Proceedings of IPACK2007
ASME InterPACK ’07
July 8-12, 2007, Vancouver, British Columbia, CANADA
David B. Sarraf
Advanced Cooling Technologies, Inc.
1046 New Holland Avenue
Lancaster, PA 17601
Phone: 717-295-6059, Fax: 717-295-6064
William G. Anderson
Advanced Cooling Technologies, Inc.
1046 New Holland Avenue
Lancaster, PA 17601
Phone: 717-295-6104, Fax: 717-295-6064
Copper water heat pipes are a well-established solution for many conventional electronics cooling applications; however they have several problems when applied to high temperature electronics. The high vapor pressure of the working fluid combined with the decreasing strength of an already soft material leads to excessive wall thickness, high mass, and an inability to make thermally useful structures such as planar heat pipes (vapor chambers) or heat pipes with flat input surfaces. Titanium/water and Monel/water heat pipes can overcome the disadvantages of copper/water heat pipes and produce a viable thermal management solution for high temperature electronics. Water remains the fluid of choice at temperature up to about 280°C due to its favorable transport properties. Life tests have shown compatibility at high temperature. At temperatures above roughly 300°C, water is no longer a suitable fluid, due to high vapor pressure and low surface tension as the critical point is approached. At higher temperatures, another working fluid/envelope combination is required, either an organic or halide working fluid. Preliminary halide life test results are presented, giving fluids that can operate at temperatures as high as 425°C. At higher temperatures, alkali metal heat pipes are suitable. Water and the higher temperature working fluids can offer solutions for cooling high-temperature electronics, or those working at or above 150°C.
High Temperature Electronics require innovative thermal management devices. Copper water heat pipes are a well established solution for many conventional electronics cooling applications; however they have several problems when applied to high temperature electronics. The high vapor pressure of the working fluid combined with the decreasing strength of an already soft material leads to excessive wall thickness, high mass, and an inability to make thermally useful structures such as planar heat pipes (vapor chambers) or heat pipes with flat input surfaces.
Historically, water was used with copper at temperatures up to about 150°C. Recent work has shown that titanium/water and Monel/water heat pipes can overcome the disadvantages of copper/water heat pipes, and produce a viable thermal management solution for high temperature electronics. Water remains the fluid of choice for temperatures up to 280°C, due to its favorable transport properties. Monel and titanium offer much higher strength and result in reasonable wall thickness and mass. The paper will present evidence that high temperature water heat pipes are now a mature technology that is ready for widespread application, including life test data (over 2.2 years with no problems), suitable wick structures, and heat pipe fabrication and testing.
At higher temperatures, the water vapor pressure is too high, and alternative working fluids are required. These fluids offer good thermal performance but at much lower vapor pressures and offer the potential of using low-mass wall materials such as aluminum or titanium. Potential working fluids include several organic compounds, as well as halides. The paper will discuss work to qualify working fluids at temperatures up to 425°C (at higher temperatures, alkali metal working fluids can be used). Water and the higher temperature working fluids can offer solutions for cooling high-temperature electronics, or those working at or above 150°C.
HIGH STRENGTH ENVELOPE MATERIALS
Titanium, titanium alloys, Monel 400, and Monel K500 have higher yield strength and lower density than copper. As discussed below, they have been shown to be compatible with water, hence be used for thinner and lighter weight heat pipes than copper at a given operating temperature and working fluid vapor pressure. Titanium has been used in heat pipes with the following fluids:
- Sodium (Anderson et al., 2006)
- Potassium (Lundberg, 1984, Sena and Merrigan, 1989)
- Cesium (Dussinger, Anderson, and Sunada, 2005)
- Dowtherm A (Heine, Groll, and Brost, 1984, Groll, 1989)
- Toluene (Heine, Groll, and Brost, 1984, Groll, 1989)
- Water (Heine, Groll, and Brost, 1984, Groll, 1989),
– Antoniak et al., 1991, Anderson et al., 2006)
- Ammonia (Ishizuka, Sasaki, and Miyazaki 1985)
- Nitrogen (Swanson et al., 1995)
– Titanium has also been used in loop heat pipes with water and
cesium (Anderson et al., 2006).
