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Combustion Engines

Tytuł artykułu

Analysis of the applicability of a common rail pump for an aircraft engine

Autorzy Sochaczewski, Rafał  Szlachetka, Marcin  Wendeker, Mirosław  Karpiński, Paweł 
Treść / Zawartość
Warianty tytułu
Języki publikacji EN
EN The paper presents an analysis of the possibility of using a common rail pump to supply an aircraft compression-ignition engine. It is an engine with a two-stroke cycle, three cylinders, opposing pistons and 100 kW power. Its each combustion chamber is supply by one or two injectors controlled by electromagnetic valves. In order to assess the possibility of using a common rail pump, four high-pressure pumps were tested on a bench. They are piston pumps differing in the number and geometry of their pumping sections. The analysis included the pumping output, the torque on the pump drive shaft and the power needed to drive the pump. The weight and overall dimensions of the pump were also considered, including the arrangement of the pumping sections and the way the drive is transmitted. The research allowed to optimize the engine power supply system depending on fuel demand and the way the pump is mounted on the engine.
Słowa kluczowe
PL silnik wysokoprężny   dwusuw   tłok przeciwbieżny   pompa paliwa   common rail  
EN diesel engine   two-stroke   opposing piston   fuel pump   common rail  
Wydawca Polskie Towarzystwo Naukowe Silników Spalinowych
Czasopismo Combustion Engines
Rocznik 2019
Tom R. 58, nr 4
Strony 192--197
Opis fizyczny Bibliogr. 29 poz., il. kolor., 1 fot., wykr.
autor Sochaczewski, Rafał
autor Szlachetka, Marcin
autor Wendeker, Mirosław
autor Karpiński, Paweł
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Kolekcja BazTech
Identyfikator YADDA bwmeta1.element.baztech-6b5d5123-90eb-476b-aaa1-91cb21dd638d
DOI 10.19206/CE-2019-432