Christina Salpingidou
Aristotle University of Thessaloniki
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Publication
Featured researches published by Christina Salpingidou.
Journal of Engineering for Gas Turbines and Power-transactions of The Asme | 2015
Michael Flouros; Andreas Kanarachos; K. Yakinthos; Christina Salpingidou; Francois Cottier
In modern aero-engines, the lubrication system holds a key role due to the demand for high reliability standards. An aero-engine bearing chamber contains components like bearings and gears. Oil is used for lubrication and for heat removal. In order to retain the oil in a bearing chamber, pressurized seals are used. These are pressurized using air from the compressor. In order to avoid overpressurization of the bearing chamber, air/oil passages are provided in the bearing chamber. At the top, a vent pipe discharges most of the sealing air and at the bottom, a scavenge pipe is used for discharging the oil by means of a pump (scavenge pump). The scavenge pipe is setup in most cases by tubes of circular or noncircular cross sections. When the scavenge pipe has to be routed in a way that sharp bends or elbows are unavoidable, flexible (corrugated) pipes can be used. Because of the corrugation, considerable flow resistance with high-pressure drop can result. This may cause overpressurization of the bearing compartment with oil loss into the turbomachinery with possibility of ignition, coking (carbon formation), or contamination of the aircraft’s air conditioning system. It is therefore important for the designer to be capable to predict the system’s pressure balance behavior. A real engine bearing chamber sealed by brush seals was used for generating different air/oil mixtures thus corresponding to different engine operating conditions. The mixtures were discharged through a scavenge pipe which was partly setup by corrugated tubes. Instead of a mechanical pump, an ejector was used for evacuating the bearing chamber. An extensive survey covering the existing technical literature on corrugated tube pressure drop was performed and is presented in this paper. The survey has covered both single-phase and multiphase flows. Existing methods were checked against the test results. The method which was most accurately predicting lean air test results from the rig was benchmarked and was used as the basis for extending into a two-phase flow pressure drop correlation by applying two-phase flow multiplier techniques similar to Lockhart and Martinelli. Comparisons of the new two-phase flow pressure drop correlation with an existing correlation by Shannak are presented for mixtures like air/oil, air/water, air/diesel, and air/kerosene. Finally, numerical analysis results using ansys cfx version 15 are presented.
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering | 2018
Christina Salpingidou; Dimitrios Misirlis; Z. Vlahostergios; Michael Flouros; Fabian Donus; K. Yakinthos
The development of more efficient aero engines is becoming a matter of great importance due to the need for pollutant emissions reduction (e.g. CO2, NOx). Toward this direction, two of the most promising aero engine architectures that have been proposed are the ultrahigh by-pass geared turbofan and the open rotor configurations, both of which are targeting the low thrust-specific fuel consumption and reduced NOx production. In the current study, investigations are performed in order to determine the improvements in thrust-specific fuel consumption for these configurations. More specifically, on the basic geared turbofan and open rotor configurations an intercooler and a recuperator are implemented between the compressors and the exhaust nozzle, respectively. The intercooler is installed in order to reduce the high pressure compressor work demand, while the recuperator is used in order to preheat the compressor discharge air by exploiting the otherwise wasted increased enthalpy content of the exhaust hot gas. The recuperator consists of elliptically profiled tubes and its design is based on the innovative tubular heat exchanger core arrangement that has been invented and developed by MTU Aero engines AG. The intercooled recuperative geared turbofan is evaluated against a nonintercooled recuperative geared turbofan, while the intercooled recuperative open rotor is evaluated against a nonintercooled recuperative open rotor. The results showed that the implementation of intercoolers and recuperators can further improve specific fuel consumption and can also lead to NOx emission reduction.
Applied Thermal Engineering | 2017
Christina Salpingidou; Z. Vlahostergios; Dimitrios Misirlis; Stefan Donnerhack; Michael Flouros; A. Goulas; K. Yakinthos
Aerospace | 2018
Michael Flouros; Francois Cottier; Markus Hirschmann; Christina Salpingidou
Chemical engineering transactions | 2016
Christina Salpingidou; Dimitrios Misirlis; Z. Vlahostergios; S. Donnerhack; M. Flourous; A. Goulas; K. Yakinthos
Journal of Engineering for Gas Turbines and Power-transactions of The Asme | 2017
Christina Salpingidou; Dimitrios Misirlis; Z. Vlahostergios; Stefan Donnerhack; Michael Flouros; A. Goulas; K. Yakinthos
Chemical engineering transactions | 2017
Christina Salpingidou; D. Tsakmakidou; Z. Vlahostergios; Dimitrios Misirlis; Michael Flouros; K. Yakinthos
Aerospace | 2017
Dimitrios Misirlis; Z. Vlahostergios; Michael Flouros; Christina Salpingidou; Stefan Donnerhack; A. Goulas; K. Yakinthos
Chemical engineering transactions | 2016
Christina Salpingidou; Dimitrios Misirlis; Z. Vlahostergios; M. Flourous; S. Donnerhack; K. Yakinthos
Volume 3: Coal, Biomass, and Alternative Fuels; Cycle Innovations; Electric Power; Industrial and Cogeneration; Organic Rankine Cycle Power Systems | 2018
Christina Salpingidou; Z. Vlahostergios; Dimitrios Misirlis; Michael Flouros; Fabian Donus; K. Yakinthos