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1

Analysis of operational characteristics of aviation diesel and gas turbine engines for light passenger aircraft

Loginov V., Ukraintes Y.

Prace Instytutu Lotnictwa

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2016

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Nr 4 (245)

103--115

EN

A comparative analysis of aviation diesel and gas turbine engines in the light passenger aircraft system was conducted. Aircraft operational characteristics were obtained with the help of developed modular software system „Integration-2.1". For the formation of 5-9 seater modifications of aircraft as a prototype was taken aircraft Diamond DA42 with the location of passengers without aisle, crew consisted of 1 person. For the formation of 10-20 sealer aircrafts modifications as prototypes were taken aircrafts EV-55 and L-410UVP, the crew consisted of 2 persons, was adopted the full completion of aircraft equipment, power plant consists of two engines was adopted. It shows the economic advisability of the aircraft gas turbine engines use for airplanes of local airlines (5-6 people). It was found that the life-cycle cost of the aircraft with more passengers become lower in modifications with gas turbine engines, therefore, the use of this type of engine is advisable for aircraft with greater passenger capacity. It was found that the main factors influencing the life-cycle cost of the aircraft, are the resource characteristics of the engine, the cost of its maintenance and repair, as well as the price of fuel.

PL

Przeprowadzono analizę porównawczą lotniczych silników diesla i silników turbinowych dla lekkich samolotów pasażerskich. Eksploatacyjne charakterystyki samolotu uzyskane przez rozwinięty modułowy system oprogramowania „Integracja-2.1". Do opracowania modyfikacij 5-9 miejscowych samolotów jako punkt wyjściowy wybrano samolot Diamond DA42 z kabiną pasażerską bez korytarza i jednoosobową załogą. Do opracowania 10-20 miejscowych modyfikacji samolotów jako punkty wyjścia wybrano-samoloty EV-55 i L-410UVP, z dwuosobową załogą, przyjęty przez pełny skład sprzętu lotniczego, punkt mocy składa się z dwóch silników. Wykazano wykonalność ekonomiczną wykorzystania lotniczych turbin gazowych dla samolotów miejscowych linii lotniczych (do 5-6 osób). Stwierdzono, że koszt cyklu życiowego samolotu z wielką ilością pasażerów staje się mniejsza u modyfikacji z turbiną gazową, więc, wykorzystanie tego typu silników jest wskazane na samolotach o większej liczbie miejsc pasażerskich. Stwierdzono, że głównymi czynnikami wpływającymi na koszt cyklu życia samolotu, są cechy silnika, koszt jego utrzymania i naprawy, a także ceny paliwa.

2

Role of a biased electrode in the production of highly charged ions using the DECRIS 14-3 ion source

Leporis M., Bogomolov S., Efremov A., Loginov V., Mironov V.

Nukleonika

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2003

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Vol. 48,suppl.2

89-92

EN

ECR ion sources are used for the production of highly charged ions in various accelerator facilities. In most of them biased electrodes are normally used to increase the ion yield. Physical processes in the plasma of an ion source are quite complicated and the role of a biased electrode is not clear. To investigate the effect of a biased electrode on the intensity of extracted highly charged ions, an axially movable electrode was placed into the plasma chamber of the DECRIS 14-3 ion source. It was found that the intensity of Ar ions depends on the position of the biased electrode and negative bias voltage. The optimal position of the biased electrode was found near the maximum of the magnetic field. Experiments with a pulsed biased electrode were also carried out. The influence of the negative pulse on the ion yield depends on the ion charge state.

3

First beam from the DECRIS 14-2m ion source for Slovak Republic

Loginov V., Bekhterev V., Bogomolov S., Efremov A., Lebedev A., Leporis M., Yazvitsky N., Zelenak A.

Nukleonika

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2003

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Vol. 48,suppl.2

85-88

EN

The ECR laboratory of the Cyclotron Centrum of Slovak Republic (CC SR) in Bratislava, Slovakia, consists of the DECRIS 14-2m ion source and two low energy channels. It is a complete injector, consisting of an ECR ion source, focusing and steering elements, an analyzing magnet, a vacuum system, and an ion beam diagnostic system. The DECRIS 14-2m ion source is a multiply charged heavy ion source based on the electron cyclotron resonance principle. The ECR ion source DECRIS 14-2m and other system have been designed and manufactured at the FLNR JINR. The preliminary testing (magnetic field measurements, vacuum testing and testing of ECR ion source) has been performed at FLNR JINR. The final assembly of the DECRIS 14-2m will be done at the CC SR in Bratislava.