High Temperature Smart Structures for Engine Noise Reduction and Performance Enhancement

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$599,831.00
Award Year:
2006
Program:
SBIR
Phase:
Phase II
Contract:
NNC06CA03C
Award Id:
72683
Agency Tracking Number:
040779
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
34 Lexington Avenue, Ewing, NJ, 08618
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
096857313
Principal Investigator:
ToddQuackenbush
Principal Investigator
(609) 538-0444
todd@continuum-dynamics.com
Business Contact:
BarbaraAgans
Business Official
(609) 538-0444
barbara@continuum-dynamics.com
Research Institute:
n/a
Abstract
Noise mitigation for subsonic transports is a continuing high priority, and recent work has identified successful exhaust mixing enhancement devices (chevrons) that have demonstrated substantial capability for reducing aircraft engine noise in critical takeoff and landing conditions. Existing fixed-geometry chevrons, however, are inherently limited to optimal noise mitigation in a single operating condition and also can impose significant performance penalties in cruise flight. An adaptive geometry chevron using embedded smart structures technology offers the possibility of maximizing engine performance while retaining and possibly enhancing the favorable noise characteristics of current designs. Phase I identified a promising candidate for a variable geometry chevron using high force Shape Memory Alloy (SMA) actuators. Building on coupled CFD/finite element modeling predicting successful performance, subscale demonstration-level actuated chevrons were constructed that yielded the required deflections in both benchtop and low speed wind tunnel tests. Phase I also identified and tested new high temperature SMA (HTSMA) materials technology to enable the devices to operate in both low temperature (fan) and high temperature (core) exhaust flows. The proposed Phase II effort will continue development of this technology and demonstrate extension of this concept to operation at full-scale stiffness levels and at realistic dynamic pressure and temperature conditions.

* information listed above is at the time of submission.

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