Thickness dependent variations in surface phosphor thermometry during transient combustion in an HCCI engine
Introduction
The temperature of combustion chamber walls is an important parameter for the generation and validation of predictive models describing heat transfer in internal combustion engines [1], [2], [3]. Amongst measurement techniques for surface temperatures, laser-induced phosphorescence has drawn increasing attention in the past few years, being a versatile alternative to conventional probing techniques such as thermocouples and pyrometry [4], [5], [6], [7], [8]. Thermographic phosphors allow remote temperature sensing with comparatively high temporal resolution by collecting the commonly red-shifted phosphorescence emission from an optically excited thin film that has been coated onto a target surface. Typical excitation sources are usually pulsed UV lasers, but also laser diodes and light emitting diodes have recently been employed as they continue to improve in terms of both price and output power [9], [10], [11]. In order to determine surface temperatures, the decay time or the relative spectral intensity distribution of the phosphor emission are most commonly exploited, the former one often regarded to allow a higher measurement precision [12], [13].
The phosphorescence emission is generally carrying the temperature information from the coated layer on top of the actual target surface, followed by the implicit assumption that the phosphor film is thin enough to adopt the temperature of the covered surface without perturbation. This assumption, however, is critical in thermal non-equilibrium situations as thermographic phosphors often are described as ceramic materials, which in turn are known to be thermal insulators. As for chemically similar thermal barrier coatings, Gentleman et al. identified temperature differences in the order of 100 K for a 140–170 μm thick surface film of YSZ [14].
In a previous study the authors have shown for the first time that temperature gradients can occur throughout a phosphor film, meaning that the phosphor temperature no longer corresponds to the wall surface temperature below. More precisely, this behavior has been observed for ⩾30 μm thick spray coatings of La2O2S:Eu which were applied inside an internal combustion engine [15]. Very recently, a theoretical study by Atakan et al. confirmed these measurement results by thoroughly investigating the optical cross-talk between spatial layers of the phosphor film and by performing a heat transfer analysis based upon our previous experimental results [16]. Another recent study used experimental surface temperatures from thin film thermocouples in an HCCI engine (Homogeneous Charge Compression Ignition) for modeling the influence of combustion chamber deposits (e.g. soot, hydrocarbons) on the wall temperature [17]. Similarly to thermographic phosphors these deposits can have a thermally insulating effect, and as they are globally present, they even influence the combustion process.
In this work a wider range of thicknesses from 5 μm up to 72 μm has been investigated experimentally to remedy a general lack of experimental data needed to quantify this effect and verify theoretical models. Especially, film thicknesses below 30 μm seem a worthwhile target for further investigations in order to study if-, and to which degree, accurate measurements can be obtained by thermographic phosphors in applications with rapidly changing spatial- and temporal temperature gradients. Another question to be addressed in this study is whether and how the temperatures from the front- and backside of phosphor coatings correlate with each other and with cycle-to-cycle variations of the global gas temperature for various film thicknesses. Finally, a second thermographic phosphor (CdWO4), was investigated along with La2O2S:Eu in order to study whether or not temperature gradients for different film thicknesses have a phosphor-specific dependency.
Section snippets
Engine environment
Phosphor film thickness experiments have been performed inside a Toyota diesel engine utilizing an experimental setup similar to the one which was used in preceding publications [15], [18]. Out of four cylinders, the engine was operated on only one cylinder that has been modified for optical access by employing a quartz liner and a piston extension of Bowditch design [19]. The engine was run in HCCI mode using PRF50 fuel, i.e. a fuel-mixture of 50% iso-octane and 50% n-heptane. Further engine
Results and discussion
Crank-angle resolved wall temperatures between −120 CAD (crank-angle degree) and 120 CAD ATDC (After Top Dead Center) have been measured in an HCCI engine using Laser-Induced Phosphorescence. Measurement points were varied in steps of 5 CAD around TDC and had a wider spacing early and late in the cycle. At a speed of 1200 revolutions per minute, the 10 Hz laser system limited the data acquisition to one measurement per combustion cycle at a specific crank-angle. Phosphor film temperatures from
Conclusions
This work is a continuation of efforts to provide experimental data for the distortion of temperature readings by thick phosphor coatings in unsteady combustion environments. Experiments determining surface temperatures in a HCCI engine were performed using two different phosphors and a range of film thicknesses from 5 to 72 μm. These phosphor films were coated on a quartz liner for optical access from two opposite sides of the coating.
Spray coatings ⩽20 μm did not show thermal gradients across
Acknowledgments
This work was performed within the D60l-2 project, funded by Swedish Energy Agency. For further financial support the authors would also like to acknowledge the European Union Seventh Framework Programme (FP7/2007-2011) under Grant agreement no. 265861 (Helios). The authors also express their gratitude to Prof. Bengt Sundén and Helgi Fridriksson for helpful discussions.
References (23)
- et al.
Sens. Actuators, B
(2009) - et al.
Prog. Energy Combust. Sci.
(2011) - et al.
Proc. Combust. Inst.
(2013) - et al.
Surf. Coat. Technol.
(2006) - et al.
Proc. Combust. Inst.
(2013) - et al.
Prog. Org. Coat.
(2010) - J. Chang, O. Güralp, Z. Filipi, D. Assanis, T. Kuo, P. Najt, R. Rask, SAE Tech. Pap. 2004-01-2996, 2004, pp....
- C. Wilhelmsson, A. Vressner, P. Tunestål, B. Johansson, G. Särner, M. Aldén, SAE Tech. Pap. 2005-01-3731, 2005, pp....
- J. Demuynck, M. De Paepe, R. Sierens, S. Verhelst, FISITA World Automotive Congress, Proceedings F2010-A-062, 2010, pp....
- et al.
Rev. Sci. Instrum.
(1997)
Rev. Sci. Instrum.
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