Wyniki wyszukiwania - BazTech

Ograniczanie wyników

Znaleziono wyników: 3

Liczba wyników na stronie

Wyniki wyszukiwania

Wyszukiwano:
w słowach kluczowych: tłokowy silnik lotniczy

Sortuj według:

Ogranicz wyniki do:

Tests of a prototype spark-ignited, direct-injection engine powered by JET-A1 fuel

Świątek Piotr, Fuć Paweł, Ziółkowski Andrzej, Świątek Lech, Melwiński Paweł

Combustion Engines

2019

R. 58, nr 3

117--120

The article presents a part of the work done in a research and development project being made by SWIATEK Lech Swiatek company. It describes the comparison of different fuels used in piston engines with JET-A1 turbine engine fuel. Next, the proposed combustion process of JET-A1 fuel and a prototype one-cylinder engine are described. In details, a special cylinder head and direct injection programmable computer are presented. In the next part, a designed and built test stand is described. Finally, the results and conclusions are presented. The designed test stand enabled to perform assumed tests. The innovative JET-A1 combustion process was possible to perform and the power and torque were higher in 1900-3000 rpm range than with the gasoline fuel. The designed GDI programmable injection computer enabled to fully control the injection and ignition parameters.

Analiza drgań skrętnych wału śmigłowego silnika lotniczego PZL-200 podczas pracy z zapłonem awaryjnym

Ostapski W., Aromiński A.

Logistyka

2015

nr 3

3636--3645, CD 1

W pracy przedstawiono wyniki badań drgań wału śmigłowego prototypowego silnika lotniczego PZL200, oraz wybranych parametrów w warunkach pracy z awaryjnym układem zapłonowym.

This paper briefly presents results of torsional shaft vibration bench tests for a prototype PZL-200 aircraft engine utilizing secondary ignition system. Some additional parameters while running on secondary ignition system were also presented.

The exhaust emission tests of a Zlin-142 M aircraft

Merkisz J., Markowski J., Pielecha J.

Silniki Spalinowe

2011

R. 50, nr 3

Due to a rapid development of air transport there is a need for assessment of real environmental perils related to the aircraft operation. The main environmental risks are the products of incomplete combustion contained in the exhaust gases. The paper presents the results of the emission tests of a Zlin-142 M under the stationary test conditions.