Study on heat transfer performance of antifreeze-R134a heat exchanger (ARHEx)

Liping Pang; Kun Luo; Shizhao Yu; Desheng Ma; Miao Zhao; Xiaodong Mao

doi:10.3390/en13226129

Study on heat transfer performance of antifreeze-R134a heat exchanger (ARHEx)

Liping Pang
, Kun Luo
, Shizhao Yu
, Desheng Ma
, Miao Zhao
, Xiaodong Mao^*

^*Corresponding author for this work

School of Aeronautic Science and Engineering

Beihang University
Xinxiang Aviation Industry (Group) Co., Ltd.
Shenyang Aerospace University

Research output: Contribution to journal › Article › peer-review

2 Scopus citations

Abstract

In this paper, the liquid cooling and vapor compression refrigeration system based on an Antifreeze-R134a Heat Exchanger (ARHEx) was applied to the thermal management system for high-power avionics in helicopters. The heat transfer performance of the ARHEx was studied. An experimental prototype of ARHEx was designed and established. A series of experiments was carried out with a ground experimental condition. A heat transfer formula for the antifreeze side in the ARHEx was obtained by means of the coefficient of Nusselt number with experimental analysis. The performance of heat transfer and pressure drop for the refrigerant side of the ARHEx was deduced for the given condition.

Original language	English
Article number	6129
Journal	Energies
Volume	13
Issue number	22
DOIs	https://doi.org/10.3390/en13226129
State	Published - 2 Nov 2020

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

SDG 7 Affordable and Clean Energy

Keywords

Antifreeze-R134a heat exchanger
Avionics
Heat transferperformance
Thermalmanagement

Access to Document

10.3390/en13226129

Cite this

@article{7e1dd18afa614a5ebe237cc3b5f370ca,

title = "Study on heat transfer performance of antifreeze-R134a heat exchanger (ARHEx)",

abstract = "In this paper, the liquid cooling and vapor compression refrigeration system based on an Antifreeze-R134a Heat Exchanger (ARHEx) was applied to the thermal management system for high-power avionics in helicopters. The heat transfer performance of the ARHEx was studied. An experimental prototype of ARHEx was designed and established. A series of experiments was carried out with a ground experimental condition. A heat transfer formula for the antifreeze side in the ARHEx was obtained by means of the coefficient of Nusselt number with experimental analysis. The performance of heat transfer and pressure drop for the refrigerant side of the ARHEx was deduced for the given condition.",

keywords = "Antifreeze-R134a heat exchanger, Avionics, Heat transferperformance, Thermalmanagement",

author = "Liping Pang and Kun Luo and Shizhao Yu and Desheng Ma and Miao Zhao and Xiaodong Mao",

note = "Publisher Copyright: {\textcopyright} 2020 by the authors. Licensee MDPI, Basel, Switzerland.",

year = "2020",

month = nov,

day = "2",

doi = "10.3390/en13226129",

language = "英语",

volume = "13",

journal = "Energies",

issn = "1996-1073",

publisher = "Multidisciplinary Digital Publishing Institute (MDPI)",

number = "22",

}

TY - JOUR

T1 - Study on heat transfer performance of antifreeze-R134a heat exchanger (ARHEx)

AU - Pang, Liping

AU - Luo, Kun

AU - Yu, Shizhao

AU - Ma, Desheng

AU - Zhao, Miao

AU - Mao, Xiaodong

PY - 2020/11/2

Y1 - 2020/11/2

N2 - In this paper, the liquid cooling and vapor compression refrigeration system based on an Antifreeze-R134a Heat Exchanger (ARHEx) was applied to the thermal management system for high-power avionics in helicopters. The heat transfer performance of the ARHEx was studied. An experimental prototype of ARHEx was designed and established. A series of experiments was carried out with a ground experimental condition. A heat transfer formula for the antifreeze side in the ARHEx was obtained by means of the coefficient of Nusselt number with experimental analysis. The performance of heat transfer and pressure drop for the refrigerant side of the ARHEx was deduced for the given condition.

AB - In this paper, the liquid cooling and vapor compression refrigeration system based on an Antifreeze-R134a Heat Exchanger (ARHEx) was applied to the thermal management system for high-power avionics in helicopters. The heat transfer performance of the ARHEx was studied. An experimental prototype of ARHEx was designed and established. A series of experiments was carried out with a ground experimental condition. A heat transfer formula for the antifreeze side in the ARHEx was obtained by means of the coefficient of Nusselt number with experimental analysis. The performance of heat transfer and pressure drop for the refrigerant side of the ARHEx was deduced for the given condition.

KW - Antifreeze-R134a heat exchanger

KW - Avionics

KW - Heat transferperformance

KW - Thermalmanagement

UR - https://www.scopus.com/pages/publications/85106654459

U2 - 10.3390/en13226129

DO - 10.3390/en13226129

M3 - 文章

AN - SCOPUS:85106654459

SN - 1996-1073

VL - 13

JO - Energies

JF - Energies

IS - 22

M1 - 6129

ER -

Study on heat transfer performance of antifreeze-R134a heat exchanger (ARHEx)

Abstract

UN SDGs

Keywords

Access to Document

Other files and links

Fingerprint

Cite this