Abstract
Conventional piezoelectric ceramic flap actuators have exhibited inadequate levels of stroke and/or force required to produce an angle of rotation in excess of ±5° at 40 Hz for full scale medium sized rotorcraft. Single crystal piezoelectric actuators represent a revolutionary advance in piezoelectric actuator technology. Because crystal electromechanical properties are significantly different than those of ceramic, it should be expected that the use of crystals requires motion amplification techniques that are tailored to crystal behavior. This paper describes a new, high authority trailing edge flap actuator concept for helicopter rotor blade vibration control that has been specifically designed for single crystal stack actuators. Invercon has analytically and experimentally evaluated the feasibility of using single crystals together with a novel, high-moment, high-displacement, buckling beam flap actuator concept, which is well-suited for single crystal stack actuation. Experimental results show that the buckling beam actuator can dramatically outperform state-of-the-art flap actuators with the capability of displacing a 36 " flap ±5° at 40 Hz under representative aerodynamic loading at 400 RPM. Such actuators also consist of less parts, and are significantly lighter than existing designs. This technology may also enable future Army technologies such as swashplateless rotors and trailing edge flaps for heavy lift rotorcraft.
| Original language | English (US) |
|---|---|
| Pages (from-to) | 840-850 |
| Number of pages | 11 |
| Journal | Annual Forum Proceedings - AHS International |
| Volume | II |
| State | Published - Sep 14 2006 |
| Event | AHS Internaitonal 62nd Annual Forum - Phoenix, AZ, United States Duration: May 9 2006 → May 11 2006 |
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All Science Journal Classification (ASJC) codes
- Engineering(all)
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Development of a novel high authority piezoelectric actuator for rotor blades with trailing edge flaps. / Szefi, Joseph T.; Mockensturm, Eric M.; Smith, Edward; Wang, Kon Well; Rehrig, Paul; Centolanza, Louis.
In: Annual Forum Proceedings - AHS International, Vol. II, 14.09.2006, p. 840-850.Research output: Contribution to journal › Conference article
TY - JOUR
T1 - Development of a novel high authority piezoelectric actuator for rotor blades with trailing edge flaps
AU - Szefi, Joseph T.
AU - Mockensturm, Eric M.
AU - Smith, Edward
AU - Wang, Kon Well
AU - Rehrig, Paul
AU - Centolanza, Louis
PY - 2006/9/14
Y1 - 2006/9/14
N2 - Conventional piezoelectric ceramic flap actuators have exhibited inadequate levels of stroke and/or force required to produce an angle of rotation in excess of ±5° at 40 Hz for full scale medium sized rotorcraft. Single crystal piezoelectric actuators represent a revolutionary advance in piezoelectric actuator technology. Because crystal electromechanical properties are significantly different than those of ceramic, it should be expected that the use of crystals requires motion amplification techniques that are tailored to crystal behavior. This paper describes a new, high authority trailing edge flap actuator concept for helicopter rotor blade vibration control that has been specifically designed for single crystal stack actuators. Invercon has analytically and experimentally evaluated the feasibility of using single crystals together with a novel, high-moment, high-displacement, buckling beam flap actuator concept, which is well-suited for single crystal stack actuation. Experimental results show that the buckling beam actuator can dramatically outperform state-of-the-art flap actuators with the capability of displacing a 36 " flap ±5° at 40 Hz under representative aerodynamic loading at 400 RPM. Such actuators also consist of less parts, and are significantly lighter than existing designs. This technology may also enable future Army technologies such as swashplateless rotors and trailing edge flaps for heavy lift rotorcraft.
AB - Conventional piezoelectric ceramic flap actuators have exhibited inadequate levels of stroke and/or force required to produce an angle of rotation in excess of ±5° at 40 Hz for full scale medium sized rotorcraft. Single crystal piezoelectric actuators represent a revolutionary advance in piezoelectric actuator technology. Because crystal electromechanical properties are significantly different than those of ceramic, it should be expected that the use of crystals requires motion amplification techniques that are tailored to crystal behavior. This paper describes a new, high authority trailing edge flap actuator concept for helicopter rotor blade vibration control that has been specifically designed for single crystal stack actuators. Invercon has analytically and experimentally evaluated the feasibility of using single crystals together with a novel, high-moment, high-displacement, buckling beam flap actuator concept, which is well-suited for single crystal stack actuation. Experimental results show that the buckling beam actuator can dramatically outperform state-of-the-art flap actuators with the capability of displacing a 36 " flap ±5° at 40 Hz under representative aerodynamic loading at 400 RPM. Such actuators also consist of less parts, and are significantly lighter than existing designs. This technology may also enable future Army technologies such as swashplateless rotors and trailing edge flaps for heavy lift rotorcraft.
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M3 - Conference article
AN - SCOPUS:33748470461
VL - II
SP - 840
EP - 850
JO - Annual Forum Proceedings - AHS International
JF - Annual Forum Proceedings - AHS International
SN - 1552-2938
ER -