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Active Gurney Flap Unit

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Abstract

This chapter presents an overview of existing Gurney flap actuation concepts for rotorcraft applications as well as suggests a new concept applicable to airfoils with little space in the vicinity of airfoil toe. Kinematic and dynamic analysis of the mechanism is performed for the required flap motion pattern. A method of calculating maximum normal force acting on Gurney flap is proposed based on inverse dynamics approach. Piezoelectric actuator force-displacement characteristic and mass properties of mechanism parts are also accounted for in the calculations. A working mock-up of the blade section with active Gurney for wind tunnel testing is designed.

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References

  • Barlas TK, van Kuik GA (2010) Review of state of the art in smart rotor control research for wind turbines. Prog Aerosp Sci 46:1–27

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  • Lee T, Chopra I (2001) Design of a bidirectional piezoelectric actuator for blade trailing-edge flap. In: Proceedings of the SPIE 4327, smart structures and materials 2001: smart structures and integrated systems, pp 36–45

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  • Thiel MR, Lesieutre GA, Maughmer MD, Koopmann GH (2006) Actuation of an active gurney flap for rotorcraft applications. AIAA Paper 2006-2181, Newport, Rhode Island

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Correspondence to R. Raczynski .

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© 2017 Springer International Publishing AG

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Berezin, I., Raczynski, R. (2017). Active Gurney Flap Unit. In: Doerffer, P., Barakos, G., Luczak, M. (eds) Recent Progress in Flow Control for Practical Flows. Springer, Cham. https://doi.org/10.1007/978-3-319-50568-8_6

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  • DOI: https://doi.org/10.1007/978-3-319-50568-8_6

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-50567-1

  • Online ISBN: 978-3-319-50568-8

  • eBook Packages: EngineeringEngineering (R0)

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