- Tytuł:
- Experimental research of oil pump for a compression-ignition aircraft engine
- Autorzy:
-
Szlachetka, Marcin
Sochaczewski, Rafał
Gęca, Michał Jan - Powiązania:
- https://bibliotekanauki.pl/articles/133729.pdf
- Data publikacji:
- 2019
- Wydawca:
- Polskie Towarzystwo Naukowe Silników Spalinowych
- Tematy:
-
diesel engine
opposed-piston engine
aircraft propulsion system
oil system
oil pump
silnik wysokoprężny
silnik o tłokach przeciwbieżnych
układ napędowy samolotu
układ olejowy
pompa oleju - Opis:
- The paper presents an analysis of the constructions of oil pumps for an aircraft compression ignition engine. It is a two-stroke liquid-cooled engine with a power of 100 kW. The system has 3 cylinders and 6 opposed pistons. The paper estimates the required oil pump capacity to make the engine components well-lubricated. Next, automotive oil pumps for diesel engines are analyzed to select a correct pump for aircraft diesel engine applications. Three pump constructions of different constructions and dimensions of a rotor were select-ed. A measurement bench was designed and built to test these oil pumps in the range of pump shaft speeds from 0 to 4500 rpm and volumetric flow rate up to 150 l/min. The bench also enables stabilization of oil temperature at the required level within the range from 30 to 120oC. In addition, flow resistance through engine slide bearings was simulated by changing the position of a throttling valve at the pump output to regulate pressure in the range of 0-700 kPa. The obtained capacity characteristics of individual pumps versus on oil pressure and temperature allowed us to find an appropriate oil pump to make individual engine nodes well-lubricated.
- Źródło:
-
Combustion Engines; 2019, 58, 4; 142-146
2300-9896
2658-1442 - Pojawia się w:
- Combustion Engines
- Dostawca treści:
- Biblioteka Nauki
Artykuł