Monel 400 and Monel K500 are two other potential heat pipe materials (Monel 400 Technical Bulletin, 2005, Monel K- 500 Technical Bulletin, 2005). Monel 400 is a solid solution alloy with roughly 63% nickel and 30% copper. It is a single phase alloy, since the copper and nickel are mutually soluble in all proportions. It can only be hardened by cold working. Monel K500 is a similar nickel-copper alloy, with the addition of small amounts of aluminum and titanium that give greater strength and hardness. The system is age-hardened by heating so that small particles of Ni3(Ti, Al) are precipitated throughout the matrix, increasing the strength of the material. The material must be annealed before welding, for ductile welds.
TITANIUM/WATER AND TI/MONEL LIFE TESTS
Life tests are required to verify that the heat pipe envelope, wick, and working fluid are compatible for the potentially long operating life of a heat pipe. The two major consequences of incompatibility are corrosion and the generation of non-condensable gas, or both. The resulting corrosion products can block portions of the wick, preventing the heat pipe from operating properly. In more extreme cases, the heat pipe can leak.
A series of simple cylindrical heat pipes were constructed and operated to demonstrate compatibility with the wall materials and working fluid. These life test pipes were electrically heated and had three thermocouples to monitor the temperature gradient along the heat pipe; see Figure 1. Any incompatibility would result in the generation of noncondensable gas, which would then accumulate in the heat pipe condenser and result in a cold end or increased end-toend temperature gradient. The heat pipes were operated at either 227 or 277°C to accelerate any reaction between the wall and working fluid. Once weekly the input power was reduced so that the heat pipes operated near 60°C. This reduced the vapor pressure of the water from roughly 60 atm (277°C) or 26 atm (227°C) to only 0.2 atm. That allowed any non-condensable gas present to expand and cover more of the condenser so it could be more easily detected.
Titanium/Water and Monel/Water life tests now have up to 2.3 years of operation, with no incompatibilities detected. The life tests include commercially pure titanium (CP-Ti), titanium alloys, Monel 400, and Monel K500 envelopes. Details of the tests are given in Table 1. The wicks tested include CPTitanium screen, CP-Titanium sintered powder, Monel 400 screen, and Monel 400 sintered powder.
Pipe 105, Monel 200 Mesh Monel Wick
Phase II Pipe 3, Grade 7 Ti Cylinder
Figure 3. Low Temperature (Non-Condensable Gas) Measurements for Grade 7 Titanium Cylinder/CP-Titanium Screen/Water Heat Pipe 3. Operating at 550 K. Purged after 3509 hours of operation.[/caption]
Typical results are shown in Figures 2 and 3 for Monel and a titanium alloy, respectively. The Monel pipes have shown no signs of gas generation.
As shown in Figure 3, the titanium heat pipes all generated gas initially. This was believed to be a result of a passivation process that produced titanium oxide on the surface of the heat pipe. The gas was removed from all of these pipes by heating to about 115°C and venting them. The thermocouples are monitored to verify that the noncondensable gas has been forced out of the condenser by the pressure difference. The heat pipe fill tube is then resealed.
INTERMEDIATE TEMPERATURE WORKING FLUIDS
The heat pipe development work and life tests discussed above show that water working fluid in titanium or Monel heat pipes is an excellent device for cooling electronics at temperatures up to 280°C. As the temperature gets closer to the critical point of water (374°C), the vapor pressure becomes too high, and the surface tension too low, for water to be suitable as a working fluid. For very high temperatures (above roughly 425°C), cesium and other alkali metals can be used as the heat pipe working fluid.
