Math Design of the Airborne Evaporation Circulatory System
Authors
Yinsai Guo, Yi Zhang, Mengyi Zhang, Xiangfu Zeng
Corresponding Author
Yinsai Guo
Available Online June 2015.
- DOI
- 10.2991/meici-15.2015.140How to use a DOI?
- Keywords
- Math Design; Thermodynamic Calculation; Compressor; Condenser; Evaporator; Expansion Valve.
- Abstract
The researches on a vapor cycle system start late in China. The vapor cycle cooling system is not a mature technolog . With the aid of advanced refrigeration technology at home and abroad, this paper focuses on research and development of the vapor cycle cooling system of the helicopter. Based on the design parameters of the vapor cycle cooling system, this paper carries out the match design, determines the operation condition and thermodynamic cycle pressure-enthalpy chart, conducts thermodynamic calculation, and obtains the main performance parameters and the required refrigerating capacity, which provides a basis for the match design in the actual system.
- Copyright
- © 2015, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Yinsai Guo AU - Yi Zhang AU - Mengyi Zhang AU - Xiangfu Zeng PY - 2015/06 DA - 2015/06 TI - Math Design of the Airborne Evaporation Circulatory System BT - Proceedings of the 2015 International Conference on Management, Education, Information and Control PB - Atlantis Press SP - 797 EP - 800 SN - 1951-6851 UR - https://doi.org/10.2991/meici-15.2015.140 DO - 10.2991/meici-15.2015.140 ID - Guo2015/06 ER -