中国航空学报(英文版)2024,Vol.37Issue(3) :92-103.DOI:10.1016/j.cja.2024.01.001

Piezoelectric resonant ice protection systems-Part 1/2:Prediction of power requirement for de-icing a NACA 0024 leading edge

Valerian PALANQUE Jason POTHIN Valérie POMMIER-BUDINGER Marc BUDINGER
中国航空学报(英文版)2024,Vol.37Issue(3) :92-103.DOI:10.1016/j.cja.2024.01.001

Piezoelectric resonant ice protection systems-Part 1/2:Prediction of power requirement for de-icing a NACA 0024 leading edge

Valerian PALANQUE 1Jason POTHIN 2Valérie POMMIER-BUDINGER 2Marc BUDINGER1
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作者信息

  • 1. Institut Clement Ader,University of Toulouse,INSA,ISAE-SUPAERO,MINES ALBI,UPS,CNRS,Toulouse 31055,France
  • 2. ISAE-SUPAERO,University of Toulouse,10 Avenue Edouard Belin,Toulouse 31055,France
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Abstract

This paper proposes a numerical method to analyze the ice protection capability and pre-dict the power requirements of a piezoelectric resonant de-icing system.The method is based on a cou-pled electro-mechanical finite element analysis which enables the fast computation of the modes of resonance of interest to de-ice curved surfaces and the estimation of the input voltage and current required for a given configuration(defined by its mode,actuator location,ice deposit,etc.).Eventually,the electric power to be supplied can be also assessed.The method is applied to a NACA 0024 leading edge equipped with piezoelectric actuators.First,two extension modes are analyzed and compared with respect to their efficiency and power requirements.Then,tests are carried out in an icing tunnel to verify the effectiveness of the piezoelectric ice protection system and the predictions of the maximal required power.The system allows de-icing the leading edge in less than 2 s for a glaze ice deposit.

Key words

Ice protection system/Piezoelectric/Resonance mode/Ice fracture/Leading edge de-icing

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出版年

2024
中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
参考文献量27
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