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Experimental study of two electro-mechanical de-icing systems applied on a wing section tested in an icing wind tunnel

Endres, Matthias and Sommerwerk, Hannah and Mendig, Christian and Sinapius, Michael and Horst, Peter (2017) Experimental study of two electro-mechanical de-icing systems applied on a wing section tested in an icing wind tunnel. CEAS Aeronautical Journal. Springer. doi: 10.1007/s13272-017-0249-0. ISSN 1869-5582.

Full text not available from this repository.

Abstract

Abstract Two electro-mechanical de-icing systems are presented, which are applied to a test specimen consisting of a wing section with an NACA0012 profile. The test specimen is of a modular design to be able to substitute the leading edge section for investigating the different de-icing systems. The de-icing tests are performed in the icing wind tunnel of the Institute of Fluid Mechanics of the TU Braunschweig. The first de-icing concept is an electromechanical system based on structural vibrations of the unstiffened sections. Due to piezoceramic actuators and their positions, the skin is excited at its natural frequency. The actuators are placed at the inner side of the leading edge. The second system under investigation is the Electro- Impulse De-Icing concept. Coils placed underneath the upper and lower aluminum skin are supplied with short, high-current impulses which produce opposing time-dependent magnetic fields around coil and skin. The resulting magnetic forces repel the structure which leads to a damped oscillation of the skin. The first aim of this work is to investigate the performance of the two electromechanical de-icing systems under various icing conditions. Operational parameters like temperature and liquid water content are varied. The test results show that the deicing performance of both systems mainly depends on the ice layer thickness and the environmental temperature. The second aim of this work is to investigate the de-icing mechanism of the accumulated ice. Therefore, the de-icing procedure is recorded with a high-speed camera.

Item URL in elib:https://elib.dlr.de/115412/
Document Type:Article
Title:Experimental study of two electro-mechanical de-icing systems applied on a wing section tested in an icing wind tunnel
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Endres, Matthiastu braunschweigUNSPECIFIED
Sommerwerk, Hannahtu braunschweigUNSPECIFIED
Mendig, Christianchristian.mendig (at) dlr.dehttps://orcid.org/0000-0002-1547-7309
Sinapius, Michaeltu braunschweig / dlr braunschweigUNSPECIFIED
Horst, Petertu braunschweigUNSPECIFIED
Date:29 May 2017
Journal or Publication Title:CEAS Aeronautical Journal
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
DOI:10.1007/s13272-017-0249-0
Editors:
EditorsEmailEditor's ORCID iD
UNSPECIFIEDSpringer-VerlagUNSPECIFIED
Publisher:Springer
ISSN:1869-5582
Status:Published
Keywords:De-Icing, IPS, electromechanical,
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Concepts and Integration (old)
Location: Braunschweig
Institutes and Institutions:Institute of Composite Structures and Adaptive Systems > Adaptronics
Deposited By: Mendig, Christian
Deposited On:05 Dec 2017 08:02
Last Modified:29 Jul 2022 11:53

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