NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Acoustic Liner for Turbomachinery ApplicationsThe purpose of this innovation is to reduce aircraft noise in the communities surrounding airports by significantly attenuating the noise generated by the turbomachinery, and enhancing safety by providing a containment barrier for a blade failure. Acoustic liners are used in today's turbofan engines to reduce noise. The amount of noise reduction from an acoustic liner is a function of the treatment area, the liner design, and the material properties, and limited by the constraints of the nacelle or casement design. It is desirable to increase the effective area of the acoustic treatment to increase noise suppression. Modern turbofan engines use wide-chord rotor blades, which means there is considerable treatment area available over the rotor tip. Turbofan engines require containment over the rotors for protection from blade failure. Traditional methods use a material wrap such as Kevlar integrated with rub strips and sometimes metal layers (sandwiches). It is possible to substitute the soft rub-strip material with an open-cell metallic foam that provides noise-reduction benefits and a sacrificial material in the first layer of the containment system. An open-cell foam was evaluated that behaves like a bulk acoustic liner, serves as a tip rub strip, and can be integrated with a rotor containment system. Foams can be integrated with the fan-containment system to provide sufficient safety margins and increased noise attenuation. The major innovation is the integration of the foam with the containment.
Document ID
20100033585
Acquisition Source
Glenn Research Center
Document Type
Other - NASA Tech Brief
Authors
Huff, Dennis L.
(NASA Glenn Research Center Cleveland, OH, United States)
Sutliff, Daniel L.
(NASA Glenn Research Center Cleveland, OH, United States)
Jones, Michael G.
(NASA Langley Research Center Hampton, VA, United States)
Hebsur, Mohan G.
(Ohio Aerospace Inst. OH, United States)
Date Acquired
August 25, 2013
Publication Date
September 1, 2010
Publication Information
Publication: NASA Tech Briefs, September 2010
Subject Category
Man/System Technology And Life Support
Report/Patent Number
LEW-18438-1
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available