Development of an SMA actuator for in-flight rotor blade tracking

Dennis K. Kennedy; Friedrich K. Straub; Lawrence McDonald Schetky; Zaffir A. Chaudhry; Richard Roznoy

doi:10.1117/12.388858

22 June 2000 Development of an SMA actuator for in-flight rotor blade tracking

Dennis K. Kennedy, Friedrich K. Straub, Lawrence McDonald Schetky, Zaffir A. Chaudhry, Richard Roznoy

Proceedings Volume 3985, Smart Structures and Materials 2000: Smart Structures and Integrated Systems; (2000) https://doi.org/10.1117/12.388858
Event: SPIE's 7th Annual International Symposium on Smart Structures and Materials, 2000, Newport Beach, CA, United States

Abstract

Another solution to the helicopter blade-tracking problem has been investigated. A discrete, blade-installed actuator utilizing shape memory alloy (SMA) torsion tubes has been developed to enable in-flight rotor tracking. SMA torsion tubes from three materials were tested and one was selected for its cyclic stability. Improved tube fabrication, heating, end attachment methods, and locking schemes were developed. The final prototype actuator employed two bi-axial SMA tubes for actuation/bias; a SMA activated lock for power off operation, and integrated microprocessor control electronics. Tests under static and dynamic loading showed that actuation requirements, except for bandwidth, were met. Increased bandwidth, were met. Increased bandwidth may be obtained by improved control algorithms or cooling. The developed SMA actuator enables an in-flight, real-time adjustment of a blade-tracking tab. Projected payoffs are reduced maintenance cost as well as reduced helicopter vibrations and improved performance.

Citation Download Citation

Dennis K. Kennedy, Friedrich K. Straub, Lawrence McDonald Schetky, Zaffir A. Chaudhry, and Richard Roznoy "Development of an SMA actuator for in-flight rotor blade tracking", Proc. SPIE 3985, Smart Structures and Materials 2000: Smart Structures and Integrated Systems, (22 June 2000); https://doi.org/10.1117/12.388858

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