High Capacity Grooved Heat Pipes

Dubois, M.; Mullender, Bernard; Oost, Stéphane Van; Supper, W.

doi:10.4271/932303

Cited by 8 publications

(2 citation statements)

References 8 publications

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“…This configuration combines a high capillary pumping pressure with a low axial pressure drop in the liquid. 2,3 In addition, the retardation of the liquid flow due to the countercurrent vapor flow over the liquidvapor interface is minimized as compared to other axial groove designs. However, the radial thermal resistance to heat transfer of the reentrant groove geometry may be larger compared to rectangular, trapezoidal, or triangular groove designs due to an increase in the wall thickness of the heat pipe.…”

Section: Introductionmentioning

confidence: 97%

Fluid Flow in Axial Reentrant Grooves with Application to Heat Pipes

Thomas

Damle

2005

Journal of Thermophysics and Heat Transfer

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The fully developed laminar flow within a reentrant groove has been analyzed using a finite element model. A parametric analysis was carried out to determine the Poiseuille number Po = fRe, the dimensionless mean velocity v * , and the dimensionless volumetric flow rateV * as functions of the geometry of the reentrant groove (groove height 1.0 < -H * < -4.0, slot half-width 0.05 < -W * /2 < -0.9, and fillet radius 0.0 < -R * f < -1.0), and the liquid-vapor shear stress (0.0 < -− −τ * lv < -2.5). The case in which the meniscus recedes into the reentrant groove was examined and could be a result of evaporator dryout or insufficient liquid fill amount. The cross-sectional area of the liquid in the groove, A * l , the meniscus radius R * m , and the aforementioned flow variables were calculated as functions of the meniscus contact angle (0 < -φ < -40 deg) and the meniscus attachment point (0.0 < -H * l < -2.75). Finally, the results of the numerical model were used to determine the capillary limit of a low-temperature heat pipe with two different working fluids, water and ethanol, for a range of meniscus contact angles. Nomenclaturecenter of circular portion of reentrant groove to top of slot, m H l = vertical location of attachment point of meniscus to reentrant groove wall, m H l,s = vertical location of attachment point of meniscus to sinusoidal groove wall, m H s = height of sinusoidal groove, m H tr = height of trapezoidal groove, m H * = H/R H * l = H l /R h f g = heat of vaporization, J/kg K = thermal conductivity, W/(m · K) L a = adiabatic length, m L c = condenser length, m L e = evaporator length, m L eff = effective heat pipe length, L e /2 + L a + L c /2, m N g = number of grooves n = coordinate normal to the liquid-vapor interface n * = n/R P = wetted perimeter, m Po = Poiseuille number, f Re P * = P/R = pressure, N/m 2 Q cap = capillary limit heat transport, Ẇ Q g = heat transfer due to a single groove, Ẇ Q t = total heat transported, N gQ g , W q lv = heat flux at the liquid-vapor interface, W/m 2 q * lv = q lv /q R q = internal volumetric heat generation, W/m 3 R = radius of circular portion of reentrant groove, m Re = Reynolds number, ρv D h /µ R f = radius of fillet, m R m = radius of meniscus, m R v = radius of heat pipe vapor space, m R * fwidth of slot, m W l = width of liquid meniscus at attachment point to reentrant groove wall, m W l,s = width of liquid meniscus at attachment point to sinusoidal groove wall, m W s = width of sinusoidal groove, m W tr = width of trapezoidal groove, m W * = W/R W * l = W l /R x, y, z = Cartesian coordinate directions x f,0 , z f,0 = location of center point of circular fillet, m x t , z t = point of tangency of fillet and circular portion of reentrant groove, m x * , y * , z * = x/R, y/R, z/R x * f,0circular segment duct half-angle, rad 395 Downloaded by MONASH UNIVERSITY on February 3, 2015 | http://arc.aiaa.org | 396 THOMAS AND DAMLEβ = aspect ratio for rectangular and trapezoidal grooves, 2H r /W r or 2H tr /W tr γ = triangular groove half-angle, rad θ = trap...

