Composite capillary core with differential thermal coefficients for loop heat pipe and preparation method of composite capillary core

A technology of loop heat pipe and thermal conductivity, which is applied in the field of composite capillary core and its preparation, can solve the problems of unfavorable heat leakage, low thermal conductivity, and unfavorable heat transfer of loop heat pipe, so as to improve the overall heat transfer performance and improve the Thermal performance, effect of promoting evaporation heat transfer coefficient

Active Publication Date: 2013-01-30
SHANDONG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, the most widely used capillary core is a capillary core made of a single metal material or a non-metallic material, which is difficult to meet the above requirements.
For example, the capillary core prepared by sintering a single metal material has a high thermal conductivity as a whole, whi

Method used

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  • Composite capillary core with differential thermal coefficients for loop heat pipe and preparation method of composite capillary core
  • Composite capillary core with differential thermal coefficients for loop heat pipe and preparation method of composite capillary core
  • Composite capillary core with differential thermal coefficients for loop heat pipe and preparation method of composite capillary core

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Experimental program
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Effect test

Embodiment 1

[0031] combine figure 2 , image 3 , the preparation steps of the composite capillary core with differential thermal conductivity used for the loop heat pipe of the present invention are:

[0032] (1) Mix powder. Fine nickel powder with uniform particle size is selected as the base metal powder for sintering, and fine copper powder is used as the subordinate metal powder. A layer of powder mixture 7, a second layer of powder mixture 8, a third layer of powder mixture 9, a fourth layer of powder mixture 10 and a fifth layer of powder mixture 11;

[0033] (2) Make capillary core sintered parison. After placing the cold press mold (base 5, cylinder 6), the quantitative first layer powder mixture 7, the second powder mixture 8, the third layer powder mixture 9, the fourth layer powder mixture 10 and the fifth layer Layers of powder mixture 11 are put in one after another, and then pressurized to press the powder into the required capillary core shape and size to make capillar...

Embodiment 2

[0036] The difference from Example 1 is that when mixing powders, fine copper powder with uniform particle size is selected as the base metal powder for sintering, and fine nickel powder is used as the subordinate metal powder; during sintering, the sintering temperature is 650°C, and the heating rate is controlled at 20°C / min, the holding time is 40min, and the rest are the same, so no more details will be given.

[0037] Implementation 3:

[0038] The difference from Example 1 is that when mixing powders, fine titanium powder with uniform particle size is selected as the base metal powder for sintering, and fine stainless steel powder is used as the subordinate metal powder; during sintering, the sintering temperature is 850°C, and the heating rate is controlled at 30°C / min, the holding time is 60min, and the rest are the same, no more details.

[0039]Combining the above three embodiments, through the control of process parameters, the present invention can be made into ...

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Abstract

The invention relates to a composite capillary core with differential thermal coefficients for a loop heat pipe and a preparation method of the composite capillary core. A thermal coefficient of the composite capillary core close to an evaporator side of the loop heat pipe is higher than that of the composite capillary core close to a compensator liquid side of the loop heat pipe. The preparation method of the composite capillary core with differential thermal coefficients comprises the following steps of: selecting sintering material matrix metal powders with an infinite mutual solubility and preparing a powder mixture with different mass proportions; filling the mixed powder mixture with different mass proportions in a mould layer by layer; carrying out cold press moulding on the powder mixture after the powder mixture is filled in the mould to form the shape and size required by a capillary core; and at last, sintering the powder mixture to prepare the composite capillary core with differential thermal coefficients. Since the composite capillary core has differential thermal coefficients, the heat transfer performance of the loop heat pipe can be favorably improved and heat control requirements of the loop heat pipe with performances of large heat transfer power and long-distance transmission can be met; and the composite capillary core with differential thermal coefficients can be used for developing efficient loop heat pipes and can be applied to the fields such as aviation heat control and ground electronic equipment cooling and the like.

Description

technical field [0001] The invention relates to a composite capillary core with differential thermal conductivity for loop heat pipes and a preparation method thereof. Background technique [0002] Loop Heat Pipe (LHP for short) is a high-efficiency heat transfer device that uses the phase change heat of the working fluid to achieve heat transfer. The basic components of the loop heat pipe include evaporator, capillary core, compensator, steam pipeline, The working principle of the liquid pipeline and the condenser is as follows: After the heat load is applied to the outside of the evaporator, the working fluid near the outer surface of the capillary core on the evaporator side is first heated and evaporated into steam, then enters the condenser through the steam pipeline, releases heat and then condenses The subcooling becomes a liquid working medium, and then flows through the liquid pipeline to return to the compensator, and then the compensator supplies the liquid workin...

Claims

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Application Information

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IPC IPC(8): F28D15/04B22F3/16
Inventor 辛公明程林
Owner SHANDONG UNIV
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