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Wyszukujesz frazę "Boruc, L." wg kryterium: Autor


Wyświetlanie 1-4 z 4
Tytuł:
Laserowe znakowanie, kodowanie i grawerowanie - kierunki rozwoju technologii i nowe obszary aplikacji
Laser marking, coding and engraving - technology development directions and new applications areas
Autorzy:
Boruc, L.
Powiązania:
https://bibliotekanauki.pl/articles/270098.pdf
Data publikacji:
2011
Wydawca:
Wrocławska Rada Federacji Stowarzyszeń Naukowo-Technicznych
Tematy:
laserowe znakowanie
kodowanie
laser marking
coding
engraving
Opis:
W artykule przedstawiono nowe możliwości laserowego znakowania kodowania i grawerowania. Wskazano nowe obszary zastosowań, a także kierunki rozwoju tej techniki obróbki. Przedstawiono źródła sukcesu tej techniki, m.in.: szeroka paleta oferowanych systemów, dopasowanych do potrzeb aplikacji, łatwość użycia i dostępność dla coraz szerszej grupy odbiorców.
In this paper new possibilities of laser marking, coding and engraving were presented. New areas of methods' applications, modern machine-tools and development directions of these manufacturing techniques were indicated. On the ground of conducted analysis one affirmed, that a source of commercial success were, among other: wide palette of the different lasers, fitted very well for the individual application, easy operation and affordability for the growing number of potential users.
Źródło:
Inżynieria Maszyn; 2011, R. 16, z. 4; 124-128
1426-708X
Pojawia się w:
Inżynieria Maszyn
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Evaluation of the possibilities of adapting a constant volume combustion chamber for research on ignition of hypergolic propellants under low and high-pressure conditions
Autorzy:
Krzesicki, M.
Boruc, Ł.
Kapusta, Ł. J.
Powiązania:
https://bibliotekanauki.pl/articles/133317.pdf
Data publikacji:
2018
Wydawca:
Polskie Towarzystwo Naukowe Silników Spalinowych
Tematy:
hypergolic ignition
hypergolic propellant
ignition delay
drop test
constant volume combustion chamber
zapłon hipergoliczny
opóźnienie zapłonu
komora spalania o stałej objętości
Opis:
In this study, the adaptation possibilities of a constant volume combustion chamber (CVCC) for research on the ignition of hypergolic propellants are presented. The application of hypergolic bipropellants and crucial parameters regarding their ignition behaviour are discussed. The initial studies on ignition delay measurements presented here does not cover the whole range of conditions present in practical systems where hypergolic ignition occurs. In the study, a need for an evaluation of the influence of pressure on the ignition delay was indicated as the reason to conduct research on hypergolic ignition in low and high-pressure environments. Moreover, the study reviews the state-of-the-art experimental methods of investigating the ignition under atmospheric, low and high-pressure conditions, including those utilizing a constant volume combustion chamber. The drop test was pointed out as the most commonly used method; this makes it advantageous in terms of comparing the results with those obtained by other researchers. Therefore, the drop test was selected as a method to be used in a CVCC. The test rig developed here was designed based on a CVCC initially designed for diesel sprays’ visualization in high-pressure conditions. All the required modifications, especially the design of the oxidizer dosing unit, are presented in the study.
Źródło:
Combustion Engines; 2018, 57, 2; 9-13
2300-9896
2658-1442
Pojawia się w:
Combustion Engines
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Numerical investigation of the back pressure influence on urea-water-solution mixing performance in close coupled SCR system
Autorzy:
Rogóż, R.
Bachanek, J.
Boruc, Ł.
Teodorczyk, A.
Powiązania:
https://bibliotekanauki.pl/articles/245838.pdf
Data publikacji:
2018
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
SCR
urea water solution
uniformity
CFD
back pressure
Opis:
The upcoming Euro 6d emission standard puts more even stringent requirements for diesel engine cars, especially in the case of nitrogen oxides (NOx) emission. The most widely used technique to meet tight standards is Selective Catalytic Reduction (SCR) with urea-water-solution (UWS) injection. One of the crucial factors is even ammonia distribution at the catalyst inlet; hence, very often product development is focused around this issue. The product development is supported by both experimental and numerical work. The common approach to measure cross section ammonia distribution on the SCR is using sampling system at catalyst outlet. Very often exhaust layout is opened just after the SCR catalyst, cutting off the rest part for instance tailpipe or Clean-up Catalyst. Therefore, a backpressure at SCR outlet resulting from the downstream part is also eliminated. This could significantly affect flow parameters as the density changes, thus ammonia distribution and wall film deposition may vary as well. Within this work, the influence of the backpressure at SCR outlet on the ammonia distribution and wall wetting was numerically investigated. The simulations were run under various boundary conditions for the Close Coupled SCR architecture. It was shown that depending on the operating point the boundary pressure affects both factors on the different level.
Źródło:
Journal of KONES; 2018, 25, 3; 377-383
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Resistojet thruster with a power system based on supercapacitors
Autorzy:
Mezyk, L.
Kobiera, A.
Boruc, L.
Biczel, P.
Wolanski, P.
Powiązania:
https://bibliotekanauki.pl/articles/115727.pdf
Data publikacji:
2014
Wydawca:
Fundacja na Rzecz Młodych Naukowców
Tematy:
resistojet
thruster
satellite
ster strumieniowy
satelita
Opis:
This paper presents research into a resistojet model that can be powered by supercapacitors for satellite propulsion applications. The performance of the system, calculated including a preliminary study of mass and power budget, shows that this solution has potential for a certain range of space missions. The main problem when designing a pulsed resistojet is the compromise between the thermal capacity of the resistojet and the heat transfer efficiency of the device. When the heater is used in pulsed mode, it should have low mass and thermal capacity in order to reduce the energy required to heat the devices. On the other hand, the main technical restriction in resistojet thrusters is heat transfer due to the laminar regime of the flow in the heater. The heat transfer area should be as large as possible, but the mass of the device limits any such increase in area. In this research several design options were considered in an attempt to find the optimal solution. After research on the oscillating element and porous heater, capillary tubes directly heated by the current were determined to be the most effective solution. A power supply based on supercapacitors was constructed. It consists of 30 supercapacitors of 300 F each, connected to deliver 70 V of voltage, 10F of total capacitance and maximum peak power of 5 kW. Research for three different gases – ammonia, propane and butane – was conducted and the results are presented in this paper.
Źródło:
Challenges of Modern Technology; 2014, 5, 3; 13-21
2082-2863
2353-4419
Pojawia się w:
Challenges of Modern Technology
Dostawca treści:
Biblioteka Nauki
Artykuł
    Wyświetlanie 1-4 z 4

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