Diesel engine for aircraft propulsion system

• Autorzy: Gęca M. , Czyż Z. , Sułek M.

Identyfikatory

DOI

10.19206/CE-2017-202

• Języki publikacji: EN

Abstrakty

EN

Stricter requirements for power in engines and difficulties in fueling gasoline engines at the airport make aircraft engine manufacturers design new engines capable of combusting fuel derived from JET-A1. New materials used in compression-ignition engines enable weight reduction, whereas the technologies of a Common Rail system, supercharging and 2-stroke working cycle enable us to increase the power generated by an engine of a given displacement. The paper discusses the parameters of about 40 types of aircraft compression ignition engines. The parameters of these engines are compared to the spark-ignition Rotax 912 and the turboprop. The paper also shows trends in developing aircraft compression-ignition engines.

Słowa kluczowe

EN

diesel engine; aircraft propulsion system; power-to-weight ratio; specific fuel consumption

PL

silnik spalinowy; lotniczy układ napędowy; jednostkowe zużycie paliwa

• Wydawca: Polskie Towarzystwo Naukowe Silników Spalinowych
• Czasopismo: Combustion Engines
• Rocznik: 2017
• Tom: R. 56, nr 2
• Strony: 7--13
• Opis fizyczny: Bibliogr. 20 poz., il., wykr.

Twórcy

autor

Gęca M.

• Faculty of Mechanical Engineering at the Lublin University of Technology

autor

Czyż Z.

• Faculty of Mechanical Engineering at the Lublin University of Technology

autor

Sułek M.

• Faculty of Mechanical Engineering at the Lublin University of Technology

Bibliografia

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Uwagi

Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniającą naukę (zadania 2017).