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Section: Introductionmentioning

confidence: 97%

Fluid Flow in Axial Reentrant Grooves with Application to Heat Pipes

Thomas

Damle

2005

Journal of Thermophysics and Heat Transfer

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“…1(a). This configuration combines a high capillary pumping pressure with a low axial pressure drop in the liquid (Dubois et al [2], [3]). In addition, the retardation of the liquid flow due to the countercurrent vapor flow over the liquid-vapor interface is minimized as compared to other axial groove designs.…”

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confidence: 99%

Analysis of Fluid Flow in Axial Re-entrant Grooves with Application to Heat Pipes

Thomas

Damle

2004

37th AIAA Thermophysics Conference

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The fully developed laminar flow within a re-entrant groove has been analyzed using a finite element model. Re-entrant grooves have been used in both axially-grooved heat pipes and in monogroove heat pipes. The main benefit to using this type of wick structure is the reduction of the liquid pressure drop along the length of the groove due to countercurrent liquid-vapor interaction at the meniscus. All previous researchers assumed that the pressure drop within the liquid could be modelled as flow within a smooth tube, but the results of the current analysis show that this assumption can lead to significant errors in the pressure drop prediction. An extensive literature survey was completed and the results of five previous studies were used to validate the current numerical model. It was found that the present finite element model is both more accurate and consumes less computer resources than a finite difference based model developed previously by one of the authors of the current manuscript. A parametric analysis was carried out to determine the Poiseuille number, Po = f Re, the dimensionless mean velocity, v * , and the dimensionless volumetric flow rate,V * , as functions of the geometry of the re-entrant groove (groove height 1.0 ≤ H * ≤ 4.0, slot half-width 0.05 ≤ W * /2 ≤ 0.9, fillet radius 0.0 ≤ R * f ≤ 1.0), and the liquid-vapor shear stress (0.0 ≤ −τ * lv ≤ 2.5). It was determined that the flow variables were strongly affected by the groove height, slot half-width and liquid-vapor shear stress, but were relatively unaffected by the fillet radius. The case in which the meniscus recedes into the re-entrant groove was examined, which could be a result of evaporator dry-out or insufficient liquid fill amount. The cross-sectional area of the liquid in the groove, A * l , the meniscus radius, R * m , and the above-mentioned flow variables were calculated as functions of the meniscus contact angle (0 • ≤ φ ≤ 40 • ) and meniscus attachment point (0.0 ≤ H * l ≤ 2.75). In general, the flow variables were more strongly affected by the meniscus attachment point than the meniscus contact angle. Finally, the results of the numerical model were used to determine the capillary limit of a low-temperature heat pipe with two different working fluids, water and ethanol, for a range of meniscus contact angles. The capillary limit heat transfer was found to attain a maximum value in the slot region and then decreased dramatically when the meniscus receded into the circular region of the re-entrant groove. NomenclatureA g = total cross-sectional area of the re-entrant groove, m = maximum mean liquid velocity, m/s v * = µv/R 2 (−dp/dy) v * = µv/R 2 (−dp/dy) V = volumetric flow rate, vA l , m 3 /ṡ V * = µV /[R 4 (−dp/dy)] W = width of the slot, m W * = W/R W l = width of the liquid meniscus at the attachment point to the re-entrant groove wall, m= width of the liquid meniscus at the attachment point to the sinusoidal groove wall, m W s = width of the sinusoidal groove, m W tr = width of the trapezoidal groove, m x, y, z = Carte...

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Elaboration of scientific-technological foundations for up-to-date heat pipe design for space application on the basis of the materials of the INTAS-CNES-NSAU project

Baturkin¹

2009

Kosm. nauka tehnol.

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High Capacity Grooved Heat Pipes

Cited by 8 publications

References 8 publications

Fluid Flow in Axial Reentrant Grooves with Application to Heat Pipes

Fluid Flow in Axial Reentrant Grooves with Application to Heat Pipes

Analysis of Fluid Flow in Axial Re-entrant Grooves with Application to Heat Pipes

Elaboration of scientific-technological foundations for up-to-date heat pipe design for space application on the basis of the materials of the INTAS-CNES-NSAU project

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