Math Design of the Airborne Evaporation Circulatory System

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/).

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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  -