Loop Heat Pipe Technology for Aircraft Anti-Icing Applications

2007-01-3312

09/24/2007

Event
2007 SAE Aircraft and Engine Icing International Conference
Authors Abstract
Content
Loop Heat Pipes (LHPs) are very efficient two-phase capillary heat transfer devices. Because of their characteristics, these devices are used commonly for thermal control applications in several fields including space and aircraft industries. In particular, for aircraft anti-icing applications, some attempts have been made to prevent ice formation on the engine inlet by using LHPs. However, because of the high temperatures involved, it is not advisable to charge the LHP with classical working fluids such as ammonia. In this paper, a trade-off between alternative working fluids is presented and a numerical analysis has been carried out to study the performances of these working fluids. Finally, the preferred solutions are proposed.
Meta TagsDetails
DOI
https://doi.org/10.4271/2007-01-3312
Pages
12
Citation
Gregori, C., Mishkinis, D., Prado, P., Torres, A. et al., "Loop Heat Pipe Technology for Aircraft Anti-Icing Applications," SAE Technical Paper 2007-01-3312, 2007, https://doi.org/10.4271/2007-01-3312.
Additional Details
Publisher
Published
Sep 24, 2007
Product Code
2007-01-3312
Content Type
Technical Paper
Language
English