Affiliation:
1. National Academy of Sciences of the Ukraine, 03057 Kyiv, Ukraine
Abstract
This paper proposes a new air cycle system by replacing the turbine assembly with vortex tubes and a parameter-matching method independent of the architecture of the air cycle system. Only, in terms of refrigerating and dehumidification, the performance of the newly proposed vortex system is worse than that of a conventional air cycle system under the same bleed air parameters. However, for aircraft practical applications, the overall performance of air cycle systems requires additional considerations such as the heating capacity, weight of the system, and extra aviation fuel used to transport that weight. Therefore, this paper conducts an integrated performance comparison between the new system and a conventional system based on the overall fuel mass penalty criterion. The results show that whether the new system has a smaller total takeoff mass depends on the bleed air parameters, flight duration, and flight speed. For specific bleed air parameters, there is a specific [Formula: see text] curve where the new system and the turbine system have the same total takeoff mass. The performance of the new system is better than that of the turbine system only when the values of flight Mach number and flight duration are at the lower left of the [Formula: see text] curve.
Funder
Research Fund of Key Laboratory of Aircraft Environment Control and Life Support, Ministry of Industry and Information Technology, Nanjing University of Aeronautics and Astronautics
China Postdoctoral Science Foundation
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Cited by
1 articles.
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1. Functional States Diagnosing in Vortex Energy Separator Under Rational Control;2023 IEEE 7th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC);2023-10-24