Advanced science.  Applied technology.

Search

Utilizing Additive Manufacturing to Enhance Liquid Cooling in Complex Castings, 03-R8848

Principal Investigators
Matthew Hoffmeyer
Christopher Wray
Inclusive Dates 
05/01/18 to 05/01/19

Background

Power output and efficiency in modern internal combustion engines are often limited by the ability to control the temperature in critical regions of complex castings. Coolant passage geometry is limited to simple shapes by the need to core or drill the passages. This leaves coolant flow rate in forced convection and nucleate boiling regimes as the only available variable determining heat transfer performance.

The objective of this project was to assess the effect of various geometric enhancements made possible by additive manufacturing on improving heat transfer performance. The results of this project are applicable not only to internal combustion engines, but to any complex castings requiring liquid cooling.

Approach

A rig was constructed where specimens could be heated using electrical cartridge heaters, and careful measurements taken, to determine heat flux rates and convection heat transfer coefficients versus coolant flow rate. A baseline specimen and five specimens using alternative cooling passage geometry were tested under identical conditions. The six tested specimens are depicted in Figure 1.

Accomplishments

All but one of the tested alternative geometry cooling jackets showed significant performance improvement over the baseline passage. Example results are shown in Figures 2 and 3 where heat flux rate and the calculated convection coefficients are plotted versus wall surface temperature for each specimen at a given coolant flow rate.

The results were similar over a wide range of flow rates. In these plots the lattice structure shows much higher performance than the other designs, but this design was also much more restrictive. The results were then normalized by coolant pumping power, and the lattice structure performed similarly to the dimpled, finned and impinging jet approaches when pumping power was held constant.

Tested specimens

Figure 1: The six specimens tested during this project.

Graph showing heat flux by coolant passage.
Graph showing convection coefficients by coolant passage

Figure 2 and 3: Example results from the project.