Alternative working fluids are currently under investigation for the temperature range from 150 C to 450 C. In addition to high temperature electronics cooling, other heat pipe applications include spacecraft radiators, fuel cell thermal control, and waste heat recovery systems. Many other working fluids are available which have lower vapor pressure, including mercury, Dowtherm fluids, sulfur/iodine mixtures, Napthalene, Phenol, Toluene, and a variety of halide salts (Anderson et al., 2004, Deverakonda and Anderson, 2005).
Typical vapor pressures for several halides are shown in Figure 4. Virtually all of the fluids have a lower vapor pressure than water, and many of them are an order of magnitude lower. An attractive feature of the halides is that the chloride, bromide, and iodide generally cover a wide range of vapor pressure (see TiCl4, TiBr4, and TiI4 in Figure 4).
For each of these fluids the merit number was also plotted to allow comparison of these materials with each other and with water. The merit number (liquid transport factor) is a
means of ranking heat pipe fluids, with higher merit number more desirable:
Figure 5 compares the figure of merit of some of the replacement fluids with water. Water has a much higher Merit number than that other fluids, which is why it is used at temperatures up to 300°C. At higher temperature other fluids must be used. Cesium is shown for comparison only. It is suitable only for temperatures above about 450°C, since the sonic limit prevents it from carrying significant power at lower temperatures.
INTERMEDIATE TEMPERATURE LIFE TESTS
As discussed above, water is generally the fluid of choice at temperatures below about 280-300°C, due to its superior fluid properties. At higher temperatures, another fluid must be used. Table 2, based on data in Saaski and Hartl (1980), and Groll et al (1989, Heine et al., 1984) summarizes previous life tests with organic fluids at temperatures above 250°C.
As shown in Table 2, the organic fluids are not compatible at temperatures approaching 400°C, but only at lower temperatures. Because of this, we have concentrated on the halides. The halides are salts of metals such as titanium, aluminum, boron, antimony, tin, and silicon.
Saaski and Owzarsky (1977) proposed an electrochemical method to predict the compatibility of halide working fluids with envelope materials. Tarau et al. (2007) found that this procedure had good agreement with previous life tests, and used it to select new working fluid/envelope combinations to test.
The procedure calculates the electromotive force difference of the reaction between the working fluid and envelope. The standard electromotive force difference or the potential difference, ΔE0, is the difference between the decomposition potentials of the two halides, the metal envelope halide, MaXcp and the working fluid, MbXc:
The standard EMF difference, ΔE0 is the decomposition potential of the envelope minus the decomposition potential of the fluid. If the standard EMF difference, ΔE0, is positive, then the reaction can proceed spontaneously and the wall will react chemically. When the standard EMF difference is negative, the probability of spontaneous reaction decreases significantly. This gives the following working fluid/envelope material selection criterion: The envelope material halide should have a lower decomposition potential than the working fluid halide. This is shown in Figure 6. AlCl3 and TiCl4 have a high decomposition potential, so they are good working fluids. Molybdenum and iron have a low decomposition potential, so should be good envelope materials.
As shown in Table 3, Tarau et al. compared the theoretical predictions with existing halide life test data, and obtained very good agreement in all but two cases. For Titanium/AlBr3, the theory predicts that the system was incompatible.
However, TiAl was formed during the tests, which was not predicted by the theory. The theory predicts that AlBr3 should be compatible with pure aluminum. During the life tests, the AlBr3 attacked the grain boundaries in the aluminum alloys; clearly the reactivity of alloying additions in commercial alloys requires closer consideration.
Envelope Material Selection
The electromotive force difference was used to select envelope materials for halide life tests. Potential envelope materials include aluminum, aluminum alloys, titanium, titanium alloys, carbon steel, stainless steels, and the superalloys. The dominant metallic components for these envelopes include Ti, Ni, Fe, Cr, Mo and Al. The following halides were examined: aluminum chloride, aluminum bromide, antimony chloride, antimony bromide, bismuth chloride, gallium chloride, lead chloride, magnesium chloride, tin dichloride, tin tetrachloride, zinc chloride and zirconium chloride.
