Detail publikace
Modeling of Thermal Phenomena in Liquid Cooling System for Aircraft Electric Unit
ANČÍK, Z. TOMAN, J. VLACH, R. HUBÍK, V.
Anglický název
Modeling of Thermal Phenomena in Liquid Cooling System for Aircraft Electric Unit
Typ
Článek recenzovaný mimo WoS a Scopus
Jazyk
en
Originální abstrakt
The aim of this paper is to show the complex thermal analyses used for examining cooling properties of a liquid cooling system integrated into an aircraft fuel metering pump. The cooling is provided by flow of aviation fuel. The main advantage of this solution is easy implementation in the place of engine bay.
Klíčová slova anglicky
Electronics cooling, fuel pump, temperature measurement, thermal factors, thermal management of electronics.
Vydáno
2012-04-12
Nakladatel
IEEE
ISSN
0278-0046
Časopis
IEEE Transactions on Industrial Electronics
Ročník
2011
Číslo
99
Strany od–do
1–1
Počet stran
7
BIBTEX
@article{BUT74384,
author="Zdeněk {Ančík} and Jiří {Toman} and Radek {Vlach} and Vladimír {Hubík}",
title="Modeling of Thermal Phenomena in Liquid Cooling System for Aircraft Electric Unit",
journal="IEEE Transactions on Industrial Electronics",
year="2012",
volume="2011",
number="99",
pages="1--1",
issn="0278-0046"
}