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Find Out Computer Model

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Cyclic thermal and mechanical loads on shot sleeves in service can lead to a variety of failures including washout under the pour hole, longitudinal and radial deformation that cause plunger tip sticking and wear, gross cracking and heat checking. However, difficulties are encountered in measuring shot sleeve temperatures and distortions in an actual diecasting machine because the sleeve operates in a thermally and mechanically hostile and cramped environment. This makes computer simulations an attractive alternative to predict distortions and temperatures in sleeves.



A current trend in the industry is the use of larger inner diameter (ID) sleeves to produce large castings. To aid in the production of diecastings and the prediction of thermal and mechanical failures in the sleeves, experimental research was performed to develop computer models to predict thermal gradients and distortions for large ID shot sleeves (7 in.) as a function of sleeve wall thickness. In the following article, this research, including actual and simulated sleeve performance, is reviewed and the results are summarized.

Experimental Data

An H13 tool steel shot sleeve with a 1.98-in. ID and 0,5-in. thickness was instrumented with thermocouple probes along the longitudinal and radial direction to collect temperature data at the molten metal--sleeve interface, A380 aluminum was poured into the sleeve and allowed to cool into a "log." This log was pushed out using a hydraulically actuated plunger tip, and the sleeve was allowed to cool for a specified period of time.

Temperature data was collected through 44 consecutive cycles during which the amounts of lubricant, type of lubricant and the fill percentage were varied. After every cycle, the outside diameter of the sleeve was measured using a micrometer in both vertical and horizontal directions. The temperature data collected then was used to calculate various thermal variables.

The time averaged heat flux (Table 1) and the time averaged heat transfer coefficient (Table 2) were calculated along the length of the sleeve at different locations for two different kinds of lubricants. These measurements were made directly below the pour hole at a distance of 5 in. (127 mm) and 13.5 in. (343 mm) from the pour hole. Measurements were made at angles of 0[degrees], 45[degrees] and 315[degrees] to the axis of symmetry along the vertical section of the sleeve.

Simulation Experiment

A 2-D plain strain finite element model (Fig. 1) was constructed based on data collected from the shot sleeve experiments. A section of the sleeve halfway between the pour hole and the platen was chosen for analysis. The model had the same dimensions as that of the sleeve used to collect data. In the model, the sleeve was assigned the material properties of H-13 tool steel.

The simulation was conducted in two stages. The first stage consisted of performing a thermal analysis on the sleeve to obtain the temperature distribution. This was performed using a 4-node linear quadrilateral element for heat transfer analysis. Based on the thermal analysis results, deformation analysis was performed using a 4-node bilinear plane strain quadrilateral element.

The simulation cycle was split into two steps, the filling phase and the empty phase. The filling period was the time in which molten metal was poured into the shot sleeve and remained there. The empty period was when there was no metal in the sleeve. The average fill period was 94 sec and the average empty time was 63 seconds,

In this model, a convection heat transfer coefficient was applied to the shot sleeve outside surface and inside non-contact surface. An interface heat transfer coefficient at the molten metal-- sleeve interface was used. The heat transfer coefficient value at the interface was critical to the model and was taken from the time-averaged values derived experimentally from the small shot sleeve. This was used as a starting point to compare temperatures between the simulated sleeve and the experimental sleeve, Tables 3 and 4 show the heat transfer coefficients at the interfaces and the corresponding temperatures for the cycle.

The simulation was performed for a section of the sleeve halfway between the platen and the pour hole and corresponded to the section of the sleeve in the experiment that was 5 in. (127mm) from the pour hole. The model had a fill percentage of 33%. The sleeve was assumed to start from room temperature [86F (30C)].

Simulation Results

The stress simulation provided the deformation data on the sleeve. In order to have a better understanding of the sleeve deformations, the maximum sleeve deformation was analyzed.

The maximum expansion of the sleeve took place at its bottom node. The results indicated that the maximum displacement of the bottom node-along the GD of the sleeve was 0.017 in. (0.43mm), which was close to the experimentally measured GD displacement of 0.019 in. (0.48mm) at

Steady state

As an MBS pool ages, or four to six months after component mortgages have passed at least once the threshold for refinancing, the prepayment speed tends to stabilize within a fairly steady range. condition. This clearly reinforces the fact that the computer model provided results that were similar to the experimental results and hence could be used to model sleeves.

Case Study: Predicting Sleeve Distortions in Production

In an effort to gauge the success of the experimental results, a case study was performed.

A large aluminum diecaster using H-13 steel shot sleeves with an inside diameter of 6.693 in. (170mm) and an outside diameter of 9.974 in. (253mm) was interested in predicting sleeve distortions when a sleeve of the same inside diameter and an outside diameter of 11.974 in. (304mm) (thicker wall) was put into service to cast aluminum automotive components. The clearance between the sleeve and the tip was 0.006 in. (0.152mm) at room temperature. The sleeve was unconstrained and allowed to freely expand on its OD.

The models developed were similar to the ones used for verification. The boundary conditions also were similar to those applied on the previous model. In order to validate the use of the correct heat transfer coefficient for large diameter sleeves, the thicker sleeve in use was instrumented with surface thermocouples on its outside diameter and the temperature readings were recorded. These readings were used for comparison with the simulation model in order to estimate the heat transfer coefficient. Based on what was learned from modeling the small shot sleeve, an initial heat transfer coefficient of 1400W/sq m x K was selected.