The electromotive force differences are shown in Figure 7. Values above zero are unstable. The calculations used a temperature of 400°C (673 K), linearly interpolating the available data (The potential difference is only a weak function of temperature).
Aluminum is the least suitable envelope material for the halides, with the exception of Mg and Zr. From an EMF standpoint, the best envelope material would be molybdenum, followed by iron. All of the halides have strong negative potential differences with Mo and Fe, hence have a low probability of spontaneous reaction. The results for iron suggest that carbon steel is a relatively stable envelope material for almost all the halides. Nickel, which is a major component in stainless steels and superalloys, shows a moderate lack of stability with bismuth trichloride, antimony trichloride and tin tetrachloride. However, it might be stable with the other halides including tin dichloride. Titanium has a higher tendency for corrosion, especially in the presence of antimony tribromide, bismuth trichloride, antimony trichloride and tin tetrachloride.
Table 4. Estimated Envelope/Halide Compatibility
Table 5. Initial Life Results.
Halide Life Tests
The data in Figure 7 was used to estimate the compatibility of halides with six different potential envelope materials, see Table 4 (0 is least compatible, and 2 is most compatible). Aluminum and titanium were examined because they are lightweight, and steel was considered because iron appears to be very compatible, see Figure 7.
Ivan Locci (2006) identified the following Hastelloy superalloys materials as possible heat pipe wall materials: B-3 (Ni-Mo), C-2000 (Ni-Cr-Mo), and C-22 (Ni-Cr-Mo-W). The selection criteria was (Locci, 2006): “The procurement of the 3 superalloys was initially based on the great general corrosion behavior to acids or excellent stress corrosion cracking and pitting resistance reported on the alloys. [The three alloys can be used to] investigate the influence of ternary
additions, e.g. the effect of Mo, Cr, or W to the heat pipe environment. Weldability was another critical factor that was considered, and in general the interest of using superalloys is the much higher specific strength to compete against Ti- or Alalloys (e.g. reduced wall thickness -> comparable density).”
From Table 4, the four halides that are believed to be most compatible with the superalloys were AlBr3, SnCl4, and TiCl4. Heat pipes were fabricated with the three superalloys and the three halides, see Table 5. TiBr4 is also believed to be compatible, based on its chemical similarity to TiCl4. However, it is significantly more expensive, so it will be examined with superalloys only if TiCl4 is compatible.
Tarau et al. (2007) have already shown that TiCl4 is compatible with titanium, so TiBr4 was put on test in a titanium envelope. Preliminary results for the halide life tests are shown in Table 5. The AlBr3, TiCl4, and TiBr4 appear to be compatible, while the SnCl4 is showing signs of gas generation.
Two alternatives to copper/water have been presented. The first, using water with high strength wall materials, gives the high performance of water at temperatures up to 300°C. Indications of maturity were presented, including life test data, the existence of suitable wick structure, and the ability to fabricate heat pipes and predict their performance accurately. Titanium/water and Monel/water heat pipes can be considered a mature or mainstream technology that is ready for widespread application. The second alternative presented was replacement working fluids. These offer good thermal performance but at much lower vapor pressures and offer the potential of using low-mass wall materials such as aluminum or thin stainless steel. This alternative is less mature, however, and will require additional work to fully characterize the thermodynamic properties of some of the working fluids and to identify envelopes with long-term compatibility. Either of the two alternatives can offer a solution for cooling high-temperature electronics, or those working at or above 150°C.
Much of the work presented in this paper was sponsored by NASA Glenn Research Center under contracts NNC04CA32C and NNC05TA36T. Duane Beach was the technical monitor. We would like to thank Ivan Locci of NASA Glenn Research Center for providing the superalloy envelopes, as well as for many helpful discussions. David Glatfelter, Rodney McClellan, and Chris Stover of Advanced Cooling Technologies were the principal technicians for the work described. They fabricated and tested the life test heat pipes and conducted the wick development work.
