Abstract

Thermal barrier coatings (TBCs) have been investigated both experimentally and through simulation for mixing controlled combustion (MCC) concepts as a method for reducing heat transfer losses and increasing cycle efficiency, but it is still a very active research area. Early studies were inconclusive, with different groups discovering obstacles to realizing the theoretical potential. Nuanced papers have shown that coating material properties, thickness, microstructure, and surface morphology/roughness all can impact the efficacy of the thermal barrier coating and must be accounted for. Adding to the complexities, a strong spatial and temporal heat flux inhomogeneity exists for mixing controlled combustion (diesel) imposed onto the surfaces from the impinging flame jets. In support of the United States Department of Energy SuperTruck II program goal to achieve 55% brake thermal efficiency on a heavy-duty diesel engines, this study sought to develop a deeper insight into the inhomogeneous heat flux from mixing controlled combustion on thermal barrier coatings and to infer concrete guidance for designing coatings. To that end, a co-simulation approach was developed that couples high-fidelity computational fluid dynamics (CFD) modeling of in-cylinder processes and combustion, and finite element analysis (FEA) modeling of the thermal barrier-coated and metal engine components to resolve spatial and temporal thermal boundary conditions. The models interface at the surface of the combustion chamber; FEA modeling predicts the spatially resolved surface temperature profile, while CFD develops insights into the effect of the thermal barrier coating on the combustion process and the boundary conditions on the gas side. The paper demonstrates the capability of the framework to estimate cycle impacts of the temperature swing at the surface, as well as identify critical locations on the piston/thermal barrier coating that exhibit the highest charge temperature and highest heat fluxes. In addition, the FEA results include predictions of thermal stresses, thus enabling insight into factors affecting coating durability. An example of the capability of the framework is provided to illustrate its use for investigating novel coatings and provide deeper insights to guide future coating design.

Highlights

  • finite element analysis (FEA) model of the metal piston and Thermal barrier coatings (TBCs) to examine the effects of coating properties on the temperature swing behavior, and in turn quantify the impact on combustion heat loss and thermal efficiency

  • The temperature fields for the metal and TBC cases were compared to highlight the magnitude of temperature swing exhibited by a gadolinium zirconate (GdZr) coating

  • The additional fidelity gained by coupling computational fluid dynamics (CFD) spatially and temporally varying boundary conditions shows the effect of the characteristic inhomogeneity of mixing controlled combustion. 0D and 1D modeling of thermal barrier coatings in a diesel environment fall short of holistically capturing the heat transfer as they do not account for the spatial effects of impinging flame jets affecting the local heat transfer significantly

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Summary

Introduction

Thermal barrier coatings (TBCs) have been studied for decades as a potential method to reduce heat transfer losses in internal combustion engines (ICEs) and allow for more efficient conversion of fuel energy into mechanical work. Studies [1,2,3,4] investigated the effect of monolithic ceramic coatings applied to the piston crown, cylinder head, and liner surfaces with the aim to develop an adiabatic engine. The results from such studies were mixed, with several indicating a thermal efficiency improvement, while others showed that TBCs had a detrimental impact on efficiency. With a reduction in heat transfer, not all the “saved”

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