2016
DOI: 10.1016/j.expthermflusci.2016.04.019
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Capillary pressure in graphene oxide nanoporous membranes for enhanced heat transport in Loop Heat Pipes for aeronautics

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Cited by 15 publications
(5 citation statements)
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“…Cowl anti-icing using LHPs in the global hawk UAV was possible due to the proximity of the cowl to the hydraulic system and the relatively small size of the cowl compared to larger civil aircraft engine intake diameters. New developments in wick materials [126] have shown a drastic increase in achievable pressure differential of the LHP, by up to 3.5-fold, which is estimated to extend the working distance of LHP from current 8-10 m to 28-35 m.…”
Section: Ice Protection Systemmentioning
confidence: 99%
“…Cowl anti-icing using LHPs in the global hawk UAV was possible due to the proximity of the cowl to the hydraulic system and the relatively small size of the cowl compared to larger civil aircraft engine intake diameters. New developments in wick materials [126] have shown a drastic increase in achievable pressure differential of the LHP, by up to 3.5-fold, which is estimated to extend the working distance of LHP from current 8-10 m to 28-35 m.…”
Section: Ice Protection Systemmentioning
confidence: 99%
“…Heat pipe that is a compact and effective heat exchanger includes microchannel heat pipe, mesh wick heat pipe, sintered core heat pipe, oscillating heat pipe and thermosyphon heat pipe, and other heat pipe forms [31]. The researchers conducted experimental studies on different types of nanofluids such as Al 2 O 3 [32,33], CuO [34,35], SiO 2 [36,37], Fe 2 O 3 [38,39], and graphene nanosheets [40][41][42] in heat pipes. The results indicated that nanofluids can enhance heat transfer of the heat pipes.…”
Section: Nanofluid Application In Heat Pipesmentioning
confidence: 99%
“…It was found that the addition of PCFSS reduces thermal resistance. The PCFSS with a porosity of 70% and fill ratio of 30% found to be an optimum condition, which helped the heat pipe to operate between 5 and 200 W. Buffone et al 19 developed a graphene-based wick structure for loop heat pipe applicable for aeronautics, in which graphene oxide particles were coated on the surface of nickel sintered powder wick that is facing towards the vapor and found that the capillary pressure was enhanced 3.5 times higher than that of the nickel sintered powder wick. Choi et al 20 developed a wick structure suitable for loop heat pipes by sintering a thin copper nanoparticles film on the microporous copper substrate by low-temperature sintering.…”
Section: Introductionmentioning
confidence: 99%