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http://yadda.icm.edu.pl:80/baztech/element/bwmeta1.element.baztech-cb485a6f-d53a-4235-9226-e73ec5f26a79

Czasopismo

Combustion Engines

Tytuł artykułu

Coolant pump for compression-ignition aircraft engine

Autorzy Gęca, Michał Jan  Pietrykowski, Konrad  Barański, Grzegorz 
Treść / Zawartość
Warianty tytułu
Języki publikacji EN
Abstrakty
EN The article presents an analysis of the design of cooling liquid pumps for a compression-ignition aircraft engine. A 100 kW twin-charged, two-stroke, liquid-cooled engine has 3 cylinders and 6 opposed-pistons. In the first part of the study, the amount of heat needed to be removed by the cooling system was estimated to obtain the required volumetric flow rate. Then, the design of automotive cooling liquid pumps for compression-ignition engines with a Common Rail power supply system and power of about 100 kW was analyzed. The aim of the analysis was to select a suitable pump for applications in the aircraft compression-ignition engine. 5 constructions of different shape, diameter and width of the working rotor were selected. The pressure and volume flow rate were determined for a given rotational speed of the pump on a specially built stand. The operation maps of individual pumps were created to select the most efficient types of pumps.
Słowa kluczowe
PL silnik wysokoprężny   silnik o tłokach przeciwbieżnych   układ napędowy samolotu   układ chłodzenia   pompa wody  
EN diesel engine   opposed-piston engine   aircraft propulsion system   cooling system   water pump  
Wydawca Polskie Towarzystwo Naukowe Silników Spalinowych
Czasopismo Combustion Engines
Rocznik 2019
Tom R. 58, nr 4
Strony 52--57
Opis fizyczny Bibliogr. 21 poz., il. kolor., fot., 1 rys., wykr.
Twórcy
autor Gęca, Michał Jan
autor Pietrykowski, Konrad
autor Barański, Grzegorz
Bibliografia
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Kolekcja BazTech
Identyfikator YADDA bwmeta1.element.baztech-cb485a6f-d53a-4235-9226-e73ec5f26a79
Identyfikatory
DOI 10.19206/CE-2019-408