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A review of loop heat pipes for aircraft anti-icing applications

  • Qian Su
  • , Shinan Chang*
  • , Yuanyuan Zhao
  • , Haikun Zheng
  • , Chaobin Dang
  • *Corresponding author for this work
  • Beihang University
  • The University of Tokyo

Research output: Contribution to journalReview articlepeer-review

Abstract

Loop heat pipes (LHPs) are highly efficient two-phase heat transfer devices with the ability to transport significant amounts of heat over long distances. Owing to the increasing demand of anti-icing applications in aircraft, certain investigations regarding LHP anti-icing have been successfully conducted, which verified the anti-icing capacity and feasibility of loop heat pipe ice protection system (LHPIPS). In this work, we will conduct a deep analysis on the LHP application to aircraft anti-icing. After a brief introduction of the historical application background and application environment of the LHPIPS, a detailed description of its fundamental design will be elucidated, followed by a series of optimization strategies, including the graphene-coating integration technology, the adoption of bidisperse wicks, the introduction of nanofluids, and the use of double compensation chamber loop heat pipe (DCCLHP). We present the additional points that require further study and that could be further optimized for the development of the LHPIPS. This work contributes to a thorough understanding of the novel and promising LHPIPS, as well as guides its future designs and applications.

Original languageEnglish
Pages (from-to)528-540
Number of pages13
JournalApplied Thermal Engineering
Volume130
DOIs
StatePublished - 5 Feb 2018

Keywords

  • Aircraft anti-icing
  • Fundamental design
  • LHP
  • Loop heat pipe ice protection system
  • Optimization design

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