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Flight testing a lamb wave based ice accretion sensor

Pohl, Martin (2024) Flight testing a lamb wave based ice accretion sensor. In: AIAA Aviation Forum 2024. AIAA Aviation Forum, 2024-07-29 - 2024-08-02, Las Vegas, USA. doi: 10.2514/6.2024-3525. ISBN 978-1-62410-716-0.

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Kurzfassung

Although modern aircraft have ice protection systems, icing is still a concern today. The reason therefore is constituted by the fact, that ice protection systems can be overwhelmed in severe icing conditions, especially conditions with supercooled large droplets (SLD). In this case water can freeze behind the protected zone or block simpler mechanical deicing systems. For that reason, recognizing icing conditions and assessing their severity as fast as possible is a necessity. This can be achieved by ice sensors, which can help to limit the activation time of ice protection systems to the required time to save fuel or allow to escape severe conditions where the ice protection systems are approaching their limit. Within the EU project SENS4ICE a variety of ice sensors were developed for wind tunnel and flight testing. One of these sensors is the Local Ice Layer Detector (LILD), which operated based on sending lamb wave pulses though an icing prone aircraft surface, such as a leading edge of wing or empennage. An ice accretion alters the wave transmission behavior, which can be used as a detection method. This sensor was developed and flight tested within the project. The paper will present the basic design and measurement principle. The main focus will be on the layout and calibration of the flight test setup. The flight test sensor setup was calibrated in an icing wind tunnel to provide reference data for the flight test. Ground tests with the sensor installed on the aircraft flights in clean air without icing conditions were used to adapt the sensor software to the installation on the aircraft. Finally one test flight will be presented in the paper. It could be shown, that the LILD sensor was able to detect an ice accretion in all icing encounters within the flight test campaign.

elib-URL des Eintrags:https://elib.dlr.de/205792/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Flight testing a lamb wave based ice accretion sensor
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Pohl, MartinMartin.Pohl (at) dlr.dehttps://orcid.org/0000-0002-1825-8419NICHT SPEZIFIZIERT
Datum:2024
Erschienen in:AIAA Aviation Forum 2024
Referierte Publikation:Ja
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
DOI:10.2514/6.2024-3525
ISBN:978-1-62410-716-0
Status:veröffentlicht
Stichwörter:ice sensor, lamb wave, flight test, SENS4ICE, aircraft, icing
Veranstaltungstitel:AIAA Aviation Forum
Veranstaltungsort:Las Vegas, USA
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:29 Juli 2024
Veranstaltungsende:2 August 2024
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Komponenten und Systeme
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L CS - Komponenten und Systeme
DLR - Teilgebiet (Projekt, Vorhaben):L - Flugzeugsysteme
Standort: Braunschweig
Institute & Einrichtungen:Institut für Systemleichtbau > Adaptronik
Hinterlegt von: Pohl, Martin
Hinterlegt am:19 Aug 2024 08:43
Letzte Änderung:19 Aug 2024 08:43

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