In the wake of recent developments that have reduced fan and jet noise contributions to overall jet-engine noise, aircraft designers are turning their attention toward reducing engine core noise. Innovators at NASA’s Glenn and Langley Research Centers are developing a compact, lightweight acoustic liner based on oxide/oxide ceramic matrix composite (CMC) materials.

NASA’s CMC-based acoustic liner can reduce jet engine noise while also reducing overall engine weight.

The CMC acoustic liner has variable-depth channels tuned to reduce broad-spectrum noise in subsonic jet engines. The design of those channels has also been focused on structures that minimize the overall liner thickness. Because the technology uses CMCs rather than heavy metallic materials, it has the potential to reduce overall engine weight. The oxide/oxide CMC materials are able to withstand extremely high temperatures as well. These CMC acoustic liners can be used in many subsonic jet engines — particularly for next-generation aircraft — to reduce engine core noise. Also, because they can withstand high temperatures, core liners constructed with CMC materials can also provide a thermal barrier.

Researchers are extending an existing oxide/oxide CMC sandwich structure concept that provides mono-tonal noise reduction. That oxide/oxide CMC has a density of about 2.8 g/cc versus the 8.4 g/cc density of a metallic liner made of IN625, thus offering the potential for component weight reduction. The composites have good high-temperature strength and oxidation resistance, allowing them to perform as core liners at temperatures up to 1000 °C (1832 °F).

NASA’s innovation uses cells of different lengths or effective lengths within a compact CMC-based liner to achieve broadband noise reduction. NASA has been able to optimize the performance of the proposed acoustic liner by using improved design tools that help reduce noise over a specified frequency range. One such improvement stems from the enhanced understanding of variable-depth liners, including the benefits of alternate channel shapes/designs (curved, bent, etc.).

These new designs have opened the door for CMC-based acoustic liners to offer core engine noise reduction in a lighter, more compact package. As a first step toward demonstrating advanced concepts, an oxide/oxide CMC acoustic testing article with different channel lengths was tested. Bulk absorbers could also be used, either in conjunction with or in place of the liner’s internal chambers, to reduce noise further if desired.

NASA is actively seeking licensees to commercialize this technology. Please contact the Technology Transfer Office at This email address is being protected from spambots. You need JavaScript enabled to view it. or 216-433-3484. Follow this link here for more information.