An active tendon concept in rotorcraft with variable speed rotors: free vibration perspective: Free vibration perspective

Vaclav Ondra, Robert P. Dibble, Brano Titurus, Benjamin K.S. Woods

Research output: Chapter in Book/Report/Conference proceedingConference Contribution (Conference Proceeding)

4 Citations (Scopus)

Abstract

Rotorcraft with variable speed rotors are known to offer performance improvement, fuel consumption efficiency and noise emissions reduction. However, significant dynamic complications may be encountered as for the various rotor speeds numerous natural frequencies of the main rotor blades can be excited. This paper investigates the use of an active tendon concept to control the dynamic properties of main rotor blades such that their resonances are adaptively avoided based on the current rotor speed. A coupled blade-tendon system is introduced and it is demonstrated that incorporating a tendon into a blade leads to two main effects-a shift of the natural frequencies of the blade, and a manifestation of tuned vibration absorber through frequency loci veering. These effects are explored using numerical simulations in context of their application in rotorcraft with a variable speed rotor. The main rotor of the Bo105 helicopter is used as a reference and it is shown how its dynamic properties may be controlled using a tendon. It is discussed that the reference rotorcraft equipped with the tendon can be operated in the range between 60-120% of its nominal rotor speed without any resonances. In addition, it is hypothesised that this concept could also be used to tune the dynamic properties of rotor blades employing shape adaptive or morphing technologies.

Original languageEnglish
Title of host publicationAIAA Scitech 2019 Forum
PublisherAmerican Institute of Aeronautics and Astronautics Inc. (AIAA)
ISBN (Print)9781624105784
DOIs
Publication statusPublished - 2019
EventAIAA Scitech Forum, 2019 - San Diego, United States
Duration: 7 Jan 201911 Jan 2019
https://scitech.aiaa.org/

Publication series

NameAIAA Scitech 2019 Forum

Conference

ConferenceAIAA Scitech Forum, 2019
CountryUnited States
CitySan Diego
Period7/01/1911/01/19
Internet address

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  • Cite this

    Ondra, V., Dibble, R. P., Titurus, B., & Woods, B. K. S. (2019). An active tendon concept in rotorcraft with variable speed rotors: free vibration perspective: Free vibration perspective. In AIAA Scitech 2019 Forum (AIAA Scitech 2019 Forum). American Institute of Aeronautics and Astronautics Inc. (AIAA). https://doi.org/10.2514/6.2019-0857