Litcius/Paper detail

Experimental and Computational Methods for the Evaluation of Double-Wall, Effusion Cooling Systems

Alexander V. Murray, Peter Ireland, Eduardo Romero

2020Journal of Turbomachinery46 citationsDOI

Abstract

Abstract Further improvements in gas turbine efficiency can be sought through more advanced cooling systems—such as the double-wall, effusion system—which provide high cooling effectiveness with low coolant utilization. The double-wall system, as described here, comprises two walls: one with a regular array of impingement holes and the other with a closely packed, regular array of film holes (characteristic of effusion systems). These walls are mechanically and thermally connected via a bank of pedestals which increase coolant wetted area and turbulent flow features. However, a lack of data exists in the open literature on these systems. This study presents a novel experimental heat transfer facility designed with the intent of investigating flat plate versions of such double-wall geometries. Key features of the facility are presented including the use of recirculation to increase the mainstream-to-coolant temperature ratio and the use of infrared thermography to obtain thermal measurements. Some rig commissioning characteristics are also provided which demonstrate well-conditioned, uniform flow. Both coolant and mainstream Reynolds numbers are matched to engine conditions, with the Biot number within around 15% of engine conditions. The facility is used to assess the cooling performance of four double-wall effusion geometries which incorporate various geometrical features. Both overall effectiveness and film effectiveness measurements are presented at a range of coolant mass flows with conclusions drawn as to preferable features from a cooling perspective. The results from a fully conjugate computational fluid dynamics (CFD) model of the facility are presented which utilized boundary conditions obtained during experimental runs. Additionally, a computationally efficient decoupled conjugate method developed previously by the authors was adapted to assess the experimental geometries with the results comparing favorably.

Topics & Concepts

CoolantBiot numberHeat transferWater coolingReynolds numberComputational fluid dynamicsTurbulenceMechanical engineeringMaterials scienceLouverInternal combustion engine coolingTurbine bladeMechanicsTurbineNuclear engineeringEngineeringPhysicsChemistryCombustionOrganic chemistryCombustion chamberHeat Transfer MechanismsTurbomachinery Performance and OptimizationFluid Dynamics and Turbulent Flows