The process time was obtained from the process sheet provided by the diecaster. The simulation was conducted in 2 steps. The first was the dwell period when the sleeve was in contact with molten metal that lasted for 10.5 sec and the second was when the sleeve was exposed to warm air for a period of 80.5 sec.

The simulation was conducted until the sleeve reached quasi steady state condition so that comparisons could be made between the two sleeves. The 2 sleeves reached quasi steady state condition in approximately 275 cycles. The initial temperature of the shot sleeve was assumed to be 30C and the fill percentage used in the sleeve was 33%,

The simulation was conducted first for the thicker sleeve whose temperatures were compared with the experimental sleeve. This helped in estimating the correct value of the heat transfer coefficient between the sleeve and the molten metal, which was then applied to the thinner sleeve.

In order to achieve agreement between the computer model and the measured surface temperatures on the case study shot sleeve, the heat transfer coefficient between the sleeve and molten metal for the thicker sleeve had to be reduced to 275W/sq m x K. The same value of heat transfer coefficient at the interface was used to conduct simulations on the thinner sleeve, It was assumed that the heat transfer coefficients in the thin and the thick sleeve would be similar since they had the same ID, surface finish, were of the same material (H13), and consisted of the same aluminum alloy at the same initial pour temperature.
Find Out Computer Model
The maximum deformation of the sleeves took place at the bottom node on the ID of the sleeve. The maximum deformation in the thin sleeve was 0.013 in. (0.33mm) and in the thick sleeve was 0.012 in. (305mm). Hence, the thick sleeve expanded slightly less, but did not show appreciable difference in comparison with the thinner sleeve. However, the thick sleeve expanded more uniformly (circularity) than the thin sleeve. In either case, the models predicted the possibility of blow back of molten metal past the plunger tip due to this excessive clearance.

In diecasting practice, however, cooling water to the tip can be adjusted to control tip expansion and maintain desired tip-to-sleeve clearance. Thus, the uniformity of cylindrical expansion may be the more important factor, and the thicker sleeve would be more desirable to avoid excessive tip clearances or sticking due to out of round sleeve conditions.

The thin sleeve expanded by 0.021 in. (0.533mm) and the thick sleeve by 0.022 in. (0.559mm) on the OD. The clearance between the sleeve and the die was designed to be 0.027 in. (0.686mm) at room temperature. Therefore, model results indicated that the design clearance between the sleeve and the die on the OD of the sleeve was adequate to prevent the die from acting as a mechanical constraint to sleeve expansion.

Conclusions

This project was conducted for the purpose of assessing shot sleeve designs causing problems due to deformation. The results from the simulation model were compared with experimental temperature and deformation data. Using these data, heat transfer coefficients were determined. The models were found suitable for temperature and deformation analysis predictions.

Based on the model developed for verification purposes, the distortions experienced in commercial H-13 shot sleeves were studied. Comparisons of the maximum distortion in the commercial sleeves were made and it was determined that there was not much appreciable difference in maximum distortion between the thin and the thick sleeve at a section halfway between the pour hole and the biscuit.

It also was seen that in both cases the clearance between the sleeve and the plunger tip would ultimately increase, which might lead to "blow back" of molten metal past the plunger tip. Hence, the sleeve distortion at the section under study was not large enough to cause plunger tip sticking. It also was seen that a sleeve of smaller ID (relatively low mass) took fewer numbers of cycles (10) to reach quasi steady state thermal condition in comparison to sleeves of larger ID (275 cycles) having relatively high mass.

The computer simulation method developed in this model would be helpful in designing the optimal clearance between the sleeve and the plunger tip. This was an important parameter in the design of the sleeve-tip system since a large clearance leads to "blow back" of molten metal past the plunger tip and a small clearance leads to plunger tip sticking.

The time averaged heat transfer coefficients attained a constant value at quasi steady state irrespective of the lubricant used. The deformation in the sleeve decreased when a lubricant was used in the casting cycle.

Results indicate that the finite element computer models developed can be used to predict shot sleeve temperature gradients and deformations. Models applied to large diameter commercial sleeves successfully predicted distortion. The models predicted that sleeve distortions could lead to blow back of molten metal along a section halfway between the pour hole and the platen.

In the course of the research, it was seen that the sleeve to aluminum heat transfer coefficient measured experimentally (1200W/sq m x K) did not yield the most accurate computer model predictions of temperatures around the shot sleeve in the test stand. Errors inherent in the method used to measure temperatures in the shot sleeve test stand, or assumptions made in the calculation of time averaged heat transfer coefficient may be causes of this discrepancy. Also, the sleeve to aluminum heat transfer coefficient used to model the large diameter sleeves (275W/sq m x K) varied significantly from what was used successfully for small diameter shot sleeves (1400W/sq m x K).

Factors that may influence the rate of heat flow from the aluminum to the sleeve include the sleeve inside diameter curvature, sleeve surface finish, sleeve surface treatments (nitriding), type of tip lubricant used, initial % fill, alloy type and initial pour temperature. These issues require further investigation.

This article is based on a presentation (T01-05) at the 2001 North American Die casting Assn. (NADCA - National Aboriginal Dance Council Australia

NADCA - National Air Duct Cleaners Association

NADCA - National Animal Damage Control Association

NADCA - North American Die Casting Association

NADCA - North American Draft Cross Association, Inc

..... Click the link for more information.) congress. For more information, contact NADCA at 847/292-3620.

The research this article is based on was supported by the U.S. Dept. of Energy) and the Cast Metals coalition.

For a free copy of this article circle No. 341 on the Reader Action Card.

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