Volume 3B: General 1993
DOI: 10.1115/93-gt-262
|View full text |Cite
|
Sign up to set email alerts
|

Piezoelectric Actuator-Active Vibration Control of the Shaft Line for a Gas Turbine Engine Test Stand

Abstract: The Active Vibration Control (AVC) actuators which are discussed in the literature include piezoelectric, electromagnetic (contacting and non-contacting) and hydraulic. This paper presents results of an application of rotating machinery active vibration control (AVC) utilizing piezoelectric actuators. The paper gives actual test data on an aircraft engine test stand-shaft line, unlike the majority of related papers which are entirely theoretical or provide test results only on small, laboratory rotors. The AVC… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1

Citation Types

0
2
0
1

Year Published

1997
1997
2022
2022

Publication Types

Select...
3
1

Relationship

0
4

Authors

Journals

citations
Cited by 4 publications
(3 citation statements)
references
References 8 publications
0
2
0
1
Order By: Relevance
“…Similarly, manufacturer speci ed values for d 31 can be found for various piezoceramic materials and hence the analytic moments generated by the patches can be obtained from (2.4). The speci ed values for d 31 can vary by batch, however, and the static values listed by manufacturers are often signi cantly larger than the actual values obtained in dynamic experiments 15,19,20]. Finally, the strain output for the patches often decays over time which is manifested in the moment expression (2.4) by a decrease in d 31 .…”
Section: Strong Form Of the Plate Equationmentioning
confidence: 99%
See 1 more Smart Citation
“…Similarly, manufacturer speci ed values for d 31 can be found for various piezoceramic materials and hence the analytic moments generated by the patches can be obtained from (2.4). The speci ed values for d 31 can vary by batch, however, and the static values listed by manufacturers are often signi cantly larger than the actual values obtained in dynamic experiments 15,19,20]. Finally, the strain output for the patches often decays over time which is manifested in the moment expression (2.4) by a decrease in d 31 .…”
Section: Strong Form Of the Plate Equationmentioning
confidence: 99%
“…While di erences occur between the \handbook" values of the Young's modulus and Poisson ratio and the \true" parameters for the experimental patch, perhaps the biggest source of variation occurs in the values for the strain constant d 31 . The value reported in the product literature (and given in Table 1) was obtained through static tests while the estimated value is obtained in a dynamic setting which tends to decrease the realized values of strain parameters such as d 31 15,19,20]. Hence while the analytic values given by the model (2.5) can be used as starting values in the optimization routine, they will not in general yield an accurate model response due to physical variations in the material patch properties.…”
Section: Example 4: Axisymmetric Excitation { Voltage Spike To Patchmentioning
confidence: 99%
“…Esto se consigue mediante un control activo de la aceleración (Zhu and Tryggvason, 2004). El control de la vibración incluye actuadores (piezoeléctricos, materiales inteligentes, etc) que permiten aplicacio-nes como el eje de una turbina (Palazzolo et al, 1993), estructuras espaciales inflables (Kamel and He, 2010) y estructuras espacialesópticas (Bronowicki et al, 1999).…”
Section: Aplicaciones Del Control Activo-semiactivo En Otrasáreas De unclassified