SBIR-STTR Award

Advanced Acoustic Blankets for Improved Aircraft Interior Noise Reduction
Award last edited on: 3/12/2024

Sponsored Program
SBIR
Awarding Agency
NASA : LaRC
Total Award Amount
$669,899
Award Phase
2
Solicitation Topic Code
A2.04
Principal Investigator
Curtis R Mitchell

Company Information

SMD Corporation

19301 Winmeade Drive Suite 208
Leesburg, VA 20176
   (407) 448-0744
   info@smdcorp.com
   www.smdcorp.com
Location: Single
Congr. District: 10
County: Hampton city

Phase I

Contract Number: NNL05AA99P
Start Date: 1/21/2005    Completed: 7/25/2005
Phase I year
2005
Phase I Amount
$69,953
In this project advanced acoustic blankets for improved low frequency interior noise control in aircraft will be developed and demonstrated. The improved performance is achieved with a novel lightweight composite system that has been previously experimentally demonstrated on laboratory structures. The advanced blanket system will also satisfy new flammability and toxicity requirements with minimal integration issues. Work will be carried out with our partner NEVA Associates and acoustic material manufacturers to design commercial versions of the advanced blankets suitable for aircraft. Integration issues related to application in aircraft fuselages will be considered.

Phase II

Contract Number: NNL06AA05C
Start Date: 12/2/2005    Completed: 12/3/2007
Phase II year
2006
Phase II Amount
$599,946
The objective of the proposed Phase II research effort is to develop heterogeneous (HG) blankets for improved sound reduction in aircraft structures. Phase I successfully demonstrated the use of HG blankets for sound transmission suppression and the applicability of the technology to aircraft interior noise control perpetuating a license agreement with a major U.S. Fortune 100 company to aggressively and expeditiously pursue product commercialization. The highest performing HG blanket resulted in ~5 dB reduction in radiated power from an aircraft test panel. Reductions are broadband with an effective frequency range from approximately 100 to 1000 Hz resulting in decreased vibration and radiated acoustic levels across this range. The small 6-10% weight has acoustic benefits far greater than standard mass law effects. In Phase II attachment, temperature, and installation effects will be studied. Additionally, analytical design tools will be developed to automate the design process for practicing engineers making it possible to work from basic concepts and application requirements/specifications to achieve a final product which can be readily manufactured. Together the proven design concepts of Phase I and those proposed in Phase II represent the future in aircraft insulation in terms of acoustic performance, cost, weight, airframe integration, and passenger safety.