Enhancement of ultrasonic De-icing via transient excitation

Nicola DiPlacido, Jared Soltis, Edward Smith, Jose Palacios

Research output: Chapter in Book/Report/Conference proceedingConference contribution

2 Citations (Scopus)

Abstract

Previous ultrasonic de-icing research on rotorcraft has shown that a multi-frequency tone burst actuation scheme has increased the coverage of the deicing system. The physical mechanisms responsible for this increase in de-icing performance are modeled using finite elements and tested using both freezer ice on a titanium plate and impact ice under rotation in the AERTS facility on a NACA 0015 airfoil structure. Burst actuation techniques are shown to have up to 400% increase in de-icing potential when compared to long tone actuation methods.

Original languageEnglish (US)
Title of host publicationAmerican Helicopter Society International - 2nd Asian/Australian Rotorcraft Forum, ARF 2013 and the 4th International Basic Research Conference on Rotorcraft Technology 2013, IBRCRT 2013
PublisherAmerican Helicopter Society International
Pages376-384
Number of pages9
ISBN (Print)9781632662828
StatePublished - Jan 1 2013
Event2nd Asian/Australian Rotorcraft Forum, ARF 2013 and the 4th International Basic Research Conference on Rotorcraft Technology 2013, IBRCRT 2013 - Tianjin, China
Duration: Sep 8 2013Sep 11 2013

Publication series

NameAmerican Helicopter Society International - 2nd Asian/Australian Rotorcraft Forum, ARF 2013 and the 4th International Basic Research Conference on Rotorcraft Technology 2013, IBRCRT 2013

Other

Other2nd Asian/Australian Rotorcraft Forum, ARF 2013 and the 4th International Basic Research Conference on Rotorcraft Technology 2013, IBRCRT 2013
CountryChina
CityTianjin
Period9/8/139/11/13

Fingerprint

Snow and ice removal
Ultrasonics
Ice
Airfoils
Titanium

All Science Journal Classification (ASJC) codes

  • Automotive Engineering

Cite this

DiPlacido, N., Soltis, J., Smith, E., & Palacios, J. (2013). Enhancement of ultrasonic De-icing via transient excitation. In American Helicopter Society International - 2nd Asian/Australian Rotorcraft Forum, ARF 2013 and the 4th International Basic Research Conference on Rotorcraft Technology 2013, IBRCRT 2013 (pp. 376-384). (American Helicopter Society International - 2nd Asian/Australian Rotorcraft Forum, ARF 2013 and the 4th International Basic Research Conference on Rotorcraft Technology 2013, IBRCRT 2013). American Helicopter Society International.
DiPlacido, Nicola ; Soltis, Jared ; Smith, Edward ; Palacios, Jose. / Enhancement of ultrasonic De-icing via transient excitation. American Helicopter Society International - 2nd Asian/Australian Rotorcraft Forum, ARF 2013 and the 4th International Basic Research Conference on Rotorcraft Technology 2013, IBRCRT 2013. American Helicopter Society International, 2013. pp. 376-384 (American Helicopter Society International - 2nd Asian/Australian Rotorcraft Forum, ARF 2013 and the 4th International Basic Research Conference on Rotorcraft Technology 2013, IBRCRT 2013).
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title = "Enhancement of ultrasonic De-icing via transient excitation",
abstract = "Previous ultrasonic de-icing research on rotorcraft has shown that a multi-frequency tone burst actuation scheme has increased the coverage of the deicing system. The physical mechanisms responsible for this increase in de-icing performance are modeled using finite elements and tested using both freezer ice on a titanium plate and impact ice under rotation in the AERTS facility on a NACA 0015 airfoil structure. Burst actuation techniques are shown to have up to 400{\%} increase in de-icing potential when compared to long tone actuation methods.",
author = "Nicola DiPlacido and Jared Soltis and Edward Smith and Jose Palacios",
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booktitle = "American Helicopter Society International - 2nd Asian/Australian Rotorcraft Forum, ARF 2013 and the 4th International Basic Research Conference on Rotorcraft Technology 2013, IBRCRT 2013",

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DiPlacido, N, Soltis, J, Smith, E & Palacios, J 2013, Enhancement of ultrasonic De-icing via transient excitation. in American Helicopter Society International - 2nd Asian/Australian Rotorcraft Forum, ARF 2013 and the 4th International Basic Research Conference on Rotorcraft Technology 2013, IBRCRT 2013. American Helicopter Society International - 2nd Asian/Australian Rotorcraft Forum, ARF 2013 and the 4th International Basic Research Conference on Rotorcraft Technology 2013, IBRCRT 2013, American Helicopter Society International, pp. 376-384, 2nd Asian/Australian Rotorcraft Forum, ARF 2013 and the 4th International Basic Research Conference on Rotorcraft Technology 2013, IBRCRT 2013, Tianjin, China, 9/8/13.

Enhancement of ultrasonic De-icing via transient excitation. / DiPlacido, Nicola; Soltis, Jared; Smith, Edward; Palacios, Jose.

American Helicopter Society International - 2nd Asian/Australian Rotorcraft Forum, ARF 2013 and the 4th International Basic Research Conference on Rotorcraft Technology 2013, IBRCRT 2013. American Helicopter Society International, 2013. p. 376-384 (American Helicopter Society International - 2nd Asian/Australian Rotorcraft Forum, ARF 2013 and the 4th International Basic Research Conference on Rotorcraft Technology 2013, IBRCRT 2013).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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N2 - Previous ultrasonic de-icing research on rotorcraft has shown that a multi-frequency tone burst actuation scheme has increased the coverage of the deicing system. The physical mechanisms responsible for this increase in de-icing performance are modeled using finite elements and tested using both freezer ice on a titanium plate and impact ice under rotation in the AERTS facility on a NACA 0015 airfoil structure. Burst actuation techniques are shown to have up to 400% increase in de-icing potential when compared to long tone actuation methods.

AB - Previous ultrasonic de-icing research on rotorcraft has shown that a multi-frequency tone burst actuation scheme has increased the coverage of the deicing system. The physical mechanisms responsible for this increase in de-icing performance are modeled using finite elements and tested using both freezer ice on a titanium plate and impact ice under rotation in the AERTS facility on a NACA 0015 airfoil structure. Burst actuation techniques are shown to have up to 400% increase in de-icing potential when compared to long tone actuation methods.

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DiPlacido N, Soltis J, Smith E, Palacios J. Enhancement of ultrasonic De-icing via transient excitation. In American Helicopter Society International - 2nd Asian/Australian Rotorcraft Forum, ARF 2013 and the 4th International Basic Research Conference on Rotorcraft Technology 2013, IBRCRT 2013. American Helicopter Society International. 2013. p. 376-384. (American Helicopter Society International - 2nd Asian/Australian Rotorcraft Forum, ARF 2013 and the 4th International Basic Research Conference on Rotorcraft Technology 2013, IBRCRT 2013).