查看更多>>摘要：In this paper, a novel flowmeter with a double-stage perforated plate structure is proposed, and its pressure drop and flow coefficient are numerically compared with the commonly used single-stage perforated plate structure for the cryogenic fluid measurement. The numerical calculations are based on the Realizable k-epsilon turbulence model and consider the influence of cavitation with thermal effects, which is validated by modeling the cavitating flow of liquid nitrogen over the hydrofoil in the publications. The influence characteristics of the thickness of the single-stage perforated plate on the performance are firstly clarified. Then the emphases are focused on the analysis of the effects of the gap of the double-stage perforated plates on the discharge coefficient, the pressure loss coefficient and the deviation coefficient. The results reveal that compared with the single-stage perforated plate, the double-stage one with the optimized gap has a smaller pressure drop and more horizontal flow coefficient profile with the Re number. The reason for the performance improvement is primarily ascribed to the "thickness effect ", which is explained in detail. While, the increase in the number of stages makes the cavitation more likely to occur, which leads to a smaller Re range of the horizontal flow coefficient profile. The results can be used as a useful reference for the design of the cryogenic differential pressure flowmeter.
查看更多>>摘要：Understanding bubble behaviors and thermal characteristics under various working conditions is of great significance to the efficient utilization of cryogenic propellants. In the present study, simulation models of pool film boiling at horizontal plate and cylinder surface are proposed with Volume of Fluid (VOF) method combined with Lee's phase change model. Based on the physical and thermal performance, the gravity levels, physical properties, and heater structure dimensions are investigated respectively, which could satisfy the common application conditions of cryogenic propellants. The results show that the movement of bubbles at gas-liquid interface is critical to the pool film boiling heat transfer, and also the heat transfer mechanism affects the bubble motion behaviors. The critical wavelength and the most dangerous wavelength are significant length scales for the bubble behaviors in pool film boiling. When the cylindrical heater size is larger than the most dangerous wavelength, the bubble behaviors as well as the heat flux appear the similar characteristics with that at the plate heater surface. Moreover, the critical wavelength is approximately two times of the bubble departure diameter in the present cryogenic liquid boiling events, and the parameters, including liquid-vapor density difference, surface tension, and gas thermal conductivity, could affect the boiling heat flux significantly. In addition, under 0.03g condition, the bubble departure diameter could reach 27 mm and the boiling heat flux decreases to 800 W/ m2, which are significantly different from that in normal gravity. In general, the present CFD model could execute a film boiling study accurately, and a series of detailed results on the bubble behaviors as well as the heat flux could be revealed.
查看更多>>摘要：The second-stage regenerators of pulse tube refrigerators (PTRs) are routinely used to intercept heat loads without disturbing cooling at their base temperatures, often near 4 K. Gifford-McMahon cryocoolers (GMCs) have not yet demonstrated a similar capability to provide regenerator cooling, possibly because of the thermal resistance between their regenerator shell and core. Here we show that GMCs do have capacity to provide regenerator cooling when heat loads are applied directly on the outer regenerator shell, although to a lesser extent compared to PTRs of similar cooling capacity. For example, we intercepted a 900 mW heat load at 21.6 K using the second-stage regenerator of a GMC while only giving up 10 mW of cooling at 3 K (out of 270 mW). This performance may possibly be improved by optimizing heat exchange between heat source and regenerator shell. We provide detailed temperature profile measurements from both a GMC and a PTR while applying heat to the regenerators, showing distinct behavior between the two. We also show that for GMCs, the optimal location of heat injection should be farther from the cold end than for PTRs. Although the physical source of regenerator cooling is less clear for GMCs than it is for PTRs, a useful amount of cooling is available and warrants further study.
查看更多>>摘要：A cooling system using a cryocooler and boil-off gas was proposed for cryogenic propellant storage on the lunar surface. The cryogenic tank was covered with an advanced non-interlayer-contact multi-layer-insulation and coolant from the cryocooler and boil-off gas flow in the layers to remove the heat load. The proposed system included optimization factors for fluid tubes location, cryocooler temperature, and flow rate. A simple uniformtemperature thermal model was developed to optimize boil-off rates and system weights, and the results revealed a Pareto front. A three-dimensional model was developed to discuss the effect of temperature nonuniformity. Finally, the proposed concept was compared to other candidates. The results showed that the proposed system offered a well-balanced system in terms of boil-off rate, system mass, and electric power consumption, which drastically reduced the boil-off rate when compared to only multi-layer insulations, which reduced the weight and power consumptions as compared to zero-boil-off systems.
NSTL
Elsevier