Development of a Piezoelectric Active Acoustic Liner for Jet Engine Noise Reduction

Award Information
Agency:
Department of Defense
Branch
Navy
Amount:
$79,899.00
Award Year:
2008
Program:
SBIR
Phase:
Phase I
Contract:
N68335-08-C-0479
Award Id:
87738
Agency Tracking Number:
N082-142-0674
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
2513 Pierce Ave., Ames, IA, 50010
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
782766831
Principal Investigator:
Sivaram Gogineni
Project Manager
(937) 266-9570
spgogineni@gmail.com
Business Contact:
Sivaram Gogineni
President
(937) 266-9570
contact@spectralenergies.com
Research Institute:
n/a
Abstract
Acoustic liners are presently used for attenuating combustion and turbine noise radiated from jet engines. Current acoustic liners are passive by nature. This is a drawback because they are only able to absorb acoustic energy over a limited bandwidth. A possible solution to this drawback is the development of an active acoustic liner. The main advantage of this concept is the ability to tune the acoustic impedance for optimal attenuation at variable operating conditions. In this proposal we outline the development of a piezoelectric acoustic liner that is capable of adapting its attenuation characteristics to the various flight regimes, thus making it a candidate for an active acoustic liner. The liner is active because an electrical excitation is applied to the piezoelectric element causing the porous face sheet to vibrate at a prescribed frequency and displacement. Preliminary results have demonstrated that the active liner can improve the absorption characteristics compared to a passive liner. To build upon these results, a computational model will be developed during Phase I to predict the acoustic absorption properties of the piezoelectric actuator and the perforated liner sheet. Then during option portion of Phase I, the computational model will be further developed and experiments will be run to optimize the liner performance.

* information listed above is at the time of submission.

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