraft]. XLIX Gagarinskie chteniya [XLIX Gagarin Readings]. Moscow, Pero, 2023, pp. 47–48. (In Russ.).
[2] Jennions I., Ali F., Miguez M.E. et al. Simulation of an aircraft environmental control system. Appl. Therm. Eng., 2020, vol. 172, art. 114925, doi: https://doi.org/10.1016/j.applthermaleng.2020.114925
[3] Xiong P. Aircraft environmental control systems modeling for configuration selection. Master’s thesis. Cranfield University, 2013. 136 p.
[4] Perez L.D. Modeling and simulation of an aircraft environmental control system. Master’s thesis. ?cole Polytechnique de Montr?al, 2016. 144 p.
[5] Dyachenko Yu.V., Gorbachev M.V., Pashchenko N.I. Termodinamika tsiklov aviatsionnykh sistem konditsionirovaniya vozdukha [Thermodynamics of cycles of aviation air conditioning systems]. Novosibirsk, Izd-vo NGTU Publ., 2011. 240 p. (In Russ.).
[6] Kalliopin A.K., Savelyev R.S., Smagin D.I. Main trends in designing air conditioning systems for future-technology vehicles. Inzhenernyy zhurnal: nauka i innovatsii [Engineering Journal: Science and Innovation], 2017, no. 6, doi: http://dx.doi.org/10.18698/2308-6033-2017-6-1627 (in Russ.).
[7] Smagin D.I., Starostin K.I., Savelyev R.S. et al. Analysis of competing variants of air conditioning systems without air extraction from engines at the stage of passenger aircraft onboard systems conceptual design. Computational nanotechnology, 2019, vol. 6, no. 3, pp. 86–91, doi: https://doi.org/10.33693/2313-223X-2019-6-3-86-91 (in Russ.).
[8] Smagin D.I., Starostin K.I., Savelyev R.S. et al. Method for determining the design parameters of a centrifugal air compressor based on a mathematical model of a non-selective air conditioning system. Sovremennaya nauka: aktualnye problemy teorii i praktiki. Ser. Estestvennye i tekhnicheskie nauki [Modern Science: Actual Problems of Theory and Practice. Ser. Natural and Technical Sciences], 2020, no. 10, pp. 115–121, doi: https://doi.org/10.37882/2223-2966.2020.10.28 (in Russ.).
[9] Grishina L.A., Panevin A.Yu. [Selection of rational structural scheme of air cooling and formation of required selection parameters of electrified air conditioning system]. Sb. tez. rabot 22-y Mezhd. konf. Aviatsiya i kosmonavtika [Abs. 22nd Int. Conf. Aviation and Cosmonautics]. Moscow, Pero Publ., 2023, pp. 41–42. (In Russ.).
[10] Shustrov Yu.M. Proektirovanie aviatsionnykh sistem konditsionirovaniya vozdukha [Design of aviation air conditioning systems]. Moscow, Mashinostroenie Publ., 2006. 382 p. (In Russ.).
[11] Starostin K.I. Optimal choice of the high pressure water separation structure and parameters. Trudy MAI, 2013, no. 67. URL: https://trudymai.ru/published.php?ID=41577 (in Russ.).
[12] Starostin K.I., Shustrov Yu.M. Research on functioning of high-pressure water separation loop scheme during humid air processing. Vestnik MAI [Aerospace MAI Journal], 2013, vol. 20, no. 1, pp. 7–15. (In Russ.).
[13] Starostin K.I. Mathematical modelling of aviation air conditioning systems with consideration of humidity. Vestnik MAI [Aerospace MAI Journal], 2009, vol. 16, no. 2, pp. 141–145. (In Russ.).
[14] Alvarenga M., Andrade C., Zaparoli E. A thermodynamic analysis of three and four-wheel air cycle machines for aeronautical applications. IREME, 2015, vol. 9, no. 2, pp. 190–200, doi: https://doi.org/10.15866/ireme.v9i2.5543
[15] Dyachenko Yu.V., Pashchenko N.I. Estimation of thermodynamic efficiency of an aviation central air of air. Nauchnyy vestnik NGTU [Science Bulletin of the Novosibirsk State Technical University], 2010, no. 1, pp. 185–190. (In Russ.).