Anderson, W. G., Dussinger, P. M., Bonner, R. W., and Sarraf, D. B., “High Temperature Titanium-Water and Monel-Water Heat Pipes,” 4th IECEC, American Institute of Aeronautics and Astronautics, Reston, VA, 2006, Paper No. AIAA-2006-4113.
Anderson, W. G., Rosenfeld, J., Devarakonda, A., and Mi,Y., “The Evaluation of Heat Pipe Working Fluids In The Temperature Range of 450 to 750 K,” STAIF-2004, AIP Conference Proceedings No. 699, 2004, pp. 20-27.
Devarakonda, A., and Anderson, W. G., Thermo-Physical Properties of Intermediate Temperature Heat Pipe Fluids, NASA Glenn Research Center, NASA/CR-2005-213582,
Cleveland, OH, 2005.
Dussinger, P. M., Anderson, W. G., and Sunada, E. T., “Design and Testing of Titanium/Cesium and Titanium/Potassium Heat Pipes,” Proceedings of the 2005 IECEC, AIAA, ISBN 1563477696, San Francisco, Ca, August 15-18, 2005.
Groll, M., “Heat Pipe Research and Development in Western Europe”, Heat Recovery Systems and CHP (Combined Heat & Power), 9(1), pp. 19-66, 1989.
Heine, D., M. Groll, and O. Brost, “Chemical Compatibility and Thermal Stability of Heat Pipe Working Fluids for the Temperature Range 200 °C to 400 °C,” 8th ChiSA Congress, Prague, September 3-7, 1984.
Ishizuka, M., Sasaki, T., and Miyazaki, Y., “Development of Titanium Heat Pipes For Use In Space,” Proceedings of the Symposium on Mechanics for Space Flight, pp. 157-165, March, 1985.
Locci, I. E., Devarakonda, A., Copeland, E. H., and Olminsky, J. K., “Analytical and Experimental Thermo-Chemical Compatibility Study of Potential Heat Pipe Materials,” 3rd IECEC, American Institute of Aeronautics and Astronautics, Reston, VA, 2005, Paper No. AIAA-2005-5666.
Locci, I. E., personal communication, 2006.
Lundberg, L. B., “Titanium-potassium heat pipe corrosion studies,” International Symposium on High Temperature Corrosion in Energy Systems, Detroit, MI, Sep. 1984.
Monel 400 Technical Bulletin, Special Metals, http://www.specialmetals.com/documents/Monel%20alloy%2 0400.pdf, 2005.
Monel K-500 Technical Bulletin, Special Metals, http://www.specialmetals.com/documents/Monel%20alloy%2 0K-500.pdf, 2005.
Saaski, E. W., and Owzarski, P. C., Two-Phase Working Fluids for the Temperature Range 50° to 350°C, NASA CR-135255, NASA Lewis Research Center, Cleveland, OH, 1977.
Saaski, E. W., and Hartl, J. H., Two-Phase Working Fluids for the Temperature Range 50 to 350°C, NASA CR-159847, NASA Lewis Research Center, Cleveland, OH, 1980.
Sena and J. T., Merrigan, M. A., “Niobium 1 percent Zirconium/Potassium and Titanium/Potassium Life-Test Heat Pipe Design And Testing,” proceedings of the 7th Symposium on Space Nuclear Power Systems, 195, American Institute of Physics, Melville, NY, Jan. 1990.
Swanson, T., Buchko, M.,. Brennan, P., Bello, M., and Stoyanof; M., “Cryogenic Two-Phase Flight Experiment; Results Overview” proceedings of the 1995 Shuttle Small Payloads Symposium, NASA, pp. 111-123, Baltimore, MD, September 25-28, 1995.
Tarau, C., Sarraf, D. B., Locci, I. E., and Anderson, W. G., “Intermediate Temperature Fluids Life Tests – Theory,” Proceedings, STAIF 2007, AIP Conference Proceedings No. 880, pp. 137-146, 2007.