+Advanced Search
Inductively heated Ni-CNT/LIT-PDMS composite for ice-phobic/deicing applications
Author:
Affiliation:

Civil Aviation Flight University of China

Clc Number:

TB333

Fund Project:

  • Article
  • |
  • Figures
  • |
  • Metrics
  • |
  • Reference
  • |
  • Related
  • |
  • Cited by
  • |
  • Materials
  • |
  • Comments
    Abstract:

    Aircraft ice accumulation has always been one of the important factors that threaten the safety of aircraft. However, the traditional aircraft de-icing method is unable to cope with the changes of all-electric aircraft and intelligent flight in the future. A new composite material based on Ni, CNT and LIT-PDMS is proposed in this paper, which can make use of eddy current thermal effect for non-contact de-icing, and maintain its reliability in the complex working environment of aircraft. The ni-cnt/lit-pdms composite has a static contact Angle of about 106.5°, which is hydrophobic and can effectively prevent water droplets from accumulating on the surface of the aircraft and thus freezing; When the input voltage of the induction heating device is 30V, the maximum equilibrium temperature of its heating is about 119℃, and it can be heated several times with good thermal stability, only need 232 s to completely melt 20g of ice; the internal conductive network of composites has good stability and resilience after theε=0.001 30 times tension. Ni-CNT/LIT-PDMS composites material can complete the aircraft de-icing work, to ensure flight safety.

    Reference
    Related
    Cited by
Get Citation

[Qin Wenfeng, Wang Xinyuan, Li Yayun, Ai Xuan, Fu Jiawei. Inductively heated Ni-CNT/LIT-PDMS composite for ice-phobic/deicing applications[J]. Rare Metal Materials and Engineering,2021,50(3):1062~1068.]
DOI:10.12442/j. issn.1002-185X.20200269

Copy
Article Metrics
  • Abstract:
  • PDF:
  • HTML:
  • Cited by:
History
  • Received:April 23,2020
  • Revised:April 30,2020
  • Adopted:May 08,2020
  • Online: April 02,2021
